WO2008122046A2 - Method and system for assembling a solar cell package - Google Patents

Method and system for assembling a solar cell package Download PDF

Info

Publication number
WO2008122046A2
WO2008122046A2 PCT/US2008/059167 US2008059167W WO2008122046A2 WO 2008122046 A2 WO2008122046 A2 WO 2008122046A2 US 2008059167 W US2008059167 W US 2008059167W WO 2008122046 A2 WO2008122046 A2 WO 2008122046A2
Authority
WO
WIPO (PCT)
Prior art keywords
region
substrate member
substrate
peripheral region
peripheral
Prior art date
Application number
PCT/US2008/059167
Other languages
French (fr)
Other versions
WO2008122046A3 (en
Inventor
Kevin R. Gibson
Original Assignee
Solaria Corporation
Reglos, Ramon Rosal
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Solaria Corporation, Reglos, Ramon Rosal filed Critical Solaria Corporation
Publication of WO2008122046A2 publication Critical patent/WO2008122046A2/en
Publication of WO2008122046A3 publication Critical patent/WO2008122046A3/en

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/042PV modules or arrays of single PV cells
    • H01L31/048Encapsulation of modules
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/064Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms
    • B23K26/066Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms by using masks
    • B23K26/0661Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms by using masks disposed on the workpiece
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/1429Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the way of heating the interface
    • B29C65/1435Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the way of heating the interface at least passing through one of the parts to be joined, i.e. transmission welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/1496Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation making use of masks
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1629Laser beams characterised by the way of heating the interface
    • B29C65/1635Laser beams characterised by the way of heating the interface at least passing through one of the parts to be joined, i.e. laser transmission welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1629Laser beams characterised by the way of heating the interface
    • B29C65/1654Laser beams characterised by the way of heating the interface scanning at least one of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1687Laser beams making use of light guides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1696Laser beams making use of masks
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/78Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus
    • B29C65/7802Positioning the parts to be joined, e.g. aligning, indexing or centring
    • B29C65/7805Positioning the parts to be joined, e.g. aligning, indexing or centring the parts to be joined comprising positioning features
    • B29C65/7814Positioning the parts to be joined, e.g. aligning, indexing or centring the parts to be joined comprising positioning features in the form of inter-cooperating positioning features, e.g. tenons and mortises
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/02Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/022Mechanical pre-treatments, e.g. reshaping
    • B29C66/0222Mechanical pre-treatments, e.g. reshaping without removal of material, e.g. cleaning by air blowing or using brushes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/12Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
    • B29C66/124Tongue and groove joints
    • B29C66/1246Tongue and groove joints characterised by the female part, i.e. the part comprising the groove
    • B29C66/12461Tongue and groove joints characterised by the female part, i.e. the part comprising the groove being rounded, i.e. U-shaped or C-shaped
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/12Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
    • B29C66/124Tongue and groove joints
    • B29C66/1246Tongue and groove joints characterised by the female part, i.e. the part comprising the groove
    • B29C66/12463Tongue and groove joints characterised by the female part, i.e. the part comprising the groove being tapered
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/20Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/24Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight
    • B29C66/242Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours
    • B29C66/2424Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain
    • B29C66/24243Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain forming a quadrilateral
    • B29C66/24244Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being a closed polygonal chain forming a quadrilateral forming a rectangle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/347General aspects dealing with the joint area or with the area to be joined using particular temperature distributions or gradients; using particular heat distributions or gradients
    • B29C66/3474General aspects dealing with the joint area or with the area to be joined using particular temperature distributions or gradients; using particular heat distributions or gradients perpendicular to the plane of the joint
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/54Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/83General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/832Reciprocating joining or pressing tools
    • B29C66/8322Joining or pressing tools reciprocating along one axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/90Measuring or controlling the joining process
    • B29C66/91Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
    • B29C66/914Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux
    • B29C66/9141Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature
    • B29C66/91411Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature of the parts to be joined, e.g. the joining process taking the temperature of the parts to be joined into account
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/90Measuring or controlling the joining process
    • B29C66/91Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
    • B29C66/919Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges
    • B29C66/9192Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/90Measuring or controlling the joining process
    • B29C66/92Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools
    • B29C66/924Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools by controlling or regulating the pressure, the force, the mechanical power or the displacement of the joining tools
    • B29C66/9241Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools by controlling or regulating the pressure, the force, the mechanical power or the displacement of the joining tools by controlling or regulating the pressure, the force or the mechanical power
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/90Measuring or controlling the joining process
    • B29C66/92Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools
    • B29C66/929Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools characterized by specific pressure, force, mechanical power or displacement values or ranges
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/054Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
    • H01L31/0547Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means comprising light concentrating means of the reflecting type, e.g. parabolic mirrors, concentrators using total internal reflection
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1629Laser beams characterised by the way of heating the interface
    • B29C65/1664Laser beams characterised by the way of heating the interface making use of several radiators
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1629Laser beams characterised by the way of heating the interface
    • B29C65/1674Laser beams characterised by the way of heating the interface making use of laser diodes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1677Laser beams making use of an absorber or impact modifier
    • B29C65/1683Laser beams making use of an absorber or impact modifier coated on the article
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/02Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/026Chemical pre-treatments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/02Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/028Non-mechanical surface pre-treatments, i.e. by flame treatment, electric discharge treatment, plasma treatment, wave energy or particle radiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • B29C66/712General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined the composition of one of the parts to be joined being different from the composition of the other part
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/723General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/731General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the intensive physical properties of the material of the parts to be joined
    • B29C66/7316Surface properties
    • B29C66/73161Roughness or rugosity
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/733General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the optical properties of the material of the parts to be joined, e.g. fluorescence, phosphorescence
    • B29C66/7336General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the optical properties of the material of the parts to be joined, e.g. fluorescence, phosphorescence at least one of the parts to be joined being opaque, transparent or translucent to visible light
    • B29C66/73365General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the optical properties of the material of the parts to be joined, e.g. fluorescence, phosphorescence at least one of the parts to be joined being opaque, transparent or translucent to visible light at least one of the parts to be joined being transparent or translucent to visible light
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B29C66/73921General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/90Measuring or controlling the joining process
    • B29C66/91Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
    • B29C66/919Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0072Roughness, e.g. anti-slip
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/30Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3055Cars
    • B29L2031/3061Number plates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/756Microarticles, nanoarticles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • Y02E10/52PV systems with concentrators

Definitions

  • the present invention relates generally to solar energy techniques.
  • the present invention provides a method and resulting device fabricated from a plurality of concentrating elements respectively coupled to a plurality of photovoltaic regions.
  • concentrating elements are coupled to a plurality of photovoltaic regions using one or more coupled structures.
  • the present method and structure are directed to a laser sealing technique of a solar cell package apparatus.
  • the invention has been applied to solar panels, commonly termed modules, but it would be recognized that the invention has a much broader range of applicability.
  • Solar energy possesses many characteristics that are very desirable! Solar energy is renewable, clean, abundant, and often widespread. Certain technologies developed often capture solar energy, concentrate it, store it, and convert it into other useful forms of energy.
  • Solar panels have been developed to convert sunlight into energy.
  • solar thermal panels often convert electromagnetic radiation from the sun into thermal energy for heating homes, running certain industrial processes, or driving high grade turbines to generate electricity.
  • solar photovoltaic panels convert sunlight directly into electricity for a variety of applications.
  • Solar panels are generally composed of an array of solar cells, which are interconnected to each other. The cells are often arranged in series and/or parallel groups of cells in series. Accordingly, solar panels have great potential to benefit our nation, security, and human users. They can even diversify our energy requirements and reduce the world's dependence on oil and other potentially detrimental sources of energy.
  • the present invention relates generally to solar energy techniques.
  • the present invention provides a method and resulting device fabricated from a plurality of concentrating elements respectively coupled to a plurality of photovoltaic regions.
  • concentrating elements are coupled to a plurality of photovoltaic regions using one or more coupled structures.
  • the present method and structure are directed to a laser sealing technique of a solar cell package apparatus.
  • the invention has been applied to solar panels, commonly termed modules, but it would be recognized that the invention has a much broader range of applicability.
  • the present invention provides a method for fabricating solar cell for a solar panel.
  • the method includes providing a first substrate member comprising a plurality of photovoltaic strips thereon.
  • the method includes providing an optical elastomer material overlying a portion of the first substrate member.
  • the method aligns a second substrate member comprising a plurality of optical concentrating elements thereon such that at least one of the optical concentrating elements is operably coupled to at least one of the plurality of photovoltaic strips.
  • the second substrate member comprises an aperture surface region and an exit surface region.
  • the present invention provides A method for fabricating a solar cell free and separate from a solar panel.
  • the method includes providing a first substrate member comprising a plurality of photovoltaic strips thereon, the first substrate member having a first peripheral region, the first peripheral region including a first flat region and a first structure region, the first structure region including a protruding structure.
  • the method also includes providing an optical elastomer material overlying a portion of the first substrate member. Furthermore, the method includes providing a second substrate member having a second peripheral region, the second peripheral region including a second flat region and a second structure region, the second structure region including an indent structure. Additionally, the method includes aligning the second substrate member comprising a plurality of optical concentrating elements thereon such that the first flat region of the first substrate mates with the second flat region of the second substrate and the first structure region, the second substrate member comprising an aperture surface region and an exit surface region. The method also includes coupling the first substrate member to the second substrate member to form a sealing region between the first peripheral region of the first substrate member and the second peripheral region of the second substrate member and to engage the first structure region of the first substrate to the second structure region of the second substrate.
  • the present invention provides a solar cell package.
  • the package includes a first substrate member comprising a plurality of photovoltaic strips thereon, the first substrate member having a first peripheral region, the first peripheral region including a first flat region and a first structure region, the first structure region comprising an protruding structure.
  • the package also includes an optical elastomer material overlying a portion of the first substrate member.
  • the package also includes a second substrate member having a second peripheral region, the second peripheral region including a second flat region and a second structure region, the second substrate being aligned such that the first flat region of the first substrate mates with the second flat region of the second substrate and the first structure region, the second substrate member comprising an aperture surface region and an exit surface region, the second structure region comprising an indent structure.
  • the method also irradiates an entirety of the second peripheral region of the second substrate member using electromagnetic radiation to seal the interface region between the second substrate and the first substrate.
  • the blocking selectively allows for irradiation of the second peripheral region of the second substrate member to seal the interface region.
  • irradiating an entirety of the second peripheral region of the second substrate member uses a flash or pulses of electromagnetic radiation to seal the interface region between the second substrate and the first substrate, while the inner region of the aperture surface region remains blocked using blocking material.
  • the invention provides a system for manufacture of solar cells.
  • the apparatus has a stage member, which can be a mechanical attachment member, vacuum member, or other suitable device.
  • the apparatus has a first substrate member comprising a plurality of photovoltaic regions thereon provided on the stage member, an optical elastomer material overlying a portion of the first substrate member, an aligned second substrate member comprising a plurality of optical concentrating elements thereon such that at least one of the optical concentrating elements being operably coupled to at least one of the plurality of photovoltaic strips, the second substrate member comprising an aperture surface region and an exit surface region, and an interface region provided along a first peripheral region of the first substrate member and a second peripheral region of the second substrate member.
  • a blocking member is provided within an inner region of the aperture surface region of the second substrate member while exposing the peripheral region of the aperture surface region of the second substrate member.
  • the apparatus also has an irradiation source coupled to the stage member.
  • the irradiation source is adapted to irradiate an entirety of the second peripheral region of the second substrate member using a flash or pulses of electromagnetic radiation to seal the interface region between the second substrate and the first substrate, while the inner region of the aperture surface region remains blocked using blocking material.
  • the present technique provides an easy to use process that relies upon conventional technology such as silicon materials, although other materials can also be used.
  • the method provides a process that is compatible with conventional process technology without substantial modifications to conventional equipment and processes.
  • the invention provides for an improved solar cell, which is less costly and easy to handle.
  • Such solar cell uses a plurality of photovoltaic regions, which are sealed within one or more substrate structures according to a preferred embodiment.
  • the invention provides a method and completed solar cell structure using a plurality of photovoltaic strips free and clear from a module or panel assembly, which are provided during a later assembly process.
  • one or more of the solar cells have less silicon per area (e.g., 80% or less, 50% or less) than conventional solar cells.
  • the present method and cell structures are also light weight and not detrimental to building structures and the like. That is, the weight is about the same or slightly more than conventional solar cells at a module level according to a specific embodiment.
  • the present solar cell using the plurality of photovoltaic strips can be used as a "drop in" replacement of conventional solar cell structures. As a drop in replacement, the present solar cell can be used with conventional solar cell technologies for efficient implementation according to a preferred embodiment.
  • the present method and system provide a way of sealing an interface region between two substrate members using an electromagnetic radiation source, which is relatively easy to use and cost effective.
  • an electromagnetic radiation source which is relatively easy to use and cost effective.
  • one or more of these benefits may be achieved.
  • FIG. 1 is a simplified diagram of a solar cell according to an embodiment of the present invention.
  • FIG. 2 is a simplified diagram of solar cell concentrating elements according to an embodiment of the present invention.
  • Figure 2A is a simplified side-view diagram of solar cell concentrating elements according to an embodiment of the present invention.
  • FIGS 3, 3A, and 3B are simplified flow diagrams illustrating a method of assembling a solar cell apparatus according to an embodiment of the present invention
  • Figure 4 is a simplified diagram of coupling a back cover member to a concentrator member according to an embodiment of the present invention
  • Figures 5 and 5A are a simplified diagrams of irradiating peripheral regions of the concentrator member and back cover member to seal them together according to an embodiment of the present invention
  • Figure 6 is a simplified side-view diagram of a concentrator member and a back cover according to an embodiment of the present invention
  • Figure 7 is a more detailed diagram of a back cover device and a concentrator device according to an embodiment of the present invention.
  • Figure 8 is a simplified plot of temperature gradient in z direction in the seal region according to an embodiment of the present invention.
  • the present invention relates generally to solar energy techniques.
  • the present invention provides a method and resulting device fabricated from a plurality of concentrating elements respectively coupled to a plurality of photovoltaic regions.
  • concentrating elements are coupled to a plurality of photovoltaic regions using one or more coupled structures.
  • the present method and structure are directed to a laser sealing technique of a solar cell package apparatus.
  • the invention has been applied to solar panels, commonly termed modules, but it would be recognized that the invention has a much broader range of applicability.
  • FIG. 1 is a simplified diagram of a solar cell according to an embodiment of the present invention.
  • This diagram is merely an example, which should not unduly limit the scope of the claims herein.
  • One of ordinary skill in the art would recognize other variations, modifications, and alternatives.
  • the device has a back cover member 101, which includes a surface area and a back area.
  • the back cover member also has a plurality of sites, which are spatially disposed, for electrical members, such as bus bars, and a plurality of photovoltaic regions.
  • the back cover can be free from any patterns and is merely provided for support and packaging.
  • the device has a plurality of photovoltaic strips 105, each of which is disposed overlying the surface area of the back cover member.
  • the plurality of photovoltaic strips corresponds to a cumulative area occupying a total photovoltaic spatial region, which is active and converts sunlight into electrical energy.
  • An encapsulating material 115 is overlying a portion of the back cover member. That is, an encapsulating material forms overlying the plurality of strips, and exposed regions of the back cover, and electrical members.
  • the encapsulating material can be a single layer, multiple layers, or portions of layers, depending upon the application.
  • the encapsulating material can be provided overlying a portion of the photovoltaic strips or a surface region of the front cover member, which would be coupled to the plurality of photovoltaic strips.
  • the encapsulating material can be provided overlying a portion of the photovoltaic strips or a surface region of the front cover member, which would be coupled to the plurality of photovoltaic strips.
  • a front cover member 121 is coupled to the encapsulating material. That is, the front cover member is formed overlying the encapsulant to form a multilayered structure including at least the back cover, bus bars, plurality of photovoltaic strips, encapsulant, and front cover.
  • the front cover includes one or more concentrating elements, which concentrate (e.g., intensify per unit area) sunlight onto the plurality of photovoltaic strips. That is, each of the concentrating elements can be associated respectively with each of or at least one of the photovoltaic strips.
  • an interface region is provided along at least a peripheral region of the back cover member and the front cover member.
  • the interface region may also be provided surrounding each of the strips or certain groups of the strips depending upon the embodiment.
  • the device has a sealed region and is formed on at least the interface region to form an individual solar cell from the back cover member and the front cover member.
  • the sealed region maintains the active regions, including photovoltaic strips, in a controlled environment free from external effects, such as weather, mechanical handling, environmental conditions, and other influences that may degrade the quality of the solar cell.
  • the sealed region and/or sealed member (e.g., two substrates) protect certain optical characteristics associated with the solar cell and also protects and maintains any of the electrical conductive members, such as bus bars, interconnects, and the like.
  • the sealed member structure there can be other benefits achieved using the sealed member structure according to other embodiments.
  • the total photovoltaic spatial region occupies a smaller spatial region than the surface area of the back cover. That is, the total photovoltaic spatial region uses less silicon than conventional solar cells for a given solar cell size. In a preferred embodiment, the total photovoltaic spatial region occupies about 80% and less of the surface area of the back cover for the individual solar cell. Depending upon the embodiment, the photovoltaic spatial region may also occupy about 70% and less or 60% and less or preferably 50% and less of the surface area of the back cover or given area of a solar cell. Of course, there can be other percentages that have not been expressly recited according to other embodiments.
  • back cover member and “front cover member” are provided for illustrative purposes, and not intended to limit the scope of the claims to a particular configuration relative to a spatial orientation according to a specific embodiment. Further details of each of the various elements in the solar cell can be found throughout the present specification and more particularly below.
  • the present invention provides a packaged solar cell assembly being capable of stand-alone operation to generate power using the packaged solar cell assembly and/or with other solar cell assemblies.
  • the packaged solar cell assembly includes rigid front cover member having a front cover surface area and a plurality of concentrating elements thereon.
  • the rigid front cover member consists of a variety of materials.
  • the rigid front cover is made of polymer material.
  • the rigid front cover is made of transparent polymer material having a reflective index of about 1.4 or 1.42 or greater.
  • the rigid front cover has a Young's Modulus of a suitable range.
  • Each of the concentrating elements has a length extending from a first portion of the front cover surface area to a second portion of the front cover surface area.
  • Each of the concentrating elements has a width provided between the first portion and the second portion.
  • Each of the concentrating elements having a first edge region coupled to a first side of the width and a second edge region provided on a second side of the width. The first edge region and the second edge region extend from the first portion of the front cover surface area to a second portion of the front cover surface area.
  • the plurality of concentrating elements is configured in a parallel manner extending from the first portion to the second portion.
  • embodiment can have many variations.
  • the embodiment may further includes a first electrode member that is coupled to a first region of each of the plurality of photovoltaic strips and a second electrode member coupled to a second region of each of the plurality of photovoltaic strips.
  • the solar cell assembly additionally includes a first electrode member coupled to a first region of each of the plurality of photovoltaic strips and a second electrode member coupled to a second region of each of the plurality of photovoltaic strips.
  • the first electrode includes a first protruding portion extending from a first portion of the sandwiched assembly and the second electrode comprising a second protruding portion extending from a second portion of the sandwiched assembly.
  • the present invention provides a solar cell apparatus.
  • the solar cell apparatus includes a backside substrate member comprising a backside surface region and an inner surface region.
  • the backside substrate member can be made from various materials.
  • the backside member is characterized by a polymer material.
  • the present invention provides a solar cell apparatus that includes a backside substrate member.
  • the backside substrate member includes a backside surface region and an inner surface region.
  • the backside substrate member is characterized by a width.
  • the backside substrate member is characterized by a length of about eight inches and less.
  • the backside substrate member is characterized by a width of about 8 inches and less and a length of more than 8 inches.
  • U.S. Patent Application 11/445,993 (Attorney Docket No.: 025902-000210US), commonly assigned, and hereby incorporated by reference herein.
  • FIG. 2 is a simplified diagram of solar cell concentrating elements 201 according to an embodiment of the present invention.
  • This diagram is merely an example, which should not unduly limit the scope of the claims herein.
  • One of ordinary skill in the art would recognize other variations, modifications, and alternatives.
  • each of the concentrating elements for the strip configuration includes a trapezoidal shaped member 205.
  • Each of the trapezoidal shaped members has a bottom surface 203 coupled to a pyramidal shaped region coupled to an upper region 207.
  • the upper region is defined by surface 209, which is co-extensive of the front cover.
  • Each of the members is spatially disposed and in parallel to each other according to a specific embodiment.
  • a solar cell apparatus includes a shaped concentrator device operably coupled to each of the plurality of photovoltaic strips.
  • the shaped concentrator device has a first side and a second side.
  • the solar cell apparatus includes an aperture region provided on the first side of the shaped concentrator device.
  • the concentrator device includes a first side region and a second side region.
  • the first side region is characterized by a roughness of about 100 nanometers or 120 nanometers RMS and less
  • the second side region is characterized by a roughness of about 100 nanometers or 120 nanometers RMS and less.
  • the roughness is characterized by a dimension value of about 10% of a light wavelength derived from the aperture regions.
  • the backside member can have a pyramid-type shape.
  • the solar cell apparatus includes an exit region provided on the second side of the shaped concentrator device.
  • the solar cell apparatus includes a geometric concentration characteristic provided by a ratio of the aperture region to the exit region. The ratio can be characterized by a range from about 1.8 to about 4.5.
  • the solar cell apparatus also includes a polymer material characterizing the shaped concentrator device.
  • the solar cell apparatus additionally includes a refractive index of about 1.45 and greater characterizing the polymer material of the shaped concentrator device.
  • the solar cell apparatus includes a coupling material formed overlying each of the plurality of photovoltaic strips and coupling each of the plurality of photovoltaic regions to each of the concentrator devices.
  • the coupling material is characterized by a suitable Young's Modulus.
  • the solar cell apparatus includes a refractive index of about 1.45 and greater characterizing the coupling material coupling each of the plurality of photovoltaic regions to each of the concentrator device.
  • the polymer material is characterized by a thermal expansion constant that is suitable to withstand changes due to thermal expansion of elements of the solar cell apparatus.
  • the plurality of concentrating elements has a light entrance area (Al) and a light exit area (A2) such that A2/A1 is 0.8 and less.
  • the plurality of concentrating elements has a light entrance area (Al) and a light exit area (A2) such that A2/A1 is 0.8 and less, and the plurality of photovoltaic strips are coupled against the light exit area.
  • the ratio of A2/A1 is about 0.5 and less.
  • each of the concentrating elements has a height of 7mm or less.
  • the sealed sandwiched assembly has a width ranging from about 100 millimeters to about 210 millimeters and a length ranging from about 100 millimeters to about 210 millimeters. In a specific embodiment, the sealed sandwiched assembly can even have a length of about 300 millimeters and greater.
  • each of the concentrating elements has a pair of sides. In a specific embodiment, each of the sides has a surface finish of 100 nanometers or less or 120 nanometers and less RMS. Of course, there can be other variations, modifications, and alternatives.
  • FIG. 2A the front cover has been illustrated using a side view 201, which is similar to Figure 2.
  • the front cover also has a top-view illustration 210.
  • a section view 220 from “B-B” has also been illustrated.
  • a detailed view "A" of at least two of the concentrating elements 230 is also shown.
  • the concentrating elements are made of a suitable material.
  • the concentrating elements can be made of a polymer, glass, or other optically transparent materials, including any combination of these, and the like.
  • the suitable material is preferably environmentally stable and can withstand environmental temperatures, weather, and other "outdoor" conditions.
  • the concentrating elements can also include portions that are coated with an anti-reflective coating for improved efficiency. Coatings can also be used for improving a durability of the concentrating elements.
  • the solar cell apparatus includes a first reflective side provided between a first portion of the aperture region and a first portion of the exit region.
  • the first reflective side includes a first polished surface of a portion of the polymer material.
  • the first reflective side is characterized by a surface roughness of about 120 nanometers RMS and less.
  • the solar cell apparatus includes a second reflective side provided between a second portion of the aperture region and a second portion of the exit region.
  • the second reflective side comprises a second polished surface of a portion of the polymer material.
  • the second reflective side is characterized by a surface roughness of about 120 nanometers and less.
  • the first reflective side and the second reflective side provide for total internal reflection of one or more photons provided from the aperture region.
  • the solar cell apparatus includes a geometric concentration characteristic provided by a ratio of the aperture region to the exit region.
  • the ratio is characterized by a range from about 1.8 to about 4.5.
  • the solar cell apparatus includes a polymer material characterizing the shaped concentrator device, which includes the aperture region, exit region, first reflective side, and second reflective side.
  • the polymer material is capable of being free from damaged caused by ultraviolet radiation.
  • the solar cell apparatus has a refractive index of about 1.45 and greater characterizing the polymer material of the shaped concentrator device.
  • the solar cell apparatus includes a coupling material formed overlying each of the plurality of photovoltaic strips and coupling each of the plurality of photovoltaic regions to each of the concentrator devices.
  • the solar cell apparatus additionally includes one or more pocket regions facing each of the first reflective side and the second reflective side. The one or more pocket regions can be characterized by a refractive index of about 1 to cause one or more photons from the aperture region to be reflected toward the exit region.
  • each of the concentrating elements is separated by a region having a notch structure of a predetermined size and shape according to a specific embodiment.
  • a notch structure of a predetermined size and shape according to a specific embodiment.
  • FIG. 3 is a simplified flow diagram illustrating a method of assembling a solar cell apparatus according to an embodiment of the present invention.
  • the method provides a first substrate member (Step 302).
  • the first substrate member includes a plurality of photovoltaic strips thereon.
  • the method provides a second substrate member (Step 304) which includes a plurality of optical concentrating elements.
  • the first substrate member is aligned and couple to the second substrate member (Step 306).
  • an inner region of the second substrate member (Step 308) is blocked from irradiation while a peripheral region remained exposed (Step 310).
  • a pressure is applied (Step 314).
  • the method includes irradiating the exposed peripheral region of the second substrate member (Step 312) and forming a melting region in an interface region between the first substrate member and the second substrate member. The melting region is used to seal peripheral interface between first substrate and second substrate (Step 316).
  • the method continues with other steps (Step 318) to complete the solar cell panel.
  • FIG. 3 A is a simplified flow diagram illustrating a method of assembling a solar cell apparatus according to an embodiment of the present invention.
  • This diagram is merely an example, which should not unduly limit the scope of the claims herein.
  • the method provides a first substrate member (Step 302).
  • the first substrate member includes a plurality of photovoltaic strips thereon.
  • the method provides a second substrate member (Step 304) which includes a plurality of optical concentrating elements.
  • the method also includes providing a high emissivity back cover device (Step 305).
  • the first substrate member is aligned and couple to the second substrate member (Step 306).
  • an inner region of the second substrate member (Step 308) is blocked from irradiation while a peripheral region remained exposed (Step 310).
  • a pressure is applied (Step 314).
  • the method includes irradiating the exposed peripheral region of the second substrate member (Step 312) and forming a melting region in an interface region between the first substrate member and the second substrate member.
  • laser is used for providing irradiation.
  • the melting region is used to seal peripheral interface between first substrate and second substrate (Step 316).
  • the method continues with other steps (Step 318) to complete the solar cell panel.
  • FIG. 3B is a simplified flow diagram illustrating a method of assembling a solar cell apparatus according to an embodiment of the present invention.
  • the method provides a first substrate member (Step 302).
  • the first substrate member includes a plurality of photovoltaic strips thereon.
  • the method provides a second substrate member (Step 304) which includes a plurality of optical concentrating elements.
  • the method also includes providing a high emissivity back cover device (Step 305).
  • the first substrate member is aligned and couple to the second substrate member (Step 306).
  • a pressure is applied (Step 308).
  • an inner region of the second substrate member (Step 310) is blocked from irradiation while a peripheral region remained exposed (Step 312).
  • the method includes irradiating the exposed peripheral region of the second substrate member (Step 314) and forming a melting region in an interface region between the first substrate member and the second substrate member. The melting region is used to seal peripheral interface between first substrate and second substrate (Step 316). The method continues with other steps (Step 318) to complete the solar cell panel.
  • FIG 4 is a simplified diagram of coupling 400 a back cover member 401 to a concentrator member 402 according to an embodiment of the present invention.
  • This diagram is merely an example, which should not unduly limit the scope of the claims herein.
  • the back cover member 401 includes, a first peripheral region 404, which has a protruding structure 406 and a first flat region in a portion of the first peripheral region.
  • the concentrator member includes a second peripheral region 408, which has an indent structure 410 and a second flat region in a portion of the second peripheral region.
  • the protruding structure and the indent structure provides a tongue and groove mechanism to couple the back cover member and the concentrator member.
  • the back cover member and the concentrator member may be aligned using the tongue and groove mechanism in a specific embodiment, the protruding structure 406 of the back cover member is aligned to a second peripheral region 408 of the concentrator member such that each of the plurality of photovoltaic strips is coupled to a concentrator element in the concentrator member.
  • the coupled substrate member includes an interface region 412 formed from the first peripheral region and the second peripheral region.
  • the protruding structure 410 has a semi-circular cross section.
  • the protruding structure 410 has a diameter of about 10/1000 of an inch or less and runs along the second peripheral region of the concentrator member.
  • the protruding structure can be any shape, for example, the cross section can be rectangular, or other polygon shapes.
  • the indent structure can be shaped accordingly to mate with the protruding structure.
  • the interface region may be subjected to a cleaning process to remove any material that may affect sealing of the substrate members.
  • the cleaning process can include using a suitable solvents or a combination of solvents followed by drying.
  • the cleaning process may include a plasma cleaning, or a blasting process to remove undesirable material.
  • a plasma cleaning or a blasting process to remove undesirable material.
  • a force is provided to mechanically couple the aligned concentrator member to the back cover member.
  • the force may be provided by a plate, fluid pressure, a clamp or any other suitable techniques. Further details of the applied force can be found through the present specification and particularly below. Of course there can be other variations, modifications, and alternatives.
  • FIG 5-7 are simplified diagrams of joining the concentrator member and back cover member and to seal them together using an electromagnetic radiation according to an embodiment of the present invention. These diagrams are merely examples, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives.
  • a stage member including a waveguide device 504 is provided.
  • the waveguide device includes an inner waveguide 506, an outer waveguide 508, and an opening region 510.
  • the waveguide device also includes an upper surface region 512 and a back surface region 514.
  • the electromagnetic radiation is allowed to pass through the opening region of the waveguide device and blocked by the inner waveguide region and the outer waveguide region.
  • the opening region includes a straight face region 518 and an oblique face region 520.
  • the straight face region may be a flat surface.
  • the straight face region may also be a curved surface that is concave or convex depending on the application.
  • the oblique face region may be a flat surface.
  • the oblique face region may be a curved surface depending upon the application.
  • the oblique face region and the straight face region allow for a maximum transmission of the electromagnetic radiation through the opening region.
  • the waveguide device is preferably made of a highly reflective material at least in the straight face region and the oblique face region.
  • the waveguide device is made of a gold plated alloy.
  • the alloy may be steel and/or other metal materials.
  • the waveguide device is configured to allow for a concentration of the electromagnetic radiation to concentrate at a weld region 516 in the peripheral region in a specific embodiment.
  • a top view of the waveguide device is shown in Figure 5A. Of cause there can be other variations, modifications, and alternatives.
  • the waveguide device is provided overlying the aperture region of the concentrator member.
  • a force 522 is applied on the front surface region of the waveguide device to mechanically couple the concentrator member to the back cover member to form the peripheral region as also shown in Figure 5.
  • the mechanical force can be provided using air pressure or a weight such as a cylinder providing a pressure ranging from about 100 psi to about 200 psi. Other means of mechanical forces, such as an air pressure, may also be used. Of course there can be other variations, modifications, and alternatives.
  • the coupled concentrator member and the back cover member is irradiated using an electromagnetic radiation 602.
  • the electromagnetic radiation may be provided using a energy source such as a laser source or a flash lamp or other suitable energy source.
  • the electromagnetic radiation may be provided using a laser (e.g., laser diode, tunable dye, etc.) having a suitable wavelength range and providing a suitable power range.
  • the electromagnetic radiation is provided for a time period of about eight seconds or less and preferably 1-4 seconds. Effectively, the electromagnetic radiation traverses through the entire exposed peripheral region of at least the concentrator member of the coupled substrate within the entire time period and provides energy to cause a melt region 608 in the interface region while the inner region is blocked from the electromagnetic radiation.
  • the electromagnetic radiation and/or laser energy is guided using one or more fiber optics 606 from a source 604 and through the opening region of the waveguide device to the peripheral region of the coupled substrate to provide energy to cause the melt region in the peripheral region.
  • the source 604 is a laser source.
  • the laser source provides pulses of energy and the one or more fiber optics are allowed to translate above the opening region of the waveguide device to provide energy to cause the melt region in the interface region of the coupled substrate members in a specific embodiment.
  • the electromagnetic radiation can be derived from Laser IRAM assembly systems Models 200 and 300 manufactured by Branson Ultrasonics Corp., 41 Eagle Rd., Danbury, CT 06813-1961, USA. Of course there can be other variations, modifications, and alternatives.
  • the light/laser radiation traverses through the entire thickness of the concentrator member, which can be a polymer component transmissive to light.
  • the energy is absorbed at least by the back cover member at the interface region to cause a melt region 608 in the interface region.
  • the back cover member is made of a light absorbing material at least in the second peripheral region.
  • the light absorbing material absorbs irradiation energy traversing at least the first peripheral region of the concentrator element, which is transparent, to cause heating and to form the melting region in the interface region.
  • the light absorbing material can also be a light blocking material or include each of these characteristics.
  • the light absorbing material may be provided in the interface region to absorb the irradiation energy to cause heating and forming the melt region in the interface region.
  • the concentrator element can be made of an acrylic material characterized by a high transmisivity to light.
  • the back cover member can be a polymer having a high emmisivity.
  • the back cover member can be an acrylic material.
  • the back cover member can be a polycarbonate material.
  • the irradiation energy heats the interface region to a temperature of about 110 Degree Celsius to about 115 Degree Celsius to cause the melt region configured to be light absorbing.
  • at least 90% of the energy is transmitted through the first peripheral region of the concentrator member and absorbed by the back cover member to cause the melt region as shown by the relationship:
  • E E C + E B .
  • E the energy provided by the electromagnetic radiation
  • Ec the energy absorbed by the concentrator member in the peripheral region
  • E B the energy absorbed by the back cover member in the peripheral region.
  • E B ranges from 90% to 95% of E, that is 90 % to 95 % of the energy is transmitted through the concentrator member and absorbed by the back cover member to cause the melt region in the peripheral region.
  • E ranges from 90% to 95% of E, that is 90 % to 95 % of the energy is transmitted through the concentrator member and absorbed by the back cover member to cause the melt region in the peripheral region.
  • the melt region forms a seal region 702 for the back cover member and the concentrator member.
  • Figure 7 is a simplified side-view diagram of a concentrator member and a back cover member according to an embodiment of the present invention. This diagram is merely an example, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives.
  • the melt region forms a seal region 702 for the back cover member and the concentrator member. A more detailed diagram of the seal region is also shown.
  • the seal region has a width 704 of about 50 um or less and can include a protruded region 706.
  • the seal region provided is free of contaminations such as particulates or chemical species as may occur by other means.
  • the seal region maintains the photovoltaic strips and electrical conducting element in a desired controlled environment and provides protection from elements such as moisture and others.
  • the irradiation energy causes a temperature gradient within the interface region.
  • acrylic as the material for the concentrator member and polycarbonate as the material for the back cover member as an example.
  • the polycarbonate is designed to be light absorbing and the acrylic is designed to be transmissive.
  • the energy transmitted through the first peripheral region of the concentrator member provides heat energy to increase the temperature of the interface region to about 105 Degree Celsius to about 120 Degree Celsius to cause the melt region.
  • the temperature gradient is provided within a vertical distance in the interface region as illustrated in a simplified plot 800 in Figure 8. As shown, the temperature is provided on vertical axis and the vertical distance is provided on the horizontal axis. The temperature gradient is essentially provided within a vertical distance 701 as shown.
  • the temperature gradient is provided within a vertical distance of about 40 micron to about 50 micron in the vertical direction. That is the thermal energy is provided within vertical distance 801 for a time period to form the melt region in a specific embodiment.
  • the time period is about eight seconds or less and preferably 4-6 seconds in a specific embodiment.

Abstract

A method and system for assembling a solar cell package for a solar panel includes providing a first substrate member comprising a plurality of photovoltaic strips thereon, an optical elastomer material overlying a portion of the first substrate member. A second substrate member comprising a plurality of optical concentrating elements, an aperture surface region and an exit surface region, is aligned with the first substrate such that at least one of the optical concentrating elements is coupled to at least one of the photovoltaic strips. The second substrate member is coupled to the first substrate member to form an interface region along a first peripheral region of the first substrate member and along a second peripheral region of the second substrate member.

Description

METHOD AND SYSTEM FOR ASSEMBLING A SOLAR CELL PACKAGE
CROSS-REFERENCES TO RELATED APPLICATIONS
[0001] This application claims priority to United States Patent Application No. 60/909,691, filed April 02, 2007 and United States Patent Application No. 60/909, 692, filed 02, 2007, both are commonly assigned and herein incorporated by reference for all purposes.
STATEMENT AS TO RIGHTS TO INVENTIONS MADE UNDER FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT [0002] NOT APPLICABLE
REFERENCE TO A "SEQUENCE LISTING," A TABLE, OR A COMPUTER PROGRAM LISTING APPENDIX SUBMITTED ON A COMPACT DISK.
[0003] NOT APPLICABLE
BACKGROUND OF THE INVENTION
[0004] The present invention relates generally to solar energy techniques. In particular, the present invention provides a method and resulting device fabricated from a plurality of concentrating elements respectively coupled to a plurality of photovoltaic regions. For example, concentrating elements are coupled to a plurality of photovoltaic regions using one or more coupled structures. More particularly, the present method and structure are directed to a laser sealing technique of a solar cell package apparatus. Merely by way of example, the invention has been applied to solar panels, commonly termed modules, but it would be recognized that the invention has a much broader range of applicability.
[0005] As the population of the world increases, industrial expansion has lead to an equally large consumption of energy. Energy often comes from fossil fuels, including coal and oil, hydroelectric plants, nuclear sources, and others. As merely an example, the International Energy Agency projects further increases in oil consumption, with developing nations such as China and India accounting for most of the increase. Almost every element of our daily lives depends, in part, on oil, which is becoming increasingly scarce. As time further progresses, an era of "cheap" and plentiful oil is coming to an end. Accordingly, other and alternative sources of energy have been developed.
[0006] Concurrent with oil, we have also relied upon other very useful sources of energy such as hydroelectric, nuclear, and the like to provide our electricity needs. As an example, most of our conventional electricity requirements for home and business use comes from turbines run on coal or other forms of fossil fuel, nuclear power generation plants, and hydroelectric plants, as well as other forms of renewable energy. Often times, home and business use of electrical power has been stable and widespread.
[0007] Most importantly, much if not all of the useful energy found on the Earth comes from our sun. Generally all common plant life on the Earth achieves life using photosynthesis processes from sun light. Fossil fuels such as oil were also developed from biological materials derived from energy associated with the sun. For human beings including "sun worshipers," sunlight has been essential. For life on the planet Earth, the sun has been our most important energy source and fuel for modern day solar energy.
[0008] Solar energy possesses many characteristics that are very desirable! Solar energy is renewable, clean, abundant, and often widespread. Certain technologies developed often capture solar energy, concentrate it, store it, and convert it into other useful forms of energy.
[0009] Solar panels have been developed to convert sunlight into energy. As merely an example, solar thermal panels often convert electromagnetic radiation from the sun into thermal energy for heating homes, running certain industrial processes, or driving high grade turbines to generate electricity. As another example, solar photovoltaic panels convert sunlight directly into electricity for a variety of applications. Solar panels are generally composed of an array of solar cells, which are interconnected to each other. The cells are often arranged in series and/or parallel groups of cells in series. Accordingly, solar panels have great potential to benefit our nation, security, and human users. They can even diversify our energy requirements and reduce the world's dependence on oil and other potentially detrimental sources of energy.
[0010] Although solar panels have been used successful for certain applications, there are still certain limitations. Solar cells are often costly. Depending upon the geographic region, there are often financial subsidies from governmental entities for purchasing solar panels, which often cannot compete with the direct purchase of electricity from public power companies. Additionally, the panels are often composed of silicon bearing wafer materials. Such wafer materials are often costly and difficult to manufacture efficiently on a large scale. Availability of solar panels is also somewhat scarce. That is, solar panels are often difficult to find and purchase from limited sources of photovoltaic silicon bearing materials. These and other limitations are described throughout the present specification, and may be described in more detail below.
[0011] From the above, it is seen that techniques for improving solar devices is highly desirable.
BRIEF SUMMARY OF THE INVENTION
[0012] The present invention relates generally to solar energy techniques. In particular, the present invention provides a method and resulting device fabricated from a plurality of concentrating elements respectively coupled to a plurality of photovoltaic regions. For example, concentrating elements are coupled to a plurality of photovoltaic regions using one or more coupled structures. More particularly, the present method and structure are directed to a laser sealing technique of a solar cell package apparatus. Merely by way of example, the invention has been applied to solar panels, commonly termed modules, but it would be recognized that the invention has a much broader range of applicability.
[0013] In a specific embodiment, the present invention provides a method for fabricating solar cell for a solar panel. The method includes providing a first substrate member comprising a plurality of photovoltaic strips thereon. The method includes providing an optical elastomer material overlying a portion of the first substrate member. In a specific embodiment, the method aligns a second substrate member comprising a plurality of optical concentrating elements thereon such that at least one of the optical concentrating elements is operably coupled to at least one of the plurality of photovoltaic strips. In a specific embodiment, the second substrate member comprises an aperture surface region and an exit surface region. The method couples the first substrate member to the second substrate member to form an interface region along a first peripheral region of the first substrate member and a second peripheral region of the second substrate member. In a specific embodiment, the method includes blocking an inner region of the aperture surface region of the second substrate member while exposing the peripheral region of the aperture surface region of the second substrate member. [0014] According to another embodiment, the present invention provides A method for fabricating a solar cell free and separate from a solar panel. The method includes providing a first substrate member comprising a plurality of photovoltaic strips thereon, the first substrate member having a first peripheral region, the first peripheral region including a first flat region and a first structure region, the first structure region including a protruding structure. The method also includes providing an optical elastomer material overlying a portion of the first substrate member. Furthermore, the method includes providing a second substrate member having a second peripheral region, the second peripheral region including a second flat region and a second structure region, the second structure region including an indent structure. Additionally, the method includes aligning the second substrate member comprising a plurality of optical concentrating elements thereon such that the first flat region of the first substrate mates with the second flat region of the second substrate and the first structure region, the second substrate member comprising an aperture surface region and an exit surface region. The method also includes coupling the first substrate member to the second substrate member to form a sealing region between the first peripheral region of the first substrate member and the second peripheral region of the second substrate member and to engage the first structure region of the first substrate to the second structure region of the second substrate.
[0015] According to yet another embodiment, the present invention provides a solar cell package. The package includes a first substrate member comprising a plurality of photovoltaic strips thereon, the first substrate member having a first peripheral region, the first peripheral region including a first flat region and a first structure region, the first structure region comprising an protruding structure. The package also includes an optical elastomer material overlying a portion of the first substrate member. The package also includes a second substrate member having a second peripheral region, the second peripheral region including a second flat region and a second structure region, the second substrate being aligned such that the first flat region of the first substrate mates with the second flat region of the second substrate and the first structure region, the second substrate member comprising an aperture surface region and an exit surface region, the second structure region comprising an indent structure.
[0016] In a specific embodiment, the method also irradiates an entirety of the second peripheral region of the second substrate member using electromagnetic radiation to seal the interface region between the second substrate and the first substrate. In a preferred embodiment, the blocking selectively allows for irradiation of the second peripheral region of the second substrate member to seal the interface region. In an alternative embodiment, irradiating an entirety of the second peripheral region of the second substrate member uses a flash or pulses of electromagnetic radiation to seal the interface region between the second substrate and the first substrate, while the inner region of the aperture surface region remains blocked using blocking material.
[0017] In an alternative embodiment, the invention provides a system for manufacture of solar cells. In a specific embodiment, the apparatus has a stage member, which can be a mechanical attachment member, vacuum member, or other suitable device. The apparatus has a first substrate member comprising a plurality of photovoltaic regions thereon provided on the stage member, an optical elastomer material overlying a portion of the first substrate member, an aligned second substrate member comprising a plurality of optical concentrating elements thereon such that at least one of the optical concentrating elements being operably coupled to at least one of the plurality of photovoltaic strips, the second substrate member comprising an aperture surface region and an exit surface region, and an interface region provided along a first peripheral region of the first substrate member and a second peripheral region of the second substrate member. In a preferred embodiment, a blocking member is provided within an inner region of the aperture surface region of the second substrate member while exposing the peripheral region of the aperture surface region of the second substrate member. The apparatus also has an irradiation source coupled to the stage member. In a specific embodiment, the irradiation source is adapted to irradiate an entirety of the second peripheral region of the second substrate member using a flash or pulses of electromagnetic radiation to seal the interface region between the second substrate and the first substrate, while the inner region of the aperture surface region remains blocked using blocking material.
[0018] Many benefits are achieved by way of the present invention over conventional techniques. For example, the present technique provides an easy to use process that relies upon conventional technology such as silicon materials, although other materials can also be used. Additionally, the method provides a process that is compatible with conventional process technology without substantial modifications to conventional equipment and processes. Preferably, the invention provides for an improved solar cell, which is less costly and easy to handle. Such solar cell uses a plurality of photovoltaic regions, which are sealed within one or more substrate structures according to a preferred embodiment. In a preferred embodiment, the invention provides a method and completed solar cell structure using a plurality of photovoltaic strips free and clear from a module or panel assembly, which are provided during a later assembly process. Also in a preferred embodiment, one or more of the solar cells have less silicon per area (e.g., 80% or less, 50% or less) than conventional solar cells. In preferred embodiments, the present method and cell structures are also light weight and not detrimental to building structures and the like. That is, the weight is about the same or slightly more than conventional solar cells at a module level according to a specific embodiment. In a preferred embodiment, the present solar cell using the plurality of photovoltaic strips can be used as a "drop in" replacement of conventional solar cell structures. As a drop in replacement, the present solar cell can be used with conventional solar cell technologies for efficient implementation according to a preferred embodiment. In a preferred embodiment, the present method and system provide a way of sealing an interface region between two substrate members using an electromagnetic radiation source, which is relatively easy to use and cost effective. Depending upon the embodiment, one or more of these benefits may be achieved. These and other benefits will be described in more detail throughout the present specification and more particularly below.
[0019] Various additional objects, features and advantages of the present invention can be more fully appreciated with reference to the detailed description and accompanying drawings that follow.
BRIEF DESCRIPTION OF THE DRAWINGS
[0020] Figure 1 is a simplified diagram of a solar cell according to an embodiment of the present invention;
[0021] Figure 2 is a simplified diagram of solar cell concentrating elements according to an embodiment of the present invention;
[0022] Figure 2A is a simplified side-view diagram of solar cell concentrating elements according to an embodiment of the present invention;
[0023] Figures 3, 3A, and 3B are simplified flow diagrams illustrating a method of assembling a solar cell apparatus according to an embodiment of the present invention;
[0024] Figure 4 is a simplified diagram of coupling a back cover member to a concentrator member according to an embodiment of the present invention;
[0025] Figures 5 and 5A are a simplified diagrams of irradiating peripheral regions of the concentrator member and back cover member to seal them together according to an embodiment of the present invention; [0026] Figure 6 is a simplified side-view diagram of a concentrator member and a back cover according to an embodiment of the present invention;
[0027] Figure 7 is a more detailed diagram of a back cover device and a concentrator device according to an embodiment of the present invention; and
[0028] Figure 8 is a simplified plot of temperature gradient in z direction in the seal region according to an embodiment of the present invention.
DETAILED DESCRIPTION OF THE INVENTION [0029] The present invention relates generally to solar energy techniques. In particular, the present invention provides a method and resulting device fabricated from a plurality of concentrating elements respectively coupled to a plurality of photovoltaic regions. For example, concentrating elements are coupled to a plurality of photovoltaic regions using one or more coupled structures. More particularly, the present method and structure are directed to a laser sealing technique of a solar cell package apparatus. Merely by way of example, the invention has been applied to solar panels, commonly termed modules, but it would be recognized that the invention has a much broader range of applicability.
[0030] Figure 1 is a simplified diagram of a solar cell according to an embodiment of the present invention. This diagram is merely an example, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives. As shown is an expanded view of the present solar cell device structure, which includes various elements. The device has a back cover member 101, which includes a surface area and a back area. The back cover member also has a plurality of sites, which are spatially disposed, for electrical members, such as bus bars, and a plurality of photovoltaic regions. Alternatively, the back cover can be free from any patterns and is merely provided for support and packaging. Of course, there can be other variations, modifications, and alternatives.
[0031] In a preferred embodiment, the device has a plurality of photovoltaic strips 105, each of which is disposed overlying the surface area of the back cover member. In a preferred embodiment, the plurality of photovoltaic strips corresponds to a cumulative area occupying a total photovoltaic spatial region, which is active and converts sunlight into electrical energy. [0032] An encapsulating material 115 is overlying a portion of the back cover member. That is, an encapsulating material forms overlying the plurality of strips, and exposed regions of the back cover, and electrical members. In a preferred embodiment, the encapsulating material can be a single layer, multiple layers, or portions of layers, depending upon the application. In alternative embodiments, as noted, the encapsulating material can be provided overlying a portion of the photovoltaic strips or a surface region of the front cover member, which would be coupled to the plurality of photovoltaic strips. Of course, there can be other variations, modifications, and alternatives.
[0033] In a specific embodiment, a front cover member 121 is coupled to the encapsulating material. That is, the front cover member is formed overlying the encapsulant to form a multilayered structure including at least the back cover, bus bars, plurality of photovoltaic strips, encapsulant, and front cover. In a preferred embodiment, the front cover includes one or more concentrating elements, which concentrate (e.g., intensify per unit area) sunlight onto the plurality of photovoltaic strips. That is, each of the concentrating elements can be associated respectively with each of or at least one of the photovoltaic strips.
[0034] Upon assembly of the back cover, bus bars, photovoltaic strips, encapsulant, and front cover, an interface region is provided along at least a peripheral region of the back cover member and the front cover member. The interface region may also be provided surrounding each of the strips or certain groups of the strips depending upon the embodiment. The device has a sealed region and is formed on at least the interface region to form an individual solar cell from the back cover member and the front cover member. The sealed region maintains the active regions, including photovoltaic strips, in a controlled environment free from external effects, such as weather, mechanical handling, environmental conditions, and other influences that may degrade the quality of the solar cell. Additionally, the sealed region and/or sealed member (e.g., two substrates) protect certain optical characteristics associated with the solar cell and also protects and maintains any of the electrical conductive members, such as bus bars, interconnects, and the like. Of course, there can be other benefits achieved using the sealed member structure according to other embodiments.
[0035] In a preferred embodiment, the total photovoltaic spatial region occupies a smaller spatial region than the surface area of the back cover. That is, the total photovoltaic spatial region uses less silicon than conventional solar cells for a given solar cell size. In a preferred embodiment, the total photovoltaic spatial region occupies about 80% and less of the surface area of the back cover for the individual solar cell. Depending upon the embodiment, the photovoltaic spatial region may also occupy about 70% and less or 60% and less or preferably 50% and less of the surface area of the back cover or given area of a solar cell. Of course, there can be other percentages that have not been expressly recited according to other embodiments. Here, the terms "back cover member" and "front cover member" are provided for illustrative purposes, and not intended to limit the scope of the claims to a particular configuration relative to a spatial orientation according to a specific embodiment. Further details of each of the various elements in the solar cell can be found throughout the present specification and more particularly below.
[0036] In a specific embodiment, the present invention provides a packaged solar cell assembly being capable of stand-alone operation to generate power using the packaged solar cell assembly and/or with other solar cell assemblies. The packaged solar cell assembly includes rigid front cover member having a front cover surface area and a plurality of concentrating elements thereon. Depending upon applications, the rigid front cover member consists of a variety of materials. For example, the rigid front cover is made of polymer material. As another example, the rigid front cover is made of transparent polymer material having a reflective index of about 1.4 or 1.42 or greater. According to an example, the rigid front cover has a Young's Modulus of a suitable range. Each of the concentrating elements has a length extending from a first portion of the front cover surface area to a second portion of the front cover surface area. Each of the concentrating elements has a width provided between the first portion and the second portion. Each of the concentrating elements having a first edge region coupled to a first side of the width and a second edge region provided on a second side of the width. The first edge region and the second edge region extend from the first portion of the front cover surface area to a second portion of the front cover surface area. The plurality of concentrating elements is configured in a parallel manner extending from the first portion to the second portion.
[0037] It is to be appreciated that embodiment can have many variations. For example, the embodiment may further includes a first electrode member that is coupled to a first region of each of the plurality of photovoltaic strips and a second electrode member coupled to a second region of each of the plurality of photovoltaic strips.
[0038] As another example, the solar cell assembly additionally includes a first electrode member coupled to a first region of each of the plurality of photovoltaic strips and a second electrode member coupled to a second region of each of the plurality of photovoltaic strips. The first electrode includes a first protruding portion extending from a first portion of the sandwiched assembly and the second electrode comprising a second protruding portion extending from a second portion of the sandwiched assembly.
[0039] In yet another specific embodiment, the present invention provides a solar cell apparatus. The solar cell apparatus includes a backside substrate member comprising a backside surface region and an inner surface region. Depending upon application, the backside substrate member can be made from various materials. For example, the backside member is characterized by a polymer material.
[0040] In yet another embodiment, the present invention provides a solar cell apparatus that includes a backside substrate member. The backside substrate member includes a backside surface region and an inner surface region. The backside substrate member is characterized by a width. For example, the backside substrate member is characterized by a length of about eight inches and less. As an example, the backside substrate member is characterized by a width of about 8 inches and less and a length of more than 8 inches. Of course, there can be other variations, modifications, and alternatives. Further details of the solar cell assembly can be found in U.S. Patent Application 11/445,993 (Attorney Docket No.: 025902-000210US), commonly assigned, and hereby incorporated by reference herein.
[0041] Figure 2 is a simplified diagram of solar cell concentrating elements 201 according to an embodiment of the present invention. This diagram is merely an example, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives. As shown, each of the concentrating elements for the strip configuration includes a trapezoidal shaped member 205. Each of the trapezoidal shaped members has a bottom surface 203 coupled to a pyramidal shaped region coupled to an upper region 207. The upper region is defined by surface 209, which is co-extensive of the front cover. Each of the members is spatially disposed and in parallel to each other according to a specific embodiment. Here, the term "trapezoidal" or "pyramidal" may include embodiments with straight or curved or a combination of straight and curved walls according to embodiments of the present invention. Depending upon the embodiment, the concentrating elements may be on the front cover, integrated into the front cover, and/or be coupled to the front cover according to embodiments of the present invention. Further details of the front cover with concentrating elements are provided more particularly below. [0042] In a specific embodiment, a solar cell apparatus includes a shaped concentrator device operably coupled to each of the plurality of photovoltaic strips. The shaped concentrator device has a first side and a second side. In addition, the solar cell apparatus includes an aperture region provided on the first side of the shaped concentrator device. As merely an example, the concentrator device includes a first side region and a second side region.
Depending upon application, the first side region is characterized by a roughness of about 100 nanometers or 120 nanometers RMS and less, and the second side region is characterized by a roughness of about 100 nanometers or 120 nanometers RMS and less. For example, the roughness is characterized by a dimension value of about 10% of a light wavelength derived from the aperture regions. Depending upon applications, the backside member can have a pyramid-type shape.
[0043] As an example, the solar cell apparatus includes an exit region provided on the second side of the shaped concentrator device. In addition, the solar cell apparatus includes a geometric concentration characteristic provided by a ratio of the aperture region to the exit region. The ratio can be characterized by a range from about 1.8 to about 4.5. The solar cell apparatus also includes a polymer material characterizing the shaped concentrator device. The solar cell apparatus additionally includes a refractive index of about 1.45 and greater characterizing the polymer material of the shaped concentrator device. Additionally, the solar cell apparatus includes a coupling material formed overlying each of the plurality of photovoltaic strips and coupling each of the plurality of photovoltaic regions to each of the concentrator devices. For example, the coupling material is characterized by a suitable Young's Modulus.
[0044] As merely an example, the solar cell apparatus includes a refractive index of about 1.45 and greater characterizing the coupling material coupling each of the plurality of photovoltaic regions to each of the concentrator device. Depending upon application, the polymer material is characterized by a thermal expansion constant that is suitable to withstand changes due to thermal expansion of elements of the solar cell apparatus.
[0045] For certain applications, the plurality of concentrating elements has a light entrance area (Al) and a light exit area (A2) such that A2/A1 is 0.8 and less. As merely an example, the plurality of concentrating elements has a light entrance area (Al) and a light exit area (A2) such that A2/A1 is 0.8 and less, and the plurality of photovoltaic strips are coupled against the light exit area. In a preferred embodiment, the ratio of A2/A1 is about 0.5 and less. For example, each of the concentrating elements has a height of 7mm or less. In a specific embodiment, the sealed sandwiched assembly has a width ranging from about 100 millimeters to about 210 millimeters and a length ranging from about 100 millimeters to about 210 millimeters. In a specific embodiment, the sealed sandwiched assembly can even have a length of about 300 millimeters and greater. As another example, each of the concentrating elements has a pair of sides. In a specific embodiment, each of the sides has a surface finish of 100 nanometers or less or 120 nanometers and less RMS. Of course, there can be other variations, modifications, and alternatives.
[0046] Referring now to Figure 2A, the front cover has been illustrated using a side view 201, which is similar to Figure 2. The front cover also has a top-view illustration 210. A section view 220 from "B-B" has also been illustrated. A detailed view "A" of at least two of the concentrating elements 230 is also shown. Depending upon the embodiment, there can be other variations, modifications, and alternatives.
[0047] Depending upon the embodiment, the concentrating elements are made of a suitable material. The concentrating elements can be made of a polymer, glass, or other optically transparent materials, including any combination of these, and the like. The suitable material is preferably environmentally stable and can withstand environmental temperatures, weather, and other "outdoor" conditions. The concentrating elements can also include portions that are coated with an anti-reflective coating for improved efficiency. Coatings can also be used for improving a durability of the concentrating elements. Of course, there can be other variations, modifications, and alternatives.
[0048] In a specific embodiment, the solar cell apparatus includes a first reflective side provided between a first portion of the aperture region and a first portion of the exit region. As merely an example, the first reflective side includes a first polished surface of a portion of the polymer material. For certain applications, the first reflective side is characterized by a surface roughness of about 120 nanometers RMS and less.
[0049] Moreover, the solar cell apparatus includes a second reflective side provided between a second portion of the aperture region and a second portion of the exit region. For example, the second reflective side comprises a second polished surface of a portion of the polymer material. For certain applications, the second reflective side is characterized by a surface roughness of about 120 nanometers and less. As an example, the first reflective side and the second reflective side provide for total internal reflection of one or more photons provided from the aperture region.
[0050] In addition, the solar cell apparatus includes a geometric concentration characteristic provided by a ratio of the aperture region to the exit region. The ratio is characterized by a range from about 1.8 to about 4.5. Additionally, the solar cell apparatus includes a polymer material characterizing the shaped concentrator device, which includes the aperture region, exit region, first reflective side, and second reflective side. As an example, the polymer material is capable of being free from damaged caused by ultraviolet radiation.
[0051] Furthermore, the solar cell apparatus has a refractive index of about 1.45 and greater characterizing the polymer material of the shaped concentrator device. Moreover, the solar cell apparatus includes a coupling material formed overlying each of the plurality of photovoltaic strips and coupling each of the plurality of photovoltaic regions to each of the concentrator devices. The solar cell apparatus additionally includes one or more pocket regions facing each of the first reflective side and the second reflective side. The one or more pocket regions can be characterized by a refractive index of about 1 to cause one or more photons from the aperture region to be reflected toward the exit region. To maintain good efficiency of the subject concentrator devices, each of the concentrating elements is separated by a region having a notch structure of a predetermined size and shape according to a specific embodiment. Of course there can be other variations, modifications, and alternatives. Further details of the notch structures can be found throughout the present specification and more particularly below.
[0052] Figure 3 is a simplified flow diagram illustrating a method of assembling a solar cell apparatus according to an embodiment of the present invention. This diagram is merely an example, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives. As shown, the method provides a first substrate member (Step 302). The first substrate member includes a plurality of photovoltaic strips thereon. The method provides a second substrate member (Step 304) which includes a plurality of optical concentrating elements. The first substrate member is aligned and couple to the second substrate member (Step 306). In a specific embodiment, an inner region of the second substrate member (Step 308) is blocked from irradiation while a peripheral region remained exposed (Step 310). A pressure is applied (Step 314). The method includes irradiating the exposed peripheral region of the second substrate member (Step 312) and forming a melting region in an interface region between the first substrate member and the second substrate member. The melting region is used to seal peripheral interface between first substrate and second substrate (Step 316). The method continues with other steps (Step 318) to complete the solar cell panel.
[0053] The above sequence of steps provide a method for assembling a solar cell panel according to an embodiment of the present invention. Alternatively, one or more of the steps may be performed, one or more steps may be eliminated, or one or more steps may be performed in a different sequence depending on the embodiment. One skilled in the art would recognize many other variations, modifications, and alternatives.
[0054] Figure 3 A is a simplified flow diagram illustrating a method of assembling a solar cell apparatus according to an embodiment of the present invention. This diagram is merely an example, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives. As shown, the method provides a first substrate member (Step 302). The first substrate member includes a plurality of photovoltaic strips thereon. The method provides a second substrate member (Step 304) which includes a plurality of optical concentrating elements. The method also includes providing a high emissivity back cover device (Step 305). The first substrate member is aligned and couple to the second substrate member (Step 306). In a specific embodiment, an inner region of the second substrate member (Step 308) is blocked from irradiation while a peripheral region remained exposed (Step 310). A pressure is applied (Step 314). The method includes irradiating the exposed peripheral region of the second substrate member (Step 312) and forming a melting region in an interface region between the first substrate member and the second substrate member. As an example, laser is used for providing irradiation. The melting region is used to seal peripheral interface between first substrate and second substrate (Step 316). The method continues with other steps (Step 318) to complete the solar cell panel.
[0055] The above sequence of steps provide a method for assembling a solar cell panel according to an embodiment of the present invention. Alternatively, one or more of the steps may be performed, one or more steps may be eliminated, or one or more steps may be performed in a different sequence depending on the embodiment. One skilled in the art would recognize many other variations, modifications, and alternatives.
[0056] Figure 3B is a simplified flow diagram illustrating a method of assembling a solar cell apparatus according to an embodiment of the present invention. This diagram is merely an example, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives. As shown, the method provides a first substrate member (Step 302). The first substrate member includes a plurality of photovoltaic strips thereon. The method provides a second substrate member (Step 304) which includes a plurality of optical concentrating elements. The method also includes providing a high emissivity back cover device (Step 305). The first substrate member is aligned and couple to the second substrate member (Step 306). A pressure is applied (Step 308). In a specific embodiment, an inner region of the second substrate member (Step 310) is blocked from irradiation while a peripheral region remained exposed (Step 312). The method includes irradiating the exposed peripheral region of the second substrate member (Step 314) and forming a melting region in an interface region between the first substrate member and the second substrate member. The melting region is used to seal peripheral interface between first substrate and second substrate (Step 316). The method continues with other steps (Step 318) to complete the solar cell panel.
[0057] The above sequence of steps provide a method for assembling a solar cell panel according to an embodiment of the present invention. Alternatively, one or more of the steps may be performed, one or more steps may be eliminated, or one or more steps may be performed in a different sequence depending on the embodiment. One skilled in the art would recognize many other variations, modifications, and alternatives.
[0058] Figure 4 is a simplified diagram of coupling 400 a back cover member 401 to a concentrator member 402 according to an embodiment of the present invention. This diagram is merely an example, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives. As shown in Figure 4, the back cover member 401 includes, a first peripheral region 404, which has a protruding structure 406 and a first flat region in a portion of the first peripheral region. Also shown in Figure 4, the concentrator member includes a second peripheral region 408, which has an indent structure 410 and a second flat region in a portion of the second peripheral region. In a specific embodiment, the protruding structure and the indent structure provides a tongue and groove mechanism to couple the back cover member and the concentrator member. Additionally, the back cover member and the concentrator member may be aligned using the tongue and groove mechanism in a specific embodiment, the protruding structure 406 of the back cover member is aligned to a second peripheral region 408 of the concentrator member such that each of the plurality of photovoltaic strips is coupled to a concentrator element in the concentrator member. As shown in Figure 4, the coupled substrate member includes an interface region 412 formed from the first peripheral region and the second peripheral region. In a specific embodiment, the protruding structure 410 has a semi-circular cross section. For example, the protruding structure 410 has a diameter of about 10/1000 of an inch or less and runs along the second peripheral region of the concentrator member. Alternatively, the protruding structure can be any shape, for example, the cross section can be rectangular, or other polygon shapes. The indent structure can be shaped accordingly to mate with the protruding structure. Of course there can be other variations, modifications, and alternatives.
[0059] Optionally, before coupling, the interface region may be subjected to a cleaning process to remove any material that may affect sealing of the substrate members. The cleaning process can include using a suitable solvents or a combination of solvents followed by drying. Alternatively the cleaning process may include a plasma cleaning, or a blasting process to remove undesirable material. Of course there can be other variations, modifications, and alternatives.
[0060] In a specific embodiment, after aligning the concentrator member to the back cover member, a force is provided to mechanically couple the aligned concentrator member to the back cover member. The force may be provided by a plate, fluid pressure, a clamp or any other suitable techniques. Further details of the applied force can be found through the present specification and particularly below. Of course there can be other variations, modifications, and alternatives.
[0061] Figure 5-7 are simplified diagrams of joining the concentrator member and back cover member and to seal them together using an electromagnetic radiation according to an embodiment of the present invention. These diagrams are merely examples, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives. As shown in Figure 5, a stage member including a waveguide device 504 is provided. The waveguide device includes an inner waveguide 506, an outer waveguide 508, and an opening region 510. The waveguide device also includes an upper surface region 512 and a back surface region 514. In a specific embodiment, the electromagnetic radiation is allowed to pass through the opening region of the waveguide device and blocked by the inner waveguide region and the outer waveguide region. In a specific embodiment, the opening region includes a straight face region 518 and an oblique face region 520. In a specific embodiment, the straight face region may be a flat surface. The straight face region may also be a curved surface that is concave or convex depending on the application. In a specific embodiment, the oblique face region may be a flat surface. Alternatively, the oblique face region may be a curved surface depending upon the application. The oblique face region and the straight face region allow for a maximum transmission of the electromagnetic radiation through the opening region. The waveguide device is preferably made of a highly reflective material at least in the straight face region and the oblique face region. In a specific embodiment, the waveguide device is made of a gold plated alloy. For example, the alloy may be steel and/or other metal materials. The waveguide device is configured to allow for a concentration of the electromagnetic radiation to concentrate at a weld region 516 in the peripheral region in a specific embodiment. A top view of the waveguide device is shown in Figure 5A. Of cause there can be other variations, modifications, and alternatives.
[0062] In a specific embodiment, the waveguide device is provided overlying the aperture region of the concentrator member. In a specific embodiment, a force 522 is applied on the front surface region of the waveguide device to mechanically couple the concentrator member to the back cover member to form the peripheral region as also shown in Figure 5. In a specific embodiment, the mechanical force can be provided using air pressure or a weight such as a cylinder providing a pressure ranging from about 100 psi to about 200 psi. Other means of mechanical forces, such as an air pressure, may also be used. Of course there can be other variations, modifications, and alternatives.
[0063] Referring to Figure 6, the coupled concentrator member and the back cover member is irradiated using an electromagnetic radiation 602. The electromagnetic radiation may be provided using a energy source such as a laser source or a flash lamp or other suitable energy source. In a specific embodiment, the electromagnetic radiation may be provided using a laser (e.g., laser diode, tunable dye, etc.) having a suitable wavelength range and providing a suitable power range. In a preferred embodiment, the electromagnetic radiation is provided for a time period of about eight seconds or less and preferably 1-4 seconds. Effectively, the electromagnetic radiation traverses through the entire exposed peripheral region of at least the concentrator member of the coupled substrate within the entire time period and provides energy to cause a melt region 608 in the interface region while the inner region is blocked from the electromagnetic radiation.
[0064] In a specific embodiment, the electromagnetic radiation and/or laser energy is guided using one or more fiber optics 606 from a source 604 and through the opening region of the waveguide device to the peripheral region of the coupled substrate to provide energy to cause the melt region in the peripheral region. For example, the source 604 is a laser source.
The laser source provides pulses of energy and the one or more fiber optics are allowed to translate above the opening region of the waveguide device to provide energy to cause the melt region in the interface region of the coupled substrate members in a specific embodiment. As merely an example, the electromagnetic radiation can be derived from Laser IRAM assembly systems Models 200 and 300 manufactured by Branson Ultrasonics Corp., 41 Eagle Rd., Danbury, CT 06813-1961, USA. Of course there can be other variations, modifications, and alternatives.
[0065] In a specific embodiment, the light/laser radiation traverses through the entire thickness of the concentrator member, which can be a polymer component transmissive to light. The energy is absorbed at least by the back cover member at the interface region to cause a melt region 608 in the interface region. In a specific embodiment, the back cover member is made of a light absorbing material at least in the second peripheral region. The light absorbing material absorbs irradiation energy traversing at least the first peripheral region of the concentrator element, which is transparent, to cause heating and to form the melting region in the interface region. In a specific embodiment, the light absorbing material can also be a light blocking material or include each of these characteristics. In an alternative embodiment, the light absorbing material may be provided in the interface region to absorb the irradiation energy to cause heating and forming the melt region in the interface region. In a specific embodiment, the concentrator element can be made of an acrylic material characterized by a high transmisivity to light. In a specific embodiment, the back cover member can be a polymer having a high emmisivity. As merely an example, the back cover member can be an acrylic material. Alternatively, the back cover member can be a polycarbonate material. In the example of an acrylic concentrator element and a polycarbonate back cover, the irradiation energy heats the interface region to a temperature of about 110 Degree Celsius to about 115 Degree Celsius to cause the melt region configured to be light absorbing. In a specific embodiment at least 90% of the energy is transmitted through the first peripheral region of the concentrator member and absorbed by the back cover member to cause the melt region as shown by the relationship:
E =EC + EB. where E is the energy provided by the electromagnetic radiation, Ec is the energy absorbed by the concentrator member in the peripheral region, and EB is the energy absorbed by the back cover member in the peripheral region.
[0066] As shown, EB ranges from 90% to 95% of E, that is 90 % to 95 % of the energy is transmitted through the concentrator member and absorbed by the back cover member to cause the melt region in the peripheral region. Of course there can be other variations, modifications, and alternatives.
[0067] In a specific embodiment, the melt region forms a seal region 702 for the back cover member and the concentrator member. Figure 7 is a simplified side-view diagram of a concentrator member and a back cover member according to an embodiment of the present invention. This diagram is merely an example, which should not unduly limit the scope of the claims herein. One of ordinary skill in the art would recognize other variations, modifications, and alternatives. In a specific embodiment, the melt region forms a seal region 702 for the back cover member and the concentrator member. A more detailed diagram of the seal region is also shown. In a specific embodiment, the seal region has a width 704 of about 50 um or less and can include a protruded region 706. In a specific embodiment, the seal region provided is free of contaminations such as particulates or chemical species as may occur by other means. The seal region maintains the photovoltaic strips and electrical conducting element in a desired controlled environment and provides protection from elements such as moisture and others. Of course there can be other variations, modifications, and alternatives.
[0068] Effectively, the irradiation energy causes a temperature gradient within the interface region. Taking acrylic as the material for the concentrator member and polycarbonate as the material for the back cover member as an example. The polycarbonate is designed to be light absorbing and the acrylic is designed to be transmissive. The energy transmitted through the first peripheral region of the concentrator member provides heat energy to increase the temperature of the interface region to about 105 Degree Celsius to about 120 Degree Celsius to cause the melt region. In a specific embodiment, the temperature gradient is provided within a vertical distance in the interface region as illustrated in a simplified plot 800 in Figure 8. As shown, the temperature is provided on vertical axis and the vertical distance is provided on the horizontal axis. The temperature gradient is essentially provided within a vertical distance 701 as shown. In a specific embodiment, the temperature gradient is provided within a vertical distance of about 40 micron to about 50 micron in the vertical direction. That is the thermal energy is provided within vertical distance 801 for a time period to form the melt region in a specific embodiment. The time period is about eight seconds or less and preferably 4-6 seconds in a specific embodiment. Of course there can be other variations, modifications, and alternatives.
[0069] It is also understood that the examples and embodiments described herein are for illustrative purposes only and that various modifications or changes in light thereof will be suggested to persons skilled in the art and are to be included within the spirit and purview of this application and scope of the appended claims.

Claims

WHAT IS CLAIMED IS:
L A method for fabricating solar cells for a solar panel, the method comprising: providing a first substrate member comprising a plurality of photovoltaic strips thereon; providing an optical elastomer material overlying a portion of the first substrate member; aligning a second substrate member comprising a plurality of optical concentrating elements thereon such that at least one of the optical concentrating elements being operably coupled to at least one of the plurality of photovoltaic strips, the second substrate member comprising an aperture surface region and an exit surface region; coupling the first substrate member to the second substrate member to form an interface region along a first peripheral region of the first substrate member and along a second peripheral region of the second substrate member; blocking an inner region of the aperture surface region of the second substrate member while exposing the peripheral region of the aperture surface region of the second substrate member; and irradiating an entirety of the second peripheral region of the second substrate member using an electromagnetic radiation to cause a melt region and seal the interface region between the second substrate and the first substrate.
2. The method of claim 1 wherein the coupling further comprises applying a mechanical force to increase pressure at the interface region between the first substrate and the second substrate to maintain the first substrate member and the second substrate member mated together during irradiating.
3. The method of claim 1 wherein the irradiation provides a temperature gradient in a vertical distance of less than 50 um within the interface region.
4. The method of claim 2 wherein the mechanical force provides a pressure of about 150 psi and greater.
5. The method of claim 1 wherein each of the solar cells is provided in a panel.
6. The method of claim 1 wherein the second substrate member is optically transparent.
7. The method of claim 1 wherein the electromagnetic radiation comprises a flash lamp or a laser source.
8. The method of claim 1 wherein the irradiating is provided at a time period of eight seconds and less.
9. The method of claim 1 further comprising cleaning the interface region before coupling the first substrate member to the second substrate member.
10. The method of claim 1 wherein the interface region has one or more voids of a dimension of 1/1000 of an inch or less before the irradiating.
11. The method of claim 1 wherein the first substrate member comprises a polymer bearing material, a non-conductive material, or a multi-layer material.
12. The method of claim 1 wherein the electromagnetic irradiation traverses through an entirety of the second peripheral region to cause the melt region at the interface region to cause sealing of the interface region between the first substrate member and the second substrate member.
13. A method for fabricating a solar cell free and separate from a solar panel, the method comprising: providing a first substrate member comprising a plurality of photovoltaic strips thereon, the first substrate member having a first peripheral region, the first peripheral region including a first flat region and a first structure region, the first structure region including a protruding structure; providing an optical elastomer material overlying a portion of the first substrate member; providing a second substrate member having a second peripheral region, the second peripheral region including a second flat region and a second structure region, the second structure region including an indent structure; aligning the second substrate member comprising a plurality of optical concentrating elements thereon such that the first flat region of the first substrate mates with the second flat region of the second substrate and the first structure region, the second substrate member comprising an aperture surface region and an exit surface region; and coupling the first substrate member to the second substrate member to form a sealing region between the first peripheral region of the first substrate member and the second peripheral region of the second substrate member and to engage the first structure region of the first substrate to the second structure region of the second substrate.
14. The method of claim 13 wherein the protruding structure is mated to the indent structure using a tongue and groove mechanism.
15. The method of claim 13 wherein the plurality of photovoltaic strips are provided within respective plurality of recessed regions on the first substrate member.
16. The method of claim 13 wherein the first substrate member comprises a polymer bearing material, a non-conductive material, or a multilayered material.
17. The method of claim 13 wherein each of the photovoltaic strips comprises a silicon bearing material.
18. The method of claim 13 wherein the first substrate member is characterized by a high emissivity at least in the first peripheral region.
19. The method of claim 13 wherein the coupling comprises irradiating an entirety of the second peripheral region of the second substrate member.
20. The method of claim 13 wherein the electromagnetic radiation comprises a flash lamp or a laser source.
21. The method of claim 13 wherein the electromagnetic radiation is substantially absorbed by the first substrate member in the interface region to cause the melt region.
22. The method of claim 13 wherein the first flat region and the first structure has a length of about 30 microns to about 100 microns and the second flat region and the second structure has a length of about 30 microns to about 100 microns.
23. The method of claim 13 wherein the coupling comprises applying a mechanical force to increase pressure at the interface region between the first substrate and the second substrate to maintain the first substrate member and the second substrate member mated together during irradiating.
24. The method of claim 23 wherein the mechanical force provides a pressure of about 150 psi and greater.
25. A solar cell package comprising: a first substrate member comprising a plurality of photovoltaic strips thereon, the first substrate member having a first peripheral region, the first peripheral region including a first flat region and a first structure region, the first structure region comprising an protruding structure; an optical elastomer material overlying a portion of the first substrate member; and a second substrate member having a second peripheral region, the second peripheral region including a second flat region and a second structure region, the second substrate being aligned such that the first flat region of the first substrate mates with the second flat region of the second substrate and the first structure region, the second substrate member comprising an aperture surface region and an exit surface region, the second structure region comprising an indent structure.
26. The solar cell package of claim 25 further comprising a sealed region between the first peripheral region of the first substrate member and the second peripheral region of the second substrate member to engage the first structure region of the first substrate to the second structure region of the second substrate.
27. The solar cell package of claim 25 wherein the seal region is provided using an electromagnetic radiation, the electromagnetic radiation is selected from a flash lamp and a laser source.
28. The solar cell package of claim 25 wherein the protruding structure and the indent structure are mated together using a tongue and groove mechanism.
29. A system for manufacture of solar cells, the system comprising: a stage member; a first substrate member comprising a plurality of photovoltaic regions thereon provided on the stage member, an optical elastomer material overlying a portion of the first substrate member, an aligned second substrate member comprising a plurality of optical concentrating elements thereon such that at least one of the optical concentrating elements being operably coupled to at least one of the plurality of photovoltaic strips, the second substrate member comprising an aperture surface region and an exit surface region, and an interface region provided along a first peripheral region of the first substrate member and a second peripheral region of the second substrate member; a blocking member provided within an inner region of the aperture surface region of the second substrate member while exposing the peripheral region of the aperture surface region of the second substrate member; a cylinder member provided on the blocking member to provide pressure at the interface region and mechanically couple the substrate members together; and an irradiation source coupled to the stage member, the irradiation source being adapted to irradiate an entirety of the second peripheral region of the second substrate member using a flash or pulses of electromagnetic radiation to seal the interface region between the second substrate and the first substrate, while the inner region of the aperture surface region remains blocked using blocking material.
30. The system of claim 29 wherein the blocking member comprises a waveguide device, the waveguide device comprising: an inner block to block the inner region of the aperture surface region from the electromagnetic radiation; an opening to allow electromagnetic radiation to pass through and irradiate the second peripheral region of the second substrate member, the opening having a straight face region and an oblique face region to allow the electromagnetic radiation to concentrate on the interface region.
31. The system of claim 29 wherein the waveguide device is made of a highly reflective material at least for the straight face region and the oblique face region to maximize transmission of the electromagnetic radiation through the opening.
32. The system of claim 29 wherein the highly reflective material is gold plated steel alloy.
PCT/US2008/059167 2007-04-02 2008-04-02 Method and system for assembling a solar cell package WO2008122046A2 (en)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
US90969207P 2007-04-02 2007-04-02
US90969107P 2007-04-02 2007-04-02
US60/909,691 2007-04-02
US60/909,692 2007-04-02
US12/060,801 US7910392B2 (en) 2007-04-02 2008-04-01 Method and system for assembling a solar cell package
US12/060,801 2008-04-01

Publications (2)

Publication Number Publication Date
WO2008122046A2 true WO2008122046A2 (en) 2008-10-09
WO2008122046A3 WO2008122046A3 (en) 2009-01-29

Family

ID=39792208

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2008/059167 WO2008122046A2 (en) 2007-04-02 2008-04-02 Method and system for assembling a solar cell package

Country Status (2)

Country Link
US (1) US7910392B2 (en)
WO (1) WO2008122046A2 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8227688B1 (en) 2005-10-17 2012-07-24 Solaria Corporation Method and resulting structure for assembling photovoltaic regions onto lead frame members for integration on concentrating elements for solar cells
US7910822B1 (en) 2005-10-17 2011-03-22 Solaria Corporation Fabrication process for photovoltaic cell
AU2007346895A1 (en) * 2007-02-15 2008-08-21 Transform Solar Pty Ltd A method for processing elongate substrates and a substrate securing apparatus
US7910392B2 (en) 2007-04-02 2011-03-22 Solaria Corporation Method and system for assembling a solar cell package
US20090056806A1 (en) * 2007-09-05 2009-03-05 Solaria Corporation Solar cell structure including a plurality of concentrator elements with a notch design and predetermined radii and method
US8119902B2 (en) 2007-05-21 2012-02-21 Solaria Corporation Concentrating module and method of manufacture for photovoltaic strips
US7910035B2 (en) 2007-12-12 2011-03-22 Solaria Corporation Method and system for manufacturing integrated molded concentrator photovoltaic device
US20100294338A1 (en) * 2009-02-20 2010-11-25 Solaria Corporation Large Area Concentrator Lens Structure and Method
WO2010101810A1 (en) * 2009-03-03 2010-09-10 Arkema France Thermoformable photovoltaic backsheet
US20140017845A1 (en) * 2011-03-31 2014-01-16 Dow Corning Corporation Method Of Forming A Photovoltaic Cell Module With A Cell Press
USD699176S1 (en) 2011-06-02 2014-02-11 Solaria Corporation Fastener for solar modules
KR101791130B1 (en) * 2016-11-18 2017-10-27 엘지전자 주식회사 Solar cell module
CN111091444B (en) * 2019-11-28 2023-09-26 西安隆基智能技术有限公司 Solar cell matching method and device and electronic equipment

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5840147A (en) * 1995-06-07 1998-11-24 Edison Welding Institute Plastic joining method
US20030016539A1 (en) * 2000-03-16 2003-01-23 Minano Juan C. High efficiency non-imaging optics
US20060283495A1 (en) * 2005-06-06 2006-12-21 Solaria Corporation Method and system for integrated solar cell using a plurality of photovoltaic regions

Family Cites Families (250)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US633457A (en) * 1898-05-31 1899-09-19 William Hotze Hair-drying comb.
US1848319A (en) * 1926-12-01 1932-03-08 Clifford Mfg Co Method and apparatus for exhausting and sealing metallic bellows
US2470618A (en) 1946-03-26 1949-05-17 Lawrence T Holden Electrical apparatus
US3330700A (en) 1963-06-17 1967-07-11 Electro Optical Systems Inc Solar-cell panels
US3575721A (en) 1965-04-26 1971-04-20 Textron Inc Solar cell arrays and connectors
US3446676A (en) 1966-09-07 1969-05-27 Webb James E Solar battery with interconnecting means for plural cells
GB1187969A (en) 1966-11-24 1970-04-15 Pilkington Brothers Ltd Improvements relating to the Manufacture of Glass in Sheet Form.
LU52726A1 (en) 1966-12-30 1968-08-05
US3641354A (en) 1967-03-08 1972-02-08 Jack De Ment Optical modulation by fluidic optics utilizing chromatic aberration
US3849880A (en) 1969-12-12 1974-11-26 Communications Satellite Corp Solar cell array
US3700714A (en) * 1971-06-24 1972-10-24 Stephen B Hamilton Curable compositions
US3819417A (en) 1972-05-17 1974-06-25 Communications Satellite Corp Mechanically interlaced and electrically interconnected silicon solar cells
US3951633A (en) 1974-12-23 1976-04-20 Combustion Engineering, Inc. Method for producing patterned glass on a float ribbon
US3993505A (en) 1975-05-27 1976-11-23 Hughes Aircraft Company Interconnector for components such as solar cells or the like
US3999283A (en) 1975-06-11 1976-12-28 Rca Corporation Method of fabricating a photovoltaic device
US4029519A (en) * 1976-03-19 1977-06-14 The United States Of America As Represented By The United States Energy Research And Development Administration Solar collector having a solid transmission medium
US4295463A (en) 1976-04-26 1981-10-20 Citron Jeffrey M Flexible V-shaped solar tracking concentrating solar energy collector
US4056405A (en) 1976-05-10 1977-11-01 Solarex Corporation Panel for solar energy cells
US4097230A (en) * 1976-10-08 1978-06-27 Eastman Kodak Company Method for transferring heat-transferable dyes
US4143234A (en) * 1976-11-08 1979-03-06 Monsanto Company Solar collector using total internal reflectance
US4091798A (en) * 1977-02-03 1978-05-30 Nasa Non-tracking solar energy collector system
GB1554507A (en) * 1977-04-28 1979-10-24 Tideland Signal Corp Enclosure for solar cells
US4118249A (en) * 1977-08-30 1978-10-03 The United States Of America As Represented By The United States Department Of Energy Modular assembly of a photovoltaic solar energy receiver
US4106952A (en) 1977-09-09 1978-08-15 Kravitz Jerome H Solar panel unit
US4193820A (en) 1977-10-07 1980-03-18 Organisation Europeenne De Recherches Spatiales Interconnection device for solar cells
US4170507A (en) 1977-12-27 1979-10-09 Motorola, Inc. Method for encapsulating a solar cell array
US4174978A (en) 1978-05-11 1979-11-20 Chubrikov Boris A Semiconductor photovoltaic generator and method of fabricating thereof
US4203646A (en) 1978-05-17 1980-05-20 Amp Incorporated Clip for electrically connecting planar elements, such as solar cells, and the like, in series
US4166917A (en) * 1978-05-22 1979-09-04 Corning Glass Works Concentrating solar receiver
US4311869A (en) 1978-06-30 1982-01-19 Exxon Research & Engineering Co. Solar cell modules
US4257821A (en) 1978-11-13 1981-03-24 Trw Inc. Universal solar cell/conductor junction element and solar panel embodying same
DE2926754A1 (en) * 1979-07-03 1981-01-15 Licentia Gmbh SOLAR CELL ARRANGEMENT
US4239555A (en) 1979-07-30 1980-12-16 Mobil Tyco Solar Energy Corporation Encapsulated solar cell array
US4293192A (en) 1980-05-27 1981-10-06 Bronstein Allen I Solar reflector with flexible sheet tightly secured around form surfaces
US4333447A (en) * 1980-06-04 1982-06-08 Corning Glass Works Solar receiver tube support
US4355478A (en) * 1980-06-19 1982-10-26 Armstrong Joe W Method for making framed structures
US4361136A (en) 1980-08-26 1982-11-30 Linus Huang Concentric solar collector
DE3135933A1 (en) * 1980-09-26 1982-05-19 Unisearch Ltd., Kensington, New South Wales SOLAR CELL AND METHOD FOR THEIR PRODUCTION
US4362903A (en) 1980-12-29 1982-12-07 General Electric Company Electrical conductor interconnect providing solderable connections to hard-to-contact substrates, such as liquid crystal cells
DE3107888A1 (en) * 1981-03-02 1982-09-16 Imchemie Kunststoff Gmbh, 5632 Wermelskirchen SOLAR CONCENTRATOR
GB2097328B (en) * 1981-04-24 1984-09-05 Glaverbel Laminated reflective panels
US4863224A (en) * 1981-10-06 1989-09-05 Afian Viktor V Solar concentrator and manufacturing method therefor
US4691994A (en) * 1981-10-06 1987-09-08 Afian Viktor V Method for a solar concentrator manufacturing
US4454371A (en) * 1981-12-03 1984-06-12 The United States Of America As Represented By The Secretary Of The Air Force Solar energy concentrator system
US4463749A (en) * 1982-03-08 1984-08-07 Ford Aerospace & Communications Corporation Modular solar concentrator
US4457297A (en) * 1982-03-08 1984-07-03 Ford Aerospace & Communications Corp. Modular solar concentrator
US4495360A (en) 1982-04-30 1985-01-22 General Electric Company Ultraviolet light absorbing agents, method for making, compositions and articles containing same
US4449514A (en) * 1982-06-25 1984-05-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Solar concentrator protective system
JPS604270A (en) * 1983-06-22 1985-01-10 Hitachi Ltd Manufacture of solar battery
US4589191A (en) * 1983-10-20 1986-05-20 Unisearch Limited Manufacture of high efficiency solar cells
US4668314A (en) 1983-10-25 1987-05-26 Casio Computer Co., Ltd. Method of manufacturing a small electronic device
US4571812A (en) * 1984-02-16 1986-02-25 Industrial Solar Technology Method for making a solar concentrator and product
DE3418078A1 (en) 1984-05-16 1985-11-21 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt METHOD FOR PRODUCING A SUPPORT MATERIAL FOR THE SOLAR CELLS OF A SOLAR GENERATOR
US4663562A (en) 1984-07-16 1987-05-05 General Electric Company Contrast enhancement structure for color cathode ray tube
JPS6144741A (en) 1984-08-10 1986-03-04 Bridgestone Corp Production of laminate
US4638110A (en) 1985-06-13 1987-01-20 Illuminated Data, Inc. Methods and apparatus relating to photovoltaic semiconductor devices
US4711972A (en) 1985-07-05 1987-12-08 Entech, Inc. Photovoltaic cell cover for use with a primary optical concentrator in a solar energy collector
DE3527001A1 (en) 1985-07-27 1987-02-19 Telefunken Electronic Gmbh SOLAR GENERATOR
US4683154A (en) * 1985-08-19 1987-07-28 The United States Of America As Represented By The United States Department Of Energy Laser sealed vacuum insulation window
US4848319A (en) 1985-09-09 1989-07-18 Minnesota Mining And Manufacturing Company Refracting solar energy concentrator and thin flexible Fresnel lens
US4692557A (en) 1986-10-16 1987-09-08 Shell Oil Company Encapsulated solar cell assemblage and method of making
DE3741477A1 (en) 1987-12-08 1989-06-22 Fraunhofer Ges Forschung CONCENTRATOR ARRANGEMENT
AU612226B2 (en) * 1987-12-17 1991-07-04 Unisearch Limited Solar cells with tilted geometrical features
US4830038A (en) 1988-01-20 1989-05-16 Atlantic Richfield Company Photovoltaic module
JPH0769602B2 (en) 1988-04-19 1995-07-31 ソマール株式会社 Light-shielding masking film
JPH04506249A (en) 1989-03-01 1992-10-29 ボミン ゾラール ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディトゲゼルシャフト Solar concentrator - device
US5118361A (en) * 1990-05-21 1992-06-02 The Boeing Company Terrestrial concentrator solar cell module
US5096505A (en) 1990-05-21 1992-03-17 The Boeing Company Panel for solar concentrators and tandem cell units
US5006179A (en) 1989-05-24 1991-04-09 Solarex Corporation Interconnect for electrically connecting solar cells
US4953577A (en) 1989-07-06 1990-09-04 Solarex Corporation Spray encapsulation of photovoltaic modules
US5180888A (en) 1989-08-10 1993-01-19 Casio Computer Co., Ltd. Conductive bonding agent and a conductive connecting method
US4999059A (en) * 1989-08-11 1991-03-12 Bagno Robert G Universal solar concentrator panel
US5011544A (en) 1989-09-08 1991-04-30 Solarex Corporation Solar panel with interconnects and masking structure, and method
EP0440869A1 (en) 1990-02-09 1991-08-14 Bio-Photonics, Inc. Photovoltaic element able to convert solar radiation into electric current and photoelectric battery
US5133780A (en) * 1990-08-09 1992-07-28 Crs Sirrine Engineers, Inc. Apparatus for fixed bed coal gasification
FR2670774B1 (en) 1990-12-21 1993-09-10 Saint Gobain Vitrage Int DIFFUSING GLAZING.
US5245985A (en) * 1991-01-16 1993-09-21 Holland Beecher J Effective and simple solar concentrator
US5167724A (en) 1991-05-16 1992-12-01 The United States Of America As Represented By The United States Department Of Energy Planar photovoltaic solar concentrator module
US5153780A (en) 1991-06-10 1992-10-06 The United States Of America As Represented By The United States Department Of Energy Method and apparatus for uniformly concentrating solar flux for photovoltaic applications
US5240510A (en) * 1991-09-23 1993-08-31 Development Products Inc. Photovoltaic cell
US5174275A (en) 1991-11-21 1992-12-29 Holland Beecher J Wide-angle solar concentrator
US5356488A (en) * 1991-12-27 1994-10-18 Rudolf Hezel Solar cell and method for its manufacture
US5180442A (en) 1992-04-06 1993-01-19 Eric Elias Integration system for solar modules
US5261970A (en) 1992-04-08 1993-11-16 Sverdrup Technology, Inc. Optoelectronic and photovoltaic devices with low-reflectance surfaces
EP0663077A4 (en) 1992-09-04 1995-11-29 Univ Australian Optical reflector arrays and apparatus using such arrays.
US5344496A (en) * 1992-11-16 1994-09-06 General Dynamics Corporation, Space Systems Division Lightweight solar concentrator cell array
JPH0768562B2 (en) 1992-11-25 1995-07-26 三井金属鉱業株式会社 Method for producing solderable copper powder for conductive paint
EP0627495B1 (en) * 1993-05-10 1998-08-12 Optical Coating Laboratory, Inc. Self-healing UV-barrier coating with flexible polymer substrate
US6084175A (en) 1993-05-20 2000-07-04 Amoco/Enron Solar Front contact trenches for polycrystalline photovoltaic devices and semi-conductor devices with buried contacts
US5395070A (en) * 1993-11-30 1995-03-07 Stirbl; Robert C. Solar energy concentrator assembly and associated method
JP3360919B2 (en) 1993-06-11 2003-01-07 三菱電機株式会社 Method of manufacturing thin-film solar cell and thin-film solar cell
EP0631328B1 (en) * 1993-06-24 1998-05-27 Canon Kabushiki Kaisha Solar cell module having heat-fused portion to improve moisture resistance
AU7600494A (en) 1993-08-20 1995-03-21 Christopher P. Kinkaid Non-tracking solar concentrator heat sink and housing system
US5436725A (en) 1993-10-12 1995-07-25 Hughes Aircraft Company Cofocal optical system for thickness measurements of patterned wafers
US5460659A (en) 1993-12-10 1995-10-24 Spectrolab, Inc. Concentrating photovoltaic module and fabrication method
US5478402A (en) * 1994-02-17 1995-12-26 Ase Americas, Inc. Solar cell modules and method of making same
US5468304A (en) 1994-03-14 1995-11-21 Texas Instruments Incorporated Output-increasing, protective cover for a solar cell
US5508205A (en) 1994-03-29 1996-04-16 Amoco/Enron Solar Method of making and utilizing partially cured photovoltaic assemblies
AUPM597794A0 (en) 1994-05-31 1994-06-23 Australian National University, The Lenses formed by arrays of reflectors
US5517339A (en) * 1994-06-17 1996-05-14 Northeast Photosciences Method of manufacturing high efficiency, broad bandwidth, volume holographic elements and solar concentrators for use therewith
US5529054A (en) * 1994-06-20 1996-06-25 Shoen; Neil C. Solar energy concentrator and collector system and associated method
US5518387A (en) 1994-06-22 1996-05-21 Husky Injection Molding Systems Ltd. Pivoting workpiece removal device
US5466301A (en) 1994-06-29 1995-11-14 Texas Instruments Incorporated Solar cell having an output-increasing, protective cover
US5498297A (en) * 1994-09-15 1996-03-12 Entech, Inc. Photovoltaic receiver
US5915170A (en) 1994-09-20 1999-06-22 Tessera, Inc. Multiple part compliant interface for packaging of a semiconductor chip and method therefor
US6020553A (en) 1994-10-09 2000-02-01 Yeda Research And Development Co., Ltd. Photovoltaic cell system and an optical structure therefor
US5542409A (en) * 1995-01-06 1996-08-06 Sampayo; Eduardo A. Solar concentrator system
AU5353396A (en) 1995-01-26 1996-08-14 Louis J Gerics A roof module having an integral solar energy concentrator
US5564411A (en) 1995-01-26 1996-10-15 Myles, Iii; John F. Roof module having an integral solar energy concentrator
WO1996024954A1 (en) 1995-02-09 1996-08-15 Solardyne Corporation Non-tracking solar concentrator heat sink and housing system
US5735966A (en) * 1995-05-15 1998-04-07 Luch; Daniel Substrate structures for integrated series connected photovoltaic arrays and process of manufacture of such arrays
US5959787A (en) * 1995-06-06 1999-09-28 The Boeing Company Concentrating coverglass for photovoltaic cells
US6074614A (en) 1995-06-07 2000-06-13 Molecular Devices Corporation Multi-assay plate cover for elimination of meniscus
US5660644A (en) * 1995-06-19 1997-08-26 Rockwell International Corporation Photovoltaic concentrator system
US5877874A (en) * 1995-08-24 1999-03-02 Terrasun L.L.C. Device for concentrating optical radiation
US5616186A (en) 1995-09-18 1997-04-01 Jx Crystals Inc. Thermophotovoltaic electric generator using low bandgap photovoltaic cells with a hydrocarbon burner and enhanced catalytic infrared emitter
US5846444A (en) 1995-10-03 1998-12-08 Corning Incorporated Surface treatment of glass
US5733382A (en) * 1995-12-18 1998-03-31 Hanoka; Jack I. Solar cell modules and method of making same
US6093757A (en) 1995-12-19 2000-07-25 Midwest Research Institute Composition and method for encapsulating photovoltaic devices
US6433913B1 (en) * 1996-03-15 2002-08-13 Gentex Corporation Electro-optic device incorporating a discrete photovoltaic device and method and apparatus for making same
US5851309A (en) 1996-04-26 1998-12-22 Kousa; Paavo Directing and concentrating solar energy collectors
US5782993A (en) * 1996-06-28 1998-07-21 Ponewash; Jackie Photovoltaic cells having micro-embossed optical enhancing structures
US5735262A (en) 1996-07-22 1998-04-07 Stirling Thermal Motors, Inc. Solar energy diffuser
US5787878A (en) * 1996-09-23 1998-08-04 Ratliff, Jr.; George D. Solar concentrator
US5865905A (en) * 1996-09-30 1999-02-02 Boeing North American, Inc. Rolled film solar concentrator
US5882434A (en) * 1996-10-15 1999-03-16 United Solar Technologies, Inc. Solar concentrator having an offset parabolic configuration
US5936777A (en) * 1996-10-31 1999-08-10 Lightpath Technologies, Inc. Axially-graded index-based couplers for solar concentrators
US6551844B1 (en) 1997-01-15 2003-04-22 Formfactor, Inc. Test assembly including a test die for testing a semiconductor product die
AUPO468697A0 (en) 1997-01-21 1997-02-13 Australian National University, The A method of producing thin silicon epitaxial films
JPH10338548A (en) 1997-04-30 1998-12-22 Agfa Gevaert Nv Production of thin glass on roll
US6264510B1 (en) 1997-05-28 2001-07-24 Harness System Technologies Research Ltd. Laser-welded bus bar structure
JP3805889B2 (en) 1997-06-20 2006-08-09 株式会社カネカ Solar cell module and manufacturing method thereof
US5919316A (en) 1997-06-27 1999-07-06 The United States Of America As Represented By The Secretary Of The Air Force Spacecraft solar array design to control differential charging
AU745347B2 (en) 1997-07-25 2002-03-21 Arch Development Corporation Nontracking solar concentrators
US6676263B2 (en) * 1997-07-25 2004-01-13 The University Of Chicago Performance improvements of symmetry-breaking reflector structures in nonimaging devices
US6008449A (en) 1997-08-19 1999-12-28 Cole; Eric D. Reflective concentrating solar cell assembly
JPH1197733A (en) * 1997-09-18 1999-04-09 Sanyo Electric Co Ltd Photovoltaic device
US6320116B1 (en) 1997-09-26 2001-11-20 Evergreen Solar, Inc. Methods for improving polymeric materials for use in solar cell applications
DE19744767C2 (en) 1997-10-10 2001-05-17 Deutsch Zentr Luft & Raumfahrt Parabolic trough concentrator
ATE219725T1 (en) 1997-10-24 2002-07-15 Agfa Gevaert COMPOSITE DISC HAVING A THIN BOROSILICATE GLASS SUBSTRATE AS A FORMING LAYER
US6107564A (en) * 1997-11-18 2000-08-22 Deposition Sciences, Inc. Solar cell cover and coating
US6057505A (en) 1997-11-21 2000-05-02 Ortabasi; Ugur Space concentrator for advanced solar cells
JPH11186572A (en) 1997-12-22 1999-07-09 Canon Inc Photoelectromotive force element module
JP3174549B2 (en) * 1998-02-26 2001-06-11 株式会社日立製作所 Photovoltaic power generation device, photovoltaic power generation module, and method of installing photovoltaic power generation system
DE29823351U1 (en) 1998-03-10 1999-05-06 Ver Glaswerke Gmbh Glazing to control the transmission of light
JP2002507835A (en) 1998-03-13 2002-03-12 ケラー・シュテフェン Solar cell device
US7282240B1 (en) 1998-04-21 2007-10-16 President And Fellows Of Harvard College Elastomeric mask and use in fabrication of devices
GB9810587D0 (en) * 1998-05-15 1998-07-15 Cryostar France Sa Pump
AUPP437598A0 (en) 1998-06-29 1998-07-23 Unisearch Limited A self aligning method for forming a selective emitter and metallization in a solar cell
US6700054B2 (en) * 1998-07-27 2004-03-02 Sunbear Technologies, Llc Solar collector for solar energy systems
JP3259692B2 (en) 1998-09-18 2002-02-25 株式会社日立製作所 Concentrating photovoltaic module, method of manufacturing the same, and concentrating photovoltaic system
US6335479B1 (en) 1998-10-13 2002-01-01 Dai Nippon Printing Co., Ltd. Protective sheet for solar battery module, method of fabricating the same and solar battery module
GB2343741B (en) 1998-11-11 2002-03-13 Phos Energy Inc Solar energy concentrator and converter
US6118067A (en) * 1998-11-20 2000-09-12 Swales Aerospace Method and apparatus for improved solar concentration arrays
EP1048628A1 (en) 1999-04-30 2000-11-02 Schott Glas Polymer coated glassfoil substrate
US6262358B1 (en) 1999-02-18 2001-07-17 Sharp Kabushiki Kaisha Solar cell module and solar cell panel using the same
JP2000323208A (en) 1999-03-10 2000-11-24 Sharp Corp Inter-connector, its forming method and its joining device
JP4044237B2 (en) 1999-03-25 2008-02-06 株式会社カネカ Solar panel installation structure and installation method
US6150602A (en) 1999-05-25 2000-11-21 Hughes Electronics Corporation Large area solar cell extended life interconnect
US6274860B1 (en) * 1999-05-28 2001-08-14 Terrasun, Llc Device for concentrating optical radiation
EP1194956A4 (en) 1999-06-21 2005-01-19 Aec Able Eng Co Inc Solar cell array
US6580026B1 (en) * 1999-06-30 2003-06-17 Catalysts & Chemicals Industries Co., Ltd. Photovoltaic cell
US6034322A (en) 1999-07-01 2000-03-07 Space Systems/Loral, Inc. Solar cell assembly
US6091017A (en) * 1999-08-23 2000-07-18 Composite Optics Incorporated Solar concentrator array
US6134784A (en) 1999-08-27 2000-10-24 Photovoltaics International, Llc Method of making solar collectors by in-situ encapsulation of solar cells
US6333458B1 (en) 1999-11-26 2001-12-25 The Trustees Of Princeton University Highly efficient multiple reflection photosensitive optoelectronic device with optical concentrator
US6440769B2 (en) * 1999-11-26 2002-08-27 The Trustees Of Princeton University Photovoltaic device with optical concentrator and method of making the same
US6337283B1 (en) * 1999-12-30 2002-01-08 Sunpower Corporation Method of fabricating a silicon solar cell
US6423568B1 (en) * 1999-12-30 2002-07-23 Sunpower Corporation Method of fabricating a silicon solar cell
US6387726B1 (en) * 1999-12-30 2002-05-14 Sunpower Corporation Method of fabricating a silicon solar cell
US6274402B1 (en) * 1999-12-30 2001-08-14 Sunpower Corporation Method of fabricating a silicon solar cell
AU767127B2 (en) 2000-01-07 2003-10-30 Midwest Research Institute Multi-facet concentrator of solar setup for irradiating the objects placed in a target plane with solar light
US20040194820A1 (en) 2000-01-20 2004-10-07 Steven Barone Self tracking, wide angle solar concentrators
AU2001260971A1 (en) * 2000-01-20 2001-08-07 Bd Systems, Llc Self tracking, wide angle, solar concentrators
JP2001210849A (en) 2000-01-24 2001-08-03 Sumitomo Wiring Syst Ltd Connector for solar battery panel
US6293803B1 (en) 2000-02-09 2001-09-25 Trw Inc. Zee electrical interconnect
US6359209B1 (en) 2000-02-23 2002-03-19 Hughes Electronics Corporation Solar panel and solar cell having in-plane solar cell interconnect with integrated diode tab
DE10017610C2 (en) * 2000-03-30 2002-10-31 Hahn Meitner Inst Berlin Gmbh Process for producing a solar module with integrated series-connected thin-film solar cells and use thereof
US6276359B1 (en) 2000-05-24 2001-08-21 Scott Frazier Double reflecting solar concentrator
EP1174342A1 (en) * 2000-07-20 2002-01-23 Université de Liège Solar concentrator
US6333457B1 (en) 2000-08-29 2001-12-25 Sunpower Corporation Edge passivated silicon solar/photo cell and method of manufacture
JP3748370B2 (en) * 2000-09-11 2006-02-22 シャープ株式会社 Solar cell module
US6395972B1 (en) 2000-11-09 2002-05-28 Trw Inc. Method of solar cell external interconnection and solar cell panel made thereby
JP4137415B2 (en) 2000-11-21 2008-08-20 シャープ株式会社 How to replace solar cells
WO2003047004A1 (en) 2001-11-29 2003-06-05 Origin Energy Solar Pty Ltd Semiconductor texturing process
AUPR174800A0 (en) 2000-11-29 2000-12-21 Australian National University, The Semiconductor processing
US6971756B2 (en) * 2000-12-18 2005-12-06 Svv Technology Innovations, Inc. Apparatus for collecting and converting radiant energy
IL156245A0 (en) * 2000-12-22 2004-01-04 Dca Design Int Ltd Drive mechanism for an injection device
US6541694B2 (en) 2001-03-16 2003-04-01 Solar Enterprises International, Llc Nonimaging light concentrator with uniform irradiance
CN1501892A (en) 2001-03-20 2004-06-02 PPG��ҵ����˾ Method and apparatus for forming patterned and/or textured glass and glass articles formed thereby
US6620995B2 (en) * 2001-03-30 2003-09-16 Sergiy Victorovich Vasylyev Non-imaging system for radiant energy flux transformation
EP1261039A1 (en) 2001-05-23 2002-11-27 Université de Liège Solar concentrator
US6535712B2 (en) * 2001-07-06 2003-03-18 Hewlett-Packard Company Gloss control method and apparatus with disposable toner cartridges containing clear toners
JP3685097B2 (en) 2001-07-12 2005-08-17 松下電器産業株式会社 Screen printing apparatus and screen printing method
US6626415B1 (en) * 2001-07-20 2003-09-30 Rafael A. Aguila Valve assembly
US6809250B2 (en) 2001-08-10 2004-10-26 Astrium Gmbh Repaired solar panel and method of preparing same
US6668820B2 (en) 2001-08-24 2003-12-30 Solargenix Energy Llc Multiple reflector solar concentrators and systems
US6612181B2 (en) 2001-09-04 2003-09-02 Jalees Ahmad Method and system for determining crack nucleation of a part subject to fretting fatigue
KR100847618B1 (en) 2001-09-05 2008-07-21 니혼 이타가라스 가부시키가이샤 High transmission glass plates and method for manufacturing the same
WO2003022578A1 (en) 2001-09-11 2003-03-20 The Australian National University Solar energy concentrating assembly and sub-components thereof
US7208674B2 (en) * 2001-09-11 2007-04-24 Eric Aylaian Solar cell having photovoltaic cells inclined at acute angle to each other
CA2442314A1 (en) 2001-09-14 2003-03-27 Sumitomo Chemical Company, Limited Photosemiconductor encapsulating resin composition
US6804062B2 (en) * 2001-10-09 2004-10-12 California Institute Of Technology Nonimaging concentrator lens arrays and microfabrication of the same
TWI250135B (en) 2001-10-15 2006-03-01 Hoya Corp Optical glass, glass material for press molding, optical element, and method of manufacturing same
JP2003124491A (en) 2001-10-15 2003-04-25 Sharp Corp Thin film solar cell module
US7169669B2 (en) * 2001-12-04 2007-01-30 Origin Energy Solar Pty. Ltd. Method of making thin silicon sheets for solar cells
AU2003211873B2 (en) 2002-01-25 2008-05-22 Sumitomo Bakelite Co., Ltd. Transparent composite composition
US6612705B1 (en) * 2002-02-19 2003-09-02 Mark Davidson Mini-optics solar energy concentrator
US6829908B2 (en) 2002-02-27 2004-12-14 Corning Incorporated Fabrication of inclusion free homogeneous glasses
TW589919B (en) 2002-03-29 2004-06-01 Sanyo Electric Co Method for vapor deposition and method for making display device
US7388146B2 (en) 2002-04-24 2008-06-17 Jx Crystals Inc. Planar solar concentrator power module
US6619282B1 (en) * 2002-05-16 2003-09-16 R. Michael Murtha Solar concentrating liquid lightguide
US20040243364A1 (en) 2002-05-22 2004-12-02 Wendelin Timothy J. Method and system for modeling solar optics
US6758609B2 (en) 2002-06-11 2004-07-06 Lambda Technologies Methods and apparatus of joining optically coupled optoelectronic and fiber optic components using electromagnetic radiation
AU2003278267A1 (en) 2002-09-10 2004-04-30 Saint-Gobain Glass France Connecting device for a multilayer flat element equipped with electrical functional elements and flat element
US6609836B1 (en) 2002-09-17 2003-08-26 The United States Of America As Represented By The Secretary Of The Navy Method for coupling fiber optic elements
WO2004038462A1 (en) * 2002-10-22 2004-05-06 Sunray Technologies, Inc. Diffractive structures for the redirection and concentration of optical radiation
JP4181862B2 (en) 2002-11-28 2008-11-19 篠田プラズマ株式会社 Arc tube array type display device
GB0227718D0 (en) 2002-11-28 2003-01-08 Eastman Kodak Co A photovoltaic device and a manufacturing method hereof
US6686263B1 (en) * 2002-12-09 2004-02-03 Advanced Micro Devices, Inc. Selective formation of top memory electrode by electroless formation of conductive materials
EP1587635A4 (en) 2002-12-17 2006-03-01 Insight Equity A P X Lp Rapid, thermally cured, back side mar resistant and antireflective coating for ophthalmic lenses
US20040246605A1 (en) 2003-03-04 2004-12-09 Stiles Michael R. Poly-conical reflectors for collecting, concentrating, and projecting light rays
US20050081908A1 (en) * 2003-03-19 2005-04-21 Stewart Roger G. Method and apparatus for generation of electrical power from solar energy
AU2003902270A0 (en) 2003-05-09 2003-05-29 Origin Energy Solar Pty Ltd Separating and assembling semiconductor strips
ES2375607T3 (en) 2003-07-07 2012-03-02 Dow Corning Corporation ENCAPSULATION OF SOLAR CELLS.
US20050081909A1 (en) * 2003-10-20 2005-04-21 Paull James B. Concentrating solar roofing shingle
US7112253B2 (en) * 2003-10-22 2006-09-26 Mario Rabinowitz Manufacturing transparent mirrored mini-balls for solar energy concentration and analogous applications
US7055519B2 (en) 2003-12-10 2006-06-06 United Technologies Corporation Solar collector and method
US20050133082A1 (en) 2003-12-20 2005-06-23 Konold Annemarie H. Integrated solar energy roofing construction panel
US6958868B1 (en) 2004-03-29 2005-10-25 John George Pender Motion-free tracking solar concentrator
US20060266406A1 (en) 2004-06-09 2006-11-30 Tom Faust Devulcanized photovoltaic roofing tiles
JP5219512B2 (en) 2004-08-09 2013-06-26 トランスフォーム・ソーラー・ピーティーワイ・リミテッド Solar cell (elongated small piece) submodule structure
US20060042681A1 (en) 2004-08-24 2006-03-02 General Electric Company Pv laminate backplane with optical concentrator
US7442871B2 (en) * 2004-09-13 2008-10-28 General Electric Company Photovoltaic modules for solar concentrator
DE102005009066A1 (en) 2005-02-28 2006-09-07 Osram Opto Semiconductors Gmbh Method for producing an optical and a radiation-emitting component and optical and radiation-emitting component
US20060235717A1 (en) 2005-04-18 2006-10-19 Solaria Corporation Method and system for manufacturing solar panels using an integrated solar cell using a plurality of photovoltaic regions
HRPK20050434B3 (en) 2005-05-16 2008-06-30 Urli Natko Stationary photovoltaic module with low concentration ratio of solar radiation
DE102005033272A1 (en) 2005-06-03 2006-12-07 Solartec Ag Concentrator photovoltaic device, PV concentrator module formed therefrom and manufacturing method thereof
US8039731B2 (en) 2005-06-06 2011-10-18 General Electric Company Photovoltaic concentrator for solar energy system
EP1902475A2 (en) 2005-06-06 2008-03-26 Solaria Corporation Method and system for integrated solar cell using a plurality of photovoltaic regions
US20080178922A1 (en) 2005-07-26 2008-07-31 Solaria Corporation Method and system for manufacturing solar panels using an integrated solar cell using a plurality of photovoltaic regions
US20070056626A1 (en) 2005-09-12 2007-03-15 Solaria Corporation Method and system for assembling a solar cell using a plurality of photovoltaic regions
DE102005047132A1 (en) 2005-09-30 2007-04-12 Solartec Ag Concentrator photovoltaic device; Photovoltaic device for use therein and manufacturing method therefor
RU2430897C2 (en) 2005-10-21 2011-10-10 Сэн-Гобэн Гласс Франс Non-fouling material and method of producing said material
US20070146910A1 (en) 2005-12-22 2007-06-28 Solbeam, Inc. Light steering assemblies
US7855335B2 (en) 2006-04-26 2010-12-21 Palo Alto Research Center Incorporated Beam integration for concentrating solar collector
TW200814343A (en) 2006-09-12 2008-03-16 Delta Electronics Inc Energy collecting system
TW200905901A (en) 2007-03-29 2009-02-01 Daniel F Baldwin Solar module manufacturing processes
US7910392B2 (en) 2007-04-02 2011-03-22 Solaria Corporation Method and system for assembling a solar cell package
US20080314438A1 (en) 2007-06-20 2008-12-25 Alan Anthuan Tran Integrated concentrator photovoltaics and water heater

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5840147A (en) * 1995-06-07 1998-11-24 Edison Welding Institute Plastic joining method
US20030016539A1 (en) * 2000-03-16 2003-01-23 Minano Juan C. High efficiency non-imaging optics
US20060283495A1 (en) * 2005-06-06 2006-12-21 Solaria Corporation Method and system for integrated solar cell using a plurality of photovoltaic regions

Also Published As

Publication number Publication date
US7910392B2 (en) 2011-03-22
US20080236664A1 (en) 2008-10-02
WO2008122046A3 (en) 2009-01-29

Similar Documents

Publication Publication Date Title
US7910392B2 (en) Method and system for assembling a solar cell package
US8242351B2 (en) Solar cell structure including a plurality of concentrator elements with a notch design and predetermined radii and method
US20070095386A1 (en) Method and system for integrated solar cell using a plurality of photovoltaic regions
US8049098B2 (en) Notch structure for concentrating module and method of manufacture using photovoltaic strips
US20100282317A1 (en) Method and system for assembling a solar cell using a plurality of photovoltaic regions
US8119902B2 (en) Concentrating module and method of manufacture for photovoltaic strips
EP2194584A1 (en) Solar cell, concentrator photovoltaic module, concentrator photovoltaic unit and solar cell manufacturing method
US20120167945A1 (en) Photovoltaic devices having shaped concentrator members
US20120295388A1 (en) Large area concentrator lens structure and method
EP1902475A2 (en) Method and system for integrated solar cell using a plurality of photovoltaic regions
US20090188563A1 (en) Solar Cell Structure Including A Plurality of Concentrator Elements With A Notch Design and Predetermined Radii and Method
US20100282316A1 (en) Solar Cell Concentrator Structure Including A Plurality of Glass Concentrator Elements With A Notch Design
US7910035B2 (en) Method and system for manufacturing integrated molded concentrator photovoltaic device
WO2008122047A1 (en) Solar cell structure including a plurality of concentrator elements with a notch design and predetermined radii and method
US20090151770A1 (en) Method and material for coupling solar concentrators and photovoltaic devices
US8168884B2 (en) Solar cell structure including a plurality of concentrator elements with a notch design and predetermined radii and method
US8227688B1 (en) Method and resulting structure for assembling photovoltaic regions onto lead frame members for integration on concentrating elements for solar cells
US8173890B2 (en) Solar cell structure including a plurality of concentrator elements with a notch design and predetermined RADII and method
US20080236651A1 (en) Solar cell concentrator structure including a plurality of concentrator elements with a notch design and method having a predetermined efficiency
US20110017264A1 (en) Thermal management method and device for solar concentrator systems
Sweatt et al. Photo-voltaic system using micro-optics
KR20220065322A (en) Solar Cell Module with Holes and Method for Manufacturing the Same

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 08744959

Country of ref document: EP

Kind code of ref document: A2

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 08744959

Country of ref document: EP

Kind code of ref document: A2