CA2428530C - Heater for aircraft potable water tank - Google Patents
Heater for aircraft potable water tank Download PDFInfo
- Publication number
- CA2428530C CA2428530C CA2428530A CA2428530A CA2428530C CA 2428530 C CA2428530 C CA 2428530C CA 2428530 A CA2428530 A CA 2428530A CA 2428530 A CA2428530 A CA 2428530A CA 2428530 C CA2428530 C CA 2428530C
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- CA
- Canada
- Prior art keywords
- sleeve
- wire
- insulating coating
- wire structure
- heater
- Prior art date
- Legal status (The legal status 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 status listed.)
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Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/40—Heating elements having the shape of rods or tubes
- H05B3/54—Heating elements having the shape of rods or tubes flexible
- H05B3/56—Heating cables
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01C—RESISTORS
- H01C1/00—Details
- H01C1/08—Cooling, heating or ventilating arrangements
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01C—RESISTORS
- H01C3/00—Non-adjustable metal resistors made of wire or ribbon, e.g. coiled, woven or formed as grids
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01C—RESISTORS
- H01C3/00—Non-adjustable metal resistors made of wire or ribbon, e.g. coiled, woven or formed as grids
- H01C3/06—Flexible or folding resistors, whereby such a resistor can be looped or collapsed upon itself
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01C—RESISTORS
- H01C3/00—Non-adjustable metal resistors made of wire or ribbon, e.g. coiled, woven or formed as grids
- H01C3/14—Non-adjustable metal resistors made of wire or ribbon, e.g. coiled, woven or formed as grids the resistive element being formed in two or more coils or loops continuously wound as a spiral, helical or toroidal winding
- H01C3/20—Non-adjustable metal resistors made of wire or ribbon, e.g. coiled, woven or formed as grids the resistive element being formed in two or more coils or loops continuously wound as a spiral, helical or toroidal winding wound on cylindrical or prismatic base
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/20—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
- H05B3/34—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater flexible, e.g. heating nets or webs
- H05B3/36—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater flexible, e.g. heating nets or webs heating conductor embedded in insulating material
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/40—Heating elements having the shape of rods or tubes
- H05B3/42—Heating elements having the shape of rods or tubes non-flexible
- H05B3/46—Heating elements having the shape of rods or tubes non-flexible heating conductor mounted on insulating base
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/40—Heating elements having the shape of rods or tubes
- H05B3/54—Heating elements having the shape of rods or tubes flexible
- H05B3/56—Heating cables
- H05B3/565—Heating cables flat cables
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/002—Heaters using a particular layout for the resistive material or resistive elements
- H05B2203/003—Heaters using a particular layout for the resistive material or resistive elements using serpentine layout
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/017—Manufacturing methods or apparatus for heaters
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
- H05B2203/021—Heaters specially adapted for heating liquids
Abstract
A heater (10) for installation on a potable water tank (12). The heater (10) comprises a blanket (14) including an electrical resistance heating element (16) and a connection pad (18) for electrically connecting the heating element (16) to lead lines (20) to an aircraft power source (22). The water tank (12) is typically positioned under the cabin floor ar other locations on an aircraft which are susceptible to cold temperatures, moisture invasion, and pressure drops/rises caused by changing altitudes. The heater (10) maintains the tank (12) at an acceptable temperature range and prevents freezing of the water.
Description
HEATER FOR AIRCRAFT POTABLE WATER TANK
FIELD OF THE INVENTION
The present invention relates generally as indicated to a heater for an aircraft potable water tank and, more particularly, to a heater comprising a blanket with an electrical resistance heater element.
BACKGROUND OF THE INVENTION
An aircraft typically has one or more potable water tanks on board to accommodate the aircraft's plumbing system. Such water tanks are commonly.
cylindrical in shape and can range in size depending upon the aircraft and/or the number of tanks on board. In any event, a potable water tank is typically positioned under the cabin floor or other locations on the aircraft which are susceptible to cold temperatures, moisture invasion, and pressure drops/rises caused by changing altitudes.
A heater can be provided to maintain the tank at an acceptable water temperature range and to prevent freezing of the water. In one common type of heater, an electrothermal blanket is shaped and sized to be wrapped around the tank (with openings for plumbing inlets/outlets) and is secured to the tank with appropriately placed lacing hooks. The blanket includes a pattern of wire that forms an electrical resistance heating element connected to a power source on the aircraft to generate the desired heat.
To make the blanket for such a heater, a work platform is provided with pins placed in locations corresponding to the desired heating element pattern.
A
first layer of a carrier material having appropriately placed pin-accommodating openings is placed on the work platform. The heater wire is then wrapped around the pins to create the desired pattern, and a second layer of carrier material is then placed over the pattern so that the resistance wire is sandwiched therebetween. These and possibly other compiled layers are then cured to encapsulate the resistance wire.
A potable water tank is often made of an electrically conductive material, such as stainless steel or a graphite composition. Accordingly, or in any event, a heating assembly must be designed to guard against electrical shorts. To this end, the carrier layers in the heating blanket are made of an electrically insulating material such as silicone. As long as the carrier layers do not allow the introduction of water or moisture, the heating element circuit will remain electrically insulated.
In the past, heater blankets have incorporated Teflon-coated wire to protect against electrical shorts when a fluid (e.g., hydraulic oil) migrates through the silicone carrier layers. However, the "slickness" of the Teflon coating complicated assembly procedures, particularly the wire-winding process.
Specifically, the Teflon-coated wire would not "stick" to a silicon carrier layer (which has a clay-like consistency in an uncured state) during the winding process. To prevent the wire from "jumping" out of the pattern, small tie-down strips of silicone material had to be placed over winding paths throughout the pattern, dramatically slowing the process.
Moreover, the intactness of the Teflon coating was found to be difficult, if not impossible, to obtain during the manufacture of the heating element.
Specifically, pins on the work platform would crease or nick the Teflon coating, thereby providing a leakage path. Also, Teflon has a tendency to "cold flow"
around pin-imposed corners during the construction of the heating element.
Further, damage to the coating can occur from fingernails during handling of the coated wire. Accordingly, even with Teflon-coated wire, the integrity of the carrier layers remains crucial to keeping the heating element electrically insulated.
SUMMARY OF THE INVENTION
The present invention provides a heater assembly for a potable water tank wherein the heating element will remain electrically isolated regardless of the integrity of the carrier layers. In this manner, the invasion of moisture into the carrier layers will not affect the electrical insulation of the heating element.
FIELD OF THE INVENTION
The present invention relates generally as indicated to a heater for an aircraft potable water tank and, more particularly, to a heater comprising a blanket with an electrical resistance heater element.
BACKGROUND OF THE INVENTION
An aircraft typically has one or more potable water tanks on board to accommodate the aircraft's plumbing system. Such water tanks are commonly.
cylindrical in shape and can range in size depending upon the aircraft and/or the number of tanks on board. In any event, a potable water tank is typically positioned under the cabin floor or other locations on the aircraft which are susceptible to cold temperatures, moisture invasion, and pressure drops/rises caused by changing altitudes.
A heater can be provided to maintain the tank at an acceptable water temperature range and to prevent freezing of the water. In one common type of heater, an electrothermal blanket is shaped and sized to be wrapped around the tank (with openings for plumbing inlets/outlets) and is secured to the tank with appropriately placed lacing hooks. The blanket includes a pattern of wire that forms an electrical resistance heating element connected to a power source on the aircraft to generate the desired heat.
To make the blanket for such a heater, a work platform is provided with pins placed in locations corresponding to the desired heating element pattern.
A
first layer of a carrier material having appropriately placed pin-accommodating openings is placed on the work platform. The heater wire is then wrapped around the pins to create the desired pattern, and a second layer of carrier material is then placed over the pattern so that the resistance wire is sandwiched therebetween. These and possibly other compiled layers are then cured to encapsulate the resistance wire.
A potable water tank is often made of an electrically conductive material, such as stainless steel or a graphite composition. Accordingly, or in any event, a heating assembly must be designed to guard against electrical shorts. To this end, the carrier layers in the heating blanket are made of an electrically insulating material such as silicone. As long as the carrier layers do not allow the introduction of water or moisture, the heating element circuit will remain electrically insulated.
In the past, heater blankets have incorporated Teflon-coated wire to protect against electrical shorts when a fluid (e.g., hydraulic oil) migrates through the silicone carrier layers. However, the "slickness" of the Teflon coating complicated assembly procedures, particularly the wire-winding process.
Specifically, the Teflon-coated wire would not "stick" to a silicon carrier layer (which has a clay-like consistency in an uncured state) during the winding process. To prevent the wire from "jumping" out of the pattern, small tie-down strips of silicone material had to be placed over winding paths throughout the pattern, dramatically slowing the process.
Moreover, the intactness of the Teflon coating was found to be difficult, if not impossible, to obtain during the manufacture of the heating element.
Specifically, pins on the work platform would crease or nick the Teflon coating, thereby providing a leakage path. Also, Teflon has a tendency to "cold flow"
around pin-imposed corners during the construction of the heating element.
Further, damage to the coating can occur from fingernails during handling of the coated wire. Accordingly, even with Teflon-coated wire, the integrity of the carrier layers remains crucial to keeping the heating element electrically insulated.
SUMMARY OF THE INVENTION
The present invention provides a heater assembly for a potable water tank wherein the heating element will remain electrically isolated regardless of the integrity of the carrier layers. In this manner, the invasion of moisture into the carrier layers will not affect the electrical insulation of the heating element.
More particularly, the present invention provides a heater comprising a heating element and a carrier layer for the heating element. The heating element comprises a wire structure positioned in a pattern to generate required heating. The wire structure comprises an electrically conductive wire, an electrically insulating coating on the wire, and a fiber overwrap surrounding the insulating coating. The wire can be made of a metal or a metal alloy; the insulating coating can be made of polytetrafluoroethylene (Teflon); and the fiber overwrap can be made of nylon, rayon, polyester, polypropylene, polyvinylchloride, polyethylene and/or copolymers thereof.
The fiber overwrap serves to protect the electrically insulating coating, whereby the coating can remain intact before, during, and after the manufacture of a heater blanket. Specifically, the overwrap prevents pins on the work platform from nicking or creasing the coating during winding, eliminates "cold-flows" around pin-imposed corners, and guards against fingernail and other handling damage. By keeping the electrically insulating coating intact, the integrity of carrier layers is not crucial to the electrical insulation of the heating element. Additionally (or alternatively), the overwrap provides a surface for the uncured silicone to mechanically grip during the winding process. This significantly decreases wire-winding labor time. For example, a winding process which would have taken about six to seven hours with unwrapped Teflon-coated wire would take about one to two hours with the present invention.
The present invention also provides a crimp joint for between an end portion of the wire structure and a lead wire to a power source. The crimp joint comprises a crimp that electrically connects bare wire ends of the lead wire and the end portion of the wire structure, a first sleeve which protects the insulating coating on the end portion of the wire structure, and a second sleeve which surrounds the crimp and seals it relative to the insulating coating on the wire structure and the lead wire. Both of the sleeves have a dual wall construction comprising an outer wall and an inner wall. The outer wall is made of a Teflon-grade material which shrinks but does not melt when heated, and the inner wall is made of a Teflon-grade material which melts at a temperature near the melting point of the insulating coating for the wire. In this manner, sealing of the crimp can be accomplished by heating and "shrinking" the sleeve to thermally fuse it to the insulating coatings.
The wire structure and/or the crimp joint of the present invention are believed to provide adequate electrical insulation independent of other S components of-the heater. In other words, the wire structure and/or the crimp joint could satisfy electrical insulation requirements without having to be embedded or encapsulated further in an insulating medium. This greatly increases the ability of the heater to meet some rigorous requirements that conventional heaters could not even hope to satisfy. For example, a heater can be constructed according to the present invention that meets dielectric and insulation requirements during and after withstanding total immersion in a saltwater solution (i.e., waterproof) while undergoing seven vacuum cycles per day (to simulate altitude cycling of the aircraft) for a total duration of thirty days.
In one aspect, the invention provides a heater comprising a heating element and a carrier layer for the heating element, wherein the heating element comprises a wire structure positioned in a pattern to generate required heating, wherein:
the wire structure comprises an electrically conductive wire, an electrically insulating coating on the wire, and a fiber overwrap surrounding the insulating coating;
the heater further comprises a crimp joint between an end portion of the wire structure and a lead wire to a power source;
the crimp joint comprises a crimp, an electrically insulating first sleeve, and an electrically insulating second sleeve; and the crimp electrically connects bare wire ends of the lead wire and the end portion of the wire structure;
the first sleeve is positioned around an unwrapped section of the end portion of the wire structure; and the second sleeve surrounding the crimp, extends over the electrically insulating coating of the lead wire, over the electrically insulating coating of the end portion of the wire structure and over the first sleeve, and is thermally fused or bonded thereto and providing an electrically insulating sealing therefor.
These and other features of the invention are fully described and particularly pointed out in the claims. The following description and annexed drawings set forth in detail a certain illustrative embodiment of the invention, this embodiment being indicative of but one of the various ways in which the principles of the invention may be employed.
DRAWINGS
Figure 1 is a schematic view of a heater assembly according to the present invention installed on a potable water tank.
Figure 2 is a top view of the blanket of the heater assembly, with certain layers removed for purposes of explanation.
Figure 2A is an enlarged portion of Figure 2 showing a lead line connection pad.
Figures 3A - 3E are schematic. views of the steps of making a heater blanket according to the present invention.
Figure 4A is an enlarged top view of the wire used to form the resistance heating element.
Figure 4B is a sectional view as seen along lines 4B-4B in Figure 4A.
Figure 5 is an enlarged sectional view of a crimp joint.
4a Figure 5A is an enlarged side view of the shrink-wrap tube used in the crimp.
Figures 6A - 61 are schematic views showing the assembly of the crimp in the lead-line connection.
Figure 7 is a water tank incorporating the wire structure of the present invention.
Figure 7A is a schematic cross-section of the water tank shown in Figure 7.
Figure 8 is a turbine blade incorporating the wire structure of the present io invention.
DETAILED DESCRIPTION
Referring now to the drawings, and initially to Figure 1, a heater 10 according to the present invention is shown installed on a potable water tank 12.
The heater 10 comprises a blanket 14 including an electrical resistance heating element 16 and a connection pad 18 for electrically connecting the heating element 16 to lead lines 20 to an aircraft power source 22. The water tank 12 is typically positioned under the cabin floor or other locations on an aircraft which are susceptible to cold temperatures, moisture invasion, and pressure drops/rises caused by changing altitudes. The heater 10 maintains the tank 12 at an acceptable temperature range and prevents freezing of the water.
Referring now to Figure 2, the heater 10 is shown isolated from the water tank. The blanket 14 is shaped and sized to correspond to the geometry of the water tank 12 (Figure 1) whereby, in the illustrated embodiment, it has a roughly rectangular shape corresponding to the tank's cylindrical geometry. Openings 24 can be provided to fit around the tank's ports (e.g., inlet, outlet and/or pressurization ports), cut-outs 26 can be provided to accommodate the tank's mounting brackets, and/or lacing hooks 28 can be provided to attach the blanket 10 to the water tank.
The blanket 14 comprises an outer layer 30 of carrier material and an inner layer 32 of carrier material, and the heating element 16 is sandwiched therebetween. More layers of carrier material can be provided, if necessary, for a particular situation. It may be noted that with the present invention, the carrier material need not be electrically insulating (e.g., need not be silicone) as is required in conventional heating blankets for dielectric purposes. That being said, silicone could still be the preferred material for the carrier layers because it may have other advantageous properties (e.g., lightweight, flexible, thermally insulating, etc.) independent of electrical insulation.
The heating element 16 comprises a preferably continuous wire structure 34 arranged in a conventional multi-turn pattern of a desired density. As shown in more detail in Figure 2A, end sections 36 of the wire structure 34 pass through appropriately placed openings in the outer layer 30 to the connection to pad 18. The connection between the end sections 36 and the lead lines 20 is accomplished via two crimp joints 38. The lead wires 20 may be looped as shown and the loops, as well as the end sections 36, can be held in place with tie-down strips 40.
A method of making the blanket 14 is shown in Figures 3A - 3E. In the illustrated method, a work platform 42 is provided with pins 44 placed in locations corresponding to the desired heating element pattern. (Figure 3A.) It may be noted that the pattern formed by the pins 44 on the illustrated work platform 42 is much less complex and/or much less dense than would be found on most heating blankets. This pattern has been simplified in the schematic illustrations only for ease in explanation and is not representative of the complexity of expected heating element patterns.
One layer of carrier material (e.g., the outer layer 30) has appropriately placed pin-accommodating openings and is placed on the work platform 42.
(Figure 3B.) The wire structure 34 is then wrapped around the pins 44 to create the desired pattern. (Figure 3C.) Another layer of carrier material (e.g., the inner layer 32), also having appropriately placed pin-accommodating openings, is placed over the pattern so that the wire structure 34 is sandwiched between the two layers 30/32. (Figure 3D.) The compiled layers are then lifted from the work platform 42 (Figure 3E) and then cured in a suitable manner. If the blanket 14 is to include additional carrier layers, these layers can be added after the lifting step (Figure 3E) and before the curing step.
Referring now additionally to Figures 4A and 4B, the wire structure 34 is shown in detail. The wire structure 34 comprises an electrically conductive wire 50, an electrically insulating coating 52, and an overwrap 54. The wire 50 can be made of any suitable conductive material (e.g. a metal or a metal alloy) compatible with the intended use of the wire structure 34. For example, the wire 50 can be made from several (e.g., seven) alloy 90 strands of 34# AWG with a twist rate consistent with the required resistance.
The coating 52 can be made of any appropriate electrically insulating material which has the required flexibility to accommodate manufacturing techniques and/or installation. For example, the coating 52 can be made of Teflon (polytetrafluoroethylene), such as Grade 340 Teflon. Typically, the 1o coating 52 will have a nominal 0.005 inch wall thickness.
The overwrap 54 can be made of a fiber having, for example, a spiral wound or woven construction. The fiber can be selected from the group comprising nylon, rayon, polyester, polypropylene, polyvinylchloride, polyethylene and copolymers thereof. For example, the overwrap 54 can be constructed by double serve wrapping nylon fibers. Typically, the overwrap 54 will have a nominal 0.002 inch wall thickness.
The overwrap 54 serves to protect the electrically insulating coating 52, whereby the coating 52 remains intact before, during, and after the manufacture of the blanket 14. Specifically, the overwrap 54 prevents the pins 44 from nicking or creasing the coating 52, eliminates "cold-flows" around pin-imposed corners, and guards against fingernail and other handling damage before and during the manufacturing process. By keeping the electrically insulating coating 52 intact, the integrity of the carrier layers 30/32 is not crucial to the electrical insulation of the heating element 16.
In addition to protecting the coating 52, overwrap 54 also plays another important role during the construction or assembly of the heater 10. In the past, Teflon-coated wire would not "stick" to a silicone carrier layer (which has a clay-like consistency in an uncured state) during the winding process. To prevent the wire from "jumping" out of the pattern, small tie-down strips of silicone material 3o had to be placed over winding paths throughout the pattern, dramatically slowing the process. The construction of the present invention eliminates this problem, as the overwrap 54 provides a surface for the uncured silicone to mechanically grip during the winding process. This significantly decreases wire-winding labor time. For example, a winding process which would have taken about six to seven hours with unwrapped Teflon-coated wire would take about one to two hours with the present invention.
Referring now to Figure 5, one of the crimp joints 38 is shown in detail.
The crimp joint 38 comprises a crimp 60, a sleeve 62, and another sleeve 64.
The crimp 60 serves as the electrical connection between bare wire ends 66 and 68 of the lead wire 20 and the heater element end portion 36, respectively.
The sleeve 62 is positioned around an unwrapped section 70 of the end portion 36 (Le., with the coating 52 but not the overwrap 54) and is partially thermally fused 1o thereto. The sleeve 64 surrounds the crimp 60, extends over insulating coating 72 of the lead wire 20, over insulating coating 52 of the heater element end portion 36, and over the sleeve 62, and is thermally fused or bonded thereto.
As shown in Figure 5A, the sleeve 64 has a dual wall construction with an outer wall 74 and an inner wall 76. The outer wall 74 is made of a material which shrinks but does not melt when heated, and the inner wall 76 is made of a material which melts at a temperature near the melting point of the coating 52.
For example, the outer wall 74 can be made of PTFE grade of Teflon and, if the coating 52 is made of Grade 340 Teflon, the inner wall 76 can be made of FEP
grade Teflon. Such a product is manufactured and sold by Zeus Industrial Products under Vendor Part No. ZDS-L-130. The sleeve 62 can be made of a similar material but of a smaller diameter, sold by Zeus Industrial Products under Vendor Part No. ZDS-S-036. It may be noted that these sleeve materials also provide a flexible completed connection to accommodate curved installation situations and the flexible nature of silicone heaters.
Referring now to Figures 6A -61, a method of making the crimp joint 38 according to the present invention is shown. In this method, the wrapping 54 is trimmed off a distal section of the end portion 36 to form the unwrapped section 70. (Figure 6A.) The coating 52 is stripped from an end section of the unwrapped section 70 and insulating coating 72 is stripped from an end section of the lead wire 20 to expose bare wire ends 66 and 68. (Figure 6B.) The sleeve 62 is then placed on the unwrapped section 70 and the sleeve 64 is placed on the lead wire 20. (Figure 6C.) The bare wire ends 66 and 68 are then assembled with the crimp 60 with, in the illustrated embodiment, the bare wire end 68 being folded to fill the crimp's barrel. (Figure 6D.) The sleeve 64 is then slid over the crimp 60 and partially over the unwrapped section 70 and the sleeve 62. (Figure 6E.) A heat gun or other suitable device is then used to heat the sleeve 64.
The heating can start at the center of the crimp 60 (Figure 6F), move towards the lead wire 20, return towards the center of the crimp 60 (Figure 6G), and then move towards the end portion 36 (Figure 6H). This heating pattern causes the sleeve 64 to thermally bond or fuse to the lead wire 20, the heating element end portion 36, and the sleeve 62 and to shrink to seal the same. Significantly, the 1o heating purposely stops short of the end of the sleeve 62 so that a remote section of the sleeve 62 remains unheated (see Figure 61). In this manner, the sleeve 62, and particularly its unheated portion, acts as a heat shield to prevent the coating 52 on the unwrapped section 70 from being damaged (e.g., melted) during the heating of the sleeve 64.
The wire structure 34 and/or the crimp joint(s) 38 of the present invention are believed to provide adequate electrical insulation independent of other components of the heater 10. In other words, the wire structure 34 and/or the crimp joint 38 can satisfy electrical insulation requirements without having to be embedded or encapsulated further in an insulating medium. This greatly increases the ability of the heater 10 to meet some rigorous requirements that conventional heaters could not even hope to satisfy. For example, a heater can be constructed according to the present that meets dielectric and insulation requirements during and after withstanding total immersion in a saltwater solution while undergoing seven vacuum cycles per day (to simulate altitude cycling of the aircraft) for a total duration of thirty days. Thus, the heater can be constructed to be not only moisture resistant and/or water resistant, but to be also waterproof.
With particular reference to the wire structure 34, it has been discussed in detail with relation to the resistance heating element '16 within the blanket 14.
3o However, the "self-insulating property" of the wire structure 34 could allow the heater element 16 to be incorporated directly into a composite water tank 12, as shown in Figure 7, or structural composites in other applications. With conventional heater elements, dielectric layers on either side of the wire pattern would be required for electrical insulation purposes. This forms a heating element laminate. The layers in the laminate are typically made from epoxy/fiberglass materials, which are cured together while encapsulating the element in the center of the sandwich. In order to ensure the structural integrity of the tank or the composite structure, bonding or adhesion to these cured insulating layers is necessary to provide the appropriate load-carrying characteristics. In this case, the element laminate also has to be able to transfer the structural load through the composite matrix. With the wire structure 34 of the present invention, such dielectric layers (and the bonding of these layers to 1o rest of the tank) can be eliminated. As shown in Figure 7A, the wire structure 34 can simply be embedded, for example, in the graphite/epoxy composition without any insulating layers. This is done during the manufacturing of the composite tank. The wire structure is simply placed into the composite ply lay-up. The structural loads then pass around or in between the wire structure and there are not any bondlines to a laminate that require special bonding techniques. Furthermore, a composite structure without internal bondlines is inherently stronger and is less likely to structurally fail. As shown in Figure 8, for example, the wire structure 34 of the present invention could be incorporated into a fiberglass turbine blade 90.
Although the invention has been shown and described with respect to a certain preferred embodiment, it is evident that equivalent and obvious alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification. The present invention includes all such alterations and modifications and is limited only by the scope of the following claims.
The fiber overwrap serves to protect the electrically insulating coating, whereby the coating can remain intact before, during, and after the manufacture of a heater blanket. Specifically, the overwrap prevents pins on the work platform from nicking or creasing the coating during winding, eliminates "cold-flows" around pin-imposed corners, and guards against fingernail and other handling damage. By keeping the electrically insulating coating intact, the integrity of carrier layers is not crucial to the electrical insulation of the heating element. Additionally (or alternatively), the overwrap provides a surface for the uncured silicone to mechanically grip during the winding process. This significantly decreases wire-winding labor time. For example, a winding process which would have taken about six to seven hours with unwrapped Teflon-coated wire would take about one to two hours with the present invention.
The present invention also provides a crimp joint for between an end portion of the wire structure and a lead wire to a power source. The crimp joint comprises a crimp that electrically connects bare wire ends of the lead wire and the end portion of the wire structure, a first sleeve which protects the insulating coating on the end portion of the wire structure, and a second sleeve which surrounds the crimp and seals it relative to the insulating coating on the wire structure and the lead wire. Both of the sleeves have a dual wall construction comprising an outer wall and an inner wall. The outer wall is made of a Teflon-grade material which shrinks but does not melt when heated, and the inner wall is made of a Teflon-grade material which melts at a temperature near the melting point of the insulating coating for the wire. In this manner, sealing of the crimp can be accomplished by heating and "shrinking" the sleeve to thermally fuse it to the insulating coatings.
The wire structure and/or the crimp joint of the present invention are believed to provide adequate electrical insulation independent of other S components of-the heater. In other words, the wire structure and/or the crimp joint could satisfy electrical insulation requirements without having to be embedded or encapsulated further in an insulating medium. This greatly increases the ability of the heater to meet some rigorous requirements that conventional heaters could not even hope to satisfy. For example, a heater can be constructed according to the present invention that meets dielectric and insulation requirements during and after withstanding total immersion in a saltwater solution (i.e., waterproof) while undergoing seven vacuum cycles per day (to simulate altitude cycling of the aircraft) for a total duration of thirty days.
In one aspect, the invention provides a heater comprising a heating element and a carrier layer for the heating element, wherein the heating element comprises a wire structure positioned in a pattern to generate required heating, wherein:
the wire structure comprises an electrically conductive wire, an electrically insulating coating on the wire, and a fiber overwrap surrounding the insulating coating;
the heater further comprises a crimp joint between an end portion of the wire structure and a lead wire to a power source;
the crimp joint comprises a crimp, an electrically insulating first sleeve, and an electrically insulating second sleeve; and the crimp electrically connects bare wire ends of the lead wire and the end portion of the wire structure;
the first sleeve is positioned around an unwrapped section of the end portion of the wire structure; and the second sleeve surrounding the crimp, extends over the electrically insulating coating of the lead wire, over the electrically insulating coating of the end portion of the wire structure and over the first sleeve, and is thermally fused or bonded thereto and providing an electrically insulating sealing therefor.
These and other features of the invention are fully described and particularly pointed out in the claims. The following description and annexed drawings set forth in detail a certain illustrative embodiment of the invention, this embodiment being indicative of but one of the various ways in which the principles of the invention may be employed.
DRAWINGS
Figure 1 is a schematic view of a heater assembly according to the present invention installed on a potable water tank.
Figure 2 is a top view of the blanket of the heater assembly, with certain layers removed for purposes of explanation.
Figure 2A is an enlarged portion of Figure 2 showing a lead line connection pad.
Figures 3A - 3E are schematic. views of the steps of making a heater blanket according to the present invention.
Figure 4A is an enlarged top view of the wire used to form the resistance heating element.
Figure 4B is a sectional view as seen along lines 4B-4B in Figure 4A.
Figure 5 is an enlarged sectional view of a crimp joint.
4a Figure 5A is an enlarged side view of the shrink-wrap tube used in the crimp.
Figures 6A - 61 are schematic views showing the assembly of the crimp in the lead-line connection.
Figure 7 is a water tank incorporating the wire structure of the present invention.
Figure 7A is a schematic cross-section of the water tank shown in Figure 7.
Figure 8 is a turbine blade incorporating the wire structure of the present io invention.
DETAILED DESCRIPTION
Referring now to the drawings, and initially to Figure 1, a heater 10 according to the present invention is shown installed on a potable water tank 12.
The heater 10 comprises a blanket 14 including an electrical resistance heating element 16 and a connection pad 18 for electrically connecting the heating element 16 to lead lines 20 to an aircraft power source 22. The water tank 12 is typically positioned under the cabin floor or other locations on an aircraft which are susceptible to cold temperatures, moisture invasion, and pressure drops/rises caused by changing altitudes. The heater 10 maintains the tank 12 at an acceptable temperature range and prevents freezing of the water.
Referring now to Figure 2, the heater 10 is shown isolated from the water tank. The blanket 14 is shaped and sized to correspond to the geometry of the water tank 12 (Figure 1) whereby, in the illustrated embodiment, it has a roughly rectangular shape corresponding to the tank's cylindrical geometry. Openings 24 can be provided to fit around the tank's ports (e.g., inlet, outlet and/or pressurization ports), cut-outs 26 can be provided to accommodate the tank's mounting brackets, and/or lacing hooks 28 can be provided to attach the blanket 10 to the water tank.
The blanket 14 comprises an outer layer 30 of carrier material and an inner layer 32 of carrier material, and the heating element 16 is sandwiched therebetween. More layers of carrier material can be provided, if necessary, for a particular situation. It may be noted that with the present invention, the carrier material need not be electrically insulating (e.g., need not be silicone) as is required in conventional heating blankets for dielectric purposes. That being said, silicone could still be the preferred material for the carrier layers because it may have other advantageous properties (e.g., lightweight, flexible, thermally insulating, etc.) independent of electrical insulation.
The heating element 16 comprises a preferably continuous wire structure 34 arranged in a conventional multi-turn pattern of a desired density. As shown in more detail in Figure 2A, end sections 36 of the wire structure 34 pass through appropriately placed openings in the outer layer 30 to the connection to pad 18. The connection between the end sections 36 and the lead lines 20 is accomplished via two crimp joints 38. The lead wires 20 may be looped as shown and the loops, as well as the end sections 36, can be held in place with tie-down strips 40.
A method of making the blanket 14 is shown in Figures 3A - 3E. In the illustrated method, a work platform 42 is provided with pins 44 placed in locations corresponding to the desired heating element pattern. (Figure 3A.) It may be noted that the pattern formed by the pins 44 on the illustrated work platform 42 is much less complex and/or much less dense than would be found on most heating blankets. This pattern has been simplified in the schematic illustrations only for ease in explanation and is not representative of the complexity of expected heating element patterns.
One layer of carrier material (e.g., the outer layer 30) has appropriately placed pin-accommodating openings and is placed on the work platform 42.
(Figure 3B.) The wire structure 34 is then wrapped around the pins 44 to create the desired pattern. (Figure 3C.) Another layer of carrier material (e.g., the inner layer 32), also having appropriately placed pin-accommodating openings, is placed over the pattern so that the wire structure 34 is sandwiched between the two layers 30/32. (Figure 3D.) The compiled layers are then lifted from the work platform 42 (Figure 3E) and then cured in a suitable manner. If the blanket 14 is to include additional carrier layers, these layers can be added after the lifting step (Figure 3E) and before the curing step.
Referring now additionally to Figures 4A and 4B, the wire structure 34 is shown in detail. The wire structure 34 comprises an electrically conductive wire 50, an electrically insulating coating 52, and an overwrap 54. The wire 50 can be made of any suitable conductive material (e.g. a metal or a metal alloy) compatible with the intended use of the wire structure 34. For example, the wire 50 can be made from several (e.g., seven) alloy 90 strands of 34# AWG with a twist rate consistent with the required resistance.
The coating 52 can be made of any appropriate electrically insulating material which has the required flexibility to accommodate manufacturing techniques and/or installation. For example, the coating 52 can be made of Teflon (polytetrafluoroethylene), such as Grade 340 Teflon. Typically, the 1o coating 52 will have a nominal 0.005 inch wall thickness.
The overwrap 54 can be made of a fiber having, for example, a spiral wound or woven construction. The fiber can be selected from the group comprising nylon, rayon, polyester, polypropylene, polyvinylchloride, polyethylene and copolymers thereof. For example, the overwrap 54 can be constructed by double serve wrapping nylon fibers. Typically, the overwrap 54 will have a nominal 0.002 inch wall thickness.
The overwrap 54 serves to protect the electrically insulating coating 52, whereby the coating 52 remains intact before, during, and after the manufacture of the blanket 14. Specifically, the overwrap 54 prevents the pins 44 from nicking or creasing the coating 52, eliminates "cold-flows" around pin-imposed corners, and guards against fingernail and other handling damage before and during the manufacturing process. By keeping the electrically insulating coating 52 intact, the integrity of the carrier layers 30/32 is not crucial to the electrical insulation of the heating element 16.
In addition to protecting the coating 52, overwrap 54 also plays another important role during the construction or assembly of the heater 10. In the past, Teflon-coated wire would not "stick" to a silicone carrier layer (which has a clay-like consistency in an uncured state) during the winding process. To prevent the wire from "jumping" out of the pattern, small tie-down strips of silicone material 3o had to be placed over winding paths throughout the pattern, dramatically slowing the process. The construction of the present invention eliminates this problem, as the overwrap 54 provides a surface for the uncured silicone to mechanically grip during the winding process. This significantly decreases wire-winding labor time. For example, a winding process which would have taken about six to seven hours with unwrapped Teflon-coated wire would take about one to two hours with the present invention.
Referring now to Figure 5, one of the crimp joints 38 is shown in detail.
The crimp joint 38 comprises a crimp 60, a sleeve 62, and another sleeve 64.
The crimp 60 serves as the electrical connection between bare wire ends 66 and 68 of the lead wire 20 and the heater element end portion 36, respectively.
The sleeve 62 is positioned around an unwrapped section 70 of the end portion 36 (Le., with the coating 52 but not the overwrap 54) and is partially thermally fused 1o thereto. The sleeve 64 surrounds the crimp 60, extends over insulating coating 72 of the lead wire 20, over insulating coating 52 of the heater element end portion 36, and over the sleeve 62, and is thermally fused or bonded thereto.
As shown in Figure 5A, the sleeve 64 has a dual wall construction with an outer wall 74 and an inner wall 76. The outer wall 74 is made of a material which shrinks but does not melt when heated, and the inner wall 76 is made of a material which melts at a temperature near the melting point of the coating 52.
For example, the outer wall 74 can be made of PTFE grade of Teflon and, if the coating 52 is made of Grade 340 Teflon, the inner wall 76 can be made of FEP
grade Teflon. Such a product is manufactured and sold by Zeus Industrial Products under Vendor Part No. ZDS-L-130. The sleeve 62 can be made of a similar material but of a smaller diameter, sold by Zeus Industrial Products under Vendor Part No. ZDS-S-036. It may be noted that these sleeve materials also provide a flexible completed connection to accommodate curved installation situations and the flexible nature of silicone heaters.
Referring now to Figures 6A -61, a method of making the crimp joint 38 according to the present invention is shown. In this method, the wrapping 54 is trimmed off a distal section of the end portion 36 to form the unwrapped section 70. (Figure 6A.) The coating 52 is stripped from an end section of the unwrapped section 70 and insulating coating 72 is stripped from an end section of the lead wire 20 to expose bare wire ends 66 and 68. (Figure 6B.) The sleeve 62 is then placed on the unwrapped section 70 and the sleeve 64 is placed on the lead wire 20. (Figure 6C.) The bare wire ends 66 and 68 are then assembled with the crimp 60 with, in the illustrated embodiment, the bare wire end 68 being folded to fill the crimp's barrel. (Figure 6D.) The sleeve 64 is then slid over the crimp 60 and partially over the unwrapped section 70 and the sleeve 62. (Figure 6E.) A heat gun or other suitable device is then used to heat the sleeve 64.
The heating can start at the center of the crimp 60 (Figure 6F), move towards the lead wire 20, return towards the center of the crimp 60 (Figure 6G), and then move towards the end portion 36 (Figure 6H). This heating pattern causes the sleeve 64 to thermally bond or fuse to the lead wire 20, the heating element end portion 36, and the sleeve 62 and to shrink to seal the same. Significantly, the 1o heating purposely stops short of the end of the sleeve 62 so that a remote section of the sleeve 62 remains unheated (see Figure 61). In this manner, the sleeve 62, and particularly its unheated portion, acts as a heat shield to prevent the coating 52 on the unwrapped section 70 from being damaged (e.g., melted) during the heating of the sleeve 64.
The wire structure 34 and/or the crimp joint(s) 38 of the present invention are believed to provide adequate electrical insulation independent of other components of the heater 10. In other words, the wire structure 34 and/or the crimp joint 38 can satisfy electrical insulation requirements without having to be embedded or encapsulated further in an insulating medium. This greatly increases the ability of the heater 10 to meet some rigorous requirements that conventional heaters could not even hope to satisfy. For example, a heater can be constructed according to the present that meets dielectric and insulation requirements during and after withstanding total immersion in a saltwater solution while undergoing seven vacuum cycles per day (to simulate altitude cycling of the aircraft) for a total duration of thirty days. Thus, the heater can be constructed to be not only moisture resistant and/or water resistant, but to be also waterproof.
With particular reference to the wire structure 34, it has been discussed in detail with relation to the resistance heating element '16 within the blanket 14.
3o However, the "self-insulating property" of the wire structure 34 could allow the heater element 16 to be incorporated directly into a composite water tank 12, as shown in Figure 7, or structural composites in other applications. With conventional heater elements, dielectric layers on either side of the wire pattern would be required for electrical insulation purposes. This forms a heating element laminate. The layers in the laminate are typically made from epoxy/fiberglass materials, which are cured together while encapsulating the element in the center of the sandwich. In order to ensure the structural integrity of the tank or the composite structure, bonding or adhesion to these cured insulating layers is necessary to provide the appropriate load-carrying characteristics. In this case, the element laminate also has to be able to transfer the structural load through the composite matrix. With the wire structure 34 of the present invention, such dielectric layers (and the bonding of these layers to 1o rest of the tank) can be eliminated. As shown in Figure 7A, the wire structure 34 can simply be embedded, for example, in the graphite/epoxy composition without any insulating layers. This is done during the manufacturing of the composite tank. The wire structure is simply placed into the composite ply lay-up. The structural loads then pass around or in between the wire structure and there are not any bondlines to a laminate that require special bonding techniques. Furthermore, a composite structure without internal bondlines is inherently stronger and is less likely to structurally fail. As shown in Figure 8, for example, the wire structure 34 of the present invention could be incorporated into a fiberglass turbine blade 90.
Although the invention has been shown and described with respect to a certain preferred embodiment, it is evident that equivalent and obvious alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification. The present invention includes all such alterations and modifications and is limited only by the scope of the following claims.
Claims (13)
1. A heater comprising a heating element and a carrier layer for the heating element, wherein the heating element comprises a wire structure positioned in a pattern to generate required heating, wherein:
the wire structure comprises an electrically conductive wire, an electrically insulating coating on the wire, and a fiber overwrap surrounding the insulating coating;
the heater further comprises a crimp joint between an end portion of the wire structure and a lead wire to a power source;
the crimp joint comprises a crimp, an electrically insulating first sleeve, and an electrically insulating second sleeve; and the crimp electrically connects bare wire ends of the lead wire and the end portion of the wire structure;
the first sleeve is positioned around an unwrapped section of the end portion of the wire structure; and the second sleeve surrounding the crimp, extends over the electrically insulating coating of the lead wire, over the electrically insulating coating of the end portion of the wire structure and over the first sleeve, and is thermally fused or bonded thereto and providing an electrically insulating sealing therefor.
the wire structure comprises an electrically conductive wire, an electrically insulating coating on the wire, and a fiber overwrap surrounding the insulating coating;
the heater further comprises a crimp joint between an end portion of the wire structure and a lead wire to a power source;
the crimp joint comprises a crimp, an electrically insulating first sleeve, and an electrically insulating second sleeve; and the crimp electrically connects bare wire ends of the lead wire and the end portion of the wire structure;
the first sleeve is positioned around an unwrapped section of the end portion of the wire structure; and the second sleeve surrounding the crimp, extends over the electrically insulating coating of the lead wire, over the electrically insulating coating of the end portion of the wire structure and over the first sleeve, and is thermally fused or bonded thereto and providing an electrically insulating sealing therefor.
2. The heater according to claim 1, wherein:
the second sleeve has a dual wall construction with an outer wall and an inner wall;
the outer wall is made of a material which shrinks but does not melt when heated; and the inner wall is made of a material which melts at a temperature near the melting point of the insulating coating on the wire structure.
the second sleeve has a dual wall construction with an outer wall and an inner wall;
the outer wall is made of a material which shrinks but does not melt when heated; and the inner wall is made of a material which melts at a temperature near the melting point of the insulating coating on the wire structure.
3. The heater according to claim 1 or 2, wherein the first sleeve is partially thermally fused to the insulating coating of the end portion of the wire structure.
4. The heater according to claim 2 or 3, wherein:
the first sleeve has a dual wall construction with an outer wall and an inner wall;
wherein the outer wall is made of a material which shrinks but does not melt when heated; and wherein the inner wall is made of a material which melts at a temperature near the melting point of the insulating coating on the wire structure.
the first sleeve has a dual wall construction with an outer wall and an inner wall;
wherein the outer wall is made of a material which shrinks but does not melt when heated; and wherein the inner wall is made of a material which melts at a temperature near the melting point of the insulating coating on the wire structure.
5. The heater according to any one of claims 1 to 4, wherein the insulating coating of the wire structure is made of polytetrafluoroethylene.
6. The heater according to any one of claims 1 to 5, wherein the overwrap comprises a fiber made of nylon, rayon, polyester, polypropylene, polyvinylchloride, polyethylene, or copolymers thereof, or combinations thereof.
7. The heater according to any one of claims 1 to 6, comprising a further carrier layer and wherein the heating element is sandwiched between the carrier layers.
8. The heater according to any one of claims 1 to 7, wherein the carrier layer(s) is/are made of silicone.
9. A method of making the heater defined in any one of claims 1 to 8, said method comprising the step of positioning the wire structure on the carrier layer(s) in the pattern.
10. The method according to claim 9, wherein said positioning step comprises providing a work platform with pins placed in locations corresponding to the pattern and wrapping the wire structure around the pins to create the pattern.
11. A method of making the crimp joint of the heater defined in any one of claims 1 to 8, said method comprising the steps of:
12 trimming the fabric overwrap of a distal section of the end portion of the wire structure to form an unwrapped section;
stripping the insulating coating from the end of the unwrapped section and stripping insulating coating from the lead wire to expose bare wire ends;
assembling the bare wire ends in the crimp;
positioning the electrically insulating first sleeve on the unwrapped section;
positioning the electrically insulating second sleeve around the crimp, over the insulating coating of the lead wire, over the insulating coating of the end portion of the wire structure and over the first sleeve; and heating the second sleeve to thermally bond it to the insulating coating of the lead wire, the insulating coating of the end portion of the wire structure and the first sleeve while leaving a remote portion of the first sleeve unheated to prevent the insulating coating on the end portion of the wire structure from being damaged during the heating of the first sleeve.
12. A tank and the heater defined in any one of claims I to 8, wrapped around the tank.
stripping the insulating coating from the end of the unwrapped section and stripping insulating coating from the lead wire to expose bare wire ends;
assembling the bare wire ends in the crimp;
positioning the electrically insulating first sleeve on the unwrapped section;
positioning the electrically insulating second sleeve around the crimp, over the insulating coating of the lead wire, over the insulating coating of the end portion of the wire structure and over the first sleeve; and heating the second sleeve to thermally bond it to the insulating coating of the lead wire, the insulating coating of the end portion of the wire structure and the first sleeve while leaving a remote portion of the first sleeve unheated to prevent the insulating coating on the end portion of the wire structure from being damaged during the heating of the first sleeve.
12. A tank and the heater defined in any one of claims I to 8, wrapped around the tank.
13. The tank and the heater according to claim 12, wherein the tank is a potable water tank for an aircraft.
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US37972102P | 2002-05-10 | 2002-05-10 | |
US60/379,721 | 2002-05-10 |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT202100015587A1 (en) * | 2021-06-15 | 2022-12-15 | Alfonso Sacco | AIRCRAFT INCLUDING A SYSTEM AND PROCEDURE FOR THE STORAGE OF WATER WITHDRAWN FROM THE ATMOSPHERIC ENVIRONMENT |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7785760B2 (en) * | 2006-01-18 | 2010-08-31 | Ricoh Company Limited | Toner and method of preparing the toner |
US7621239B2 (en) * | 2006-06-16 | 2009-11-24 | Rice Allen C | Hot water heater blanket assembly establishing dead air spaces |
CN101132657B (en) * | 2007-09-21 | 2011-09-21 | 赵永镐 | Polytetrafluoroethylene heating product and method of manufacturing the same |
US8074933B2 (en) * | 2008-02-26 | 2011-12-13 | Goodrich Corporation | Aircraft graywater ejection system |
JP5541901B2 (en) * | 2009-10-30 | 2014-07-09 | 矢崎総業株式会社 | Water-stop treatment method and insulated coated wire |
TWM384453U (en) * | 2010-03-02 | 2010-07-11 | Winharbor Technology Co Ltd | Pull-resistant illuminating/heat generating structure capable of being charged in wireless manner |
FR2958991B1 (en) | 2010-04-14 | 2012-05-04 | Total Sa | DRIVE FOR TRANSPORTING A FLUID COMPRISING HYDROCARBON, AND METHOD OF MANUFACTURING SUCH A DRIVE. |
FR2958992B1 (en) | 2010-04-14 | 2012-05-04 | Total Sa | DRIVE FOR TRANSPORTING A FLUID COMPRISING HYDROCARBON, AND METHOD FOR MANUFACTURING THE SAME. |
FR2958995B1 (en) | 2010-04-14 | 2012-05-04 | Total Sa | HEATING DEVICE FOR A TRANSPARENT DEVICE FOR A FLUID COMPRISING A HYDROCARBON |
FR2958994B1 (en) * | 2010-04-14 | 2013-01-11 | Total Sa | HEATED COVER FOR A DEVICE FOR TRANSPORTING A FLUID COMPRISING A HYDROCARBON. |
GB2493350B (en) * | 2011-08-01 | 2019-01-09 | Osborne Andre | Method of heating diving bell external gas reclaim condensate water trap and check valve assembly to prevent freezing |
US9346550B2 (en) * | 2012-12-05 | 2016-05-24 | Mesoscribe Technologies, Inc. | Ice detection and mitigation device |
US10948217B2 (en) * | 2013-01-08 | 2021-03-16 | Alex Harel | Water supply and heating system with flexible tank and heating carpet |
IL224132A (en) * | 2013-01-08 | 2017-04-30 | Harel Alex | Supplying and heating water system comprising flexible tank and heating system |
US9316412B2 (en) | 2014-04-25 | 2016-04-19 | Goodrich Corporation | High capacity water heater |
US9909933B2 (en) * | 2014-12-09 | 2018-03-06 | Kidde Technologies, Inc. | Eutectic based continuous thermal sensing element including fiber wrapped center conductor |
EP3325867B1 (en) | 2015-07-22 | 2021-06-02 | National Machine Group | Hot water tank |
US10118361B2 (en) * | 2016-01-22 | 2018-11-06 | United Technologies Corporation | Thermal insulation |
US10425993B2 (en) * | 2016-12-08 | 2019-09-24 | Goodrich Corporation | Carbon nanotube yarn heater |
KR102157476B1 (en) * | 2018-02-14 | 2020-09-21 | (주)알파플러스 | Heater and insulator assembly for vacuum effusion cell |
IL261096A (en) * | 2018-08-10 | 2020-02-27 | Ez Pack Water Ltd | System and Method for Storage of Renewable Energy as Hot or Cold Water in Flexible Heating Tanks |
US11274853B2 (en) | 2018-10-15 | 2022-03-15 | Goodrich Corporation | Additively manufactured heaters for water system components |
US20230373632A1 (en) * | 2022-05-18 | 2023-11-23 | Goodrich Corporation | High-efficient silicone heater |
Family Cites Families (47)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US391971A (en) * | 1888-10-30 | Ticut | ||
US2564325A (en) * | 1946-04-04 | 1951-08-14 | Goodrich Co B F | Heated propeller covering |
US2786211A (en) * | 1955-02-09 | 1957-03-26 | Wrought Iron Range Company | Self-serving sink |
US3525799A (en) * | 1968-05-17 | 1970-08-25 | Raychem Corp | Heat recoverable connector |
US3702910A (en) * | 1971-03-24 | 1972-11-14 | Simmonds Precision Products | Magnetic float point sensor for high pressure containers |
US3832231A (en) * | 1972-08-21 | 1974-08-27 | Gen Electric | Method of rendering chlorosulfonated polyethylene rubber resistant to adherence of dirt,and the dirt resisting products thereof |
US4045611A (en) * | 1975-09-30 | 1977-08-30 | Belden Corporation | Hermetic lead wire |
US4037083A (en) * | 1976-05-05 | 1977-07-19 | Leavines Joseph E | High temperature parallel resistance pipe heater |
DE7711222U1 (en) * | 1977-04-09 | 1977-07-21 | Felten & Guilleaume Carlswerk Ag, 5000 Koeln | ELECTRIC HEATING MAT |
US4412898A (en) * | 1980-08-26 | 1983-11-01 | The B.F. Goodrich Company | Process for chlorination of PVC in water without use of swelling agents |
DE3041657A1 (en) * | 1980-11-05 | 1982-06-03 | HEW-Kabel Heinz Eilentropp KG, 5272 Wipperfürth | METHOD AND DEVICE FOR PRODUCING TENSILE AND PRESSURE SEAL, IN PARTICULAR TEMPERATURE-RESISTANT, CONNECTIONS FOR ELECTRICAL CABLES AND CABLES |
US4460472A (en) * | 1981-01-06 | 1984-07-17 | The B. F. Goodrich Company | Scale inhibitor for reverse osmosis water purification system |
US4553023A (en) * | 1981-11-27 | 1985-11-12 | Nordson Corporation | Thermally insulated electrically heated hose for transmitting hot liquids |
US4468557A (en) * | 1983-02-03 | 1984-08-28 | Bylin Heating Systems, Inc. | Conformable electric heating apparatus |
SE8305245L (en) * | 1983-09-28 | 1985-03-29 | Autopart Sweden Ab | VERMEDYNA, SPECIAL FOR THE VEHICLE SEAT |
US4566973A (en) * | 1984-08-06 | 1986-01-28 | The B. F. Goodrich Company | Scale inhibition in water systems |
US4869905A (en) * | 1987-05-12 | 1989-09-26 | The B. F. Goodrich Company | Method of making and a slow release composition for abating acid water formation |
US5032290A (en) * | 1988-09-08 | 1991-07-16 | Nihonkensetsu Kogyo Co., Ltd. | Method and system of water supply for a building construction |
US4969991A (en) * | 1989-08-30 | 1990-11-13 | Valadez Gerardo M | Water purifying and dispensing system |
US5303739A (en) * | 1991-09-30 | 1994-04-19 | Deutsche Aerospace Airbus Gmbh | Fresh water supply system for an aircraft |
US5309938A (en) * | 1991-09-30 | 1994-05-10 | Deutsche Aerospace Airbus Gmbh | Fresh water supply system for an aircraft |
SE469413B (en) * | 1991-11-22 | 1993-07-05 | Electrolux Ab | ENERGY AND WATER SAVING SHOWER |
US5393932A (en) * | 1992-02-14 | 1995-02-28 | Minnesota Mining And Manufacturing Company | Wire connector |
US5290996A (en) | 1992-02-21 | 1994-03-01 | The B. F. Goodrich Company | Modular drainmast for aircraft |
US5552576A (en) * | 1992-02-21 | 1996-09-03 | The Bf Goodrich Company | Modular drainmast for aircraft |
US5351337A (en) * | 1992-09-25 | 1994-09-27 | Deutsch Joseph J | Self-contained pressurized water delivery system |
US5468314A (en) * | 1993-02-26 | 1995-11-21 | W. L. Gore & Associates, Inc. | Process for making an electrical cable with expandable insulation |
GB9309816D0 (en) * | 1993-05-12 | 1993-06-23 | Raychem Ltd | Electrical connection |
DE4328207A1 (en) * | 1993-08-21 | 1995-02-23 | Stiebel Eltron Gmbh & Co Kg | Termination of an electric tubular heater |
DE4403067C1 (en) * | 1994-02-02 | 1995-04-06 | Deutsche Aerospace Airbus | Device for keeping liquid pipelines, which are open at one end, free of ice |
JP3006758U (en) * | 1994-05-13 | 1995-01-31 | 帝人株式会社 | Road heater |
WO1996039006A1 (en) * | 1995-05-29 | 1996-12-05 | R-Amtech International, Inc. | Elongated flexible electrical heater and a method of manufacturing it |
DE19546511A1 (en) * | 1995-12-13 | 1997-06-19 | Eilentropp Kg | Polymer mixture and its use for high temperature resistant fasteners and sealing elements |
US5658465A (en) * | 1995-12-28 | 1997-08-19 | The B.F. Goodrich Company | Method for inhibiting the deposition of silica and silicate compounds in water systems |
USD391971S (en) | 1996-05-17 | 1998-03-10 | Stevens-Lee Company | Refrigerated milk dispenser |
US5883363A (en) * | 1996-08-12 | 1999-03-16 | Nichias Corporation | Heating mantle and method for fabricating the same |
US5675880A (en) | 1996-08-29 | 1997-10-14 | Bethlehem Steel Corporation | Descaling system for use in the manufacture of steel and corresponding method |
US5938078A (en) | 1997-05-09 | 1999-08-17 | Stevens-Lee Company | Valve for beverage dispenser |
DE19726418A1 (en) * | 1997-06-23 | 1999-01-28 | Daimler Benz Aerospace Airbus | Heating conductor connection system |
US6463956B2 (en) | 1998-09-29 | 2002-10-15 | International Water-Guard Industries Inc. | Method of water distribution and apparatus therefor |
US6211494B1 (en) | 1999-08-25 | 2001-04-03 | The B. F. Goodrich Company | Drainmast with integral electronic temperature control |
DE19948819C2 (en) * | 1999-10-09 | 2002-01-24 | Airbus Gmbh | Heating conductor with a connection element and / or a termination element and a method for producing the same |
US6412344B1 (en) | 1999-11-15 | 2002-07-02 | Rosemount Aerospace Inc. | Fluid level sensor with dry couplant |
JP2001267048A (en) * | 2000-01-11 | 2001-09-28 | Tsuneji Sasaki | Insulation method of carbon filament and coaxial treatment of carbon filament and conductive wire |
US6609679B1 (en) | 2000-11-24 | 2003-08-26 | Rosemount Aerospace Inc. | Component mounting permitting one hand installation |
US6615657B2 (en) | 2001-01-04 | 2003-09-09 | Rosemount Aerospace, Inc. | Built-in test procedure for non-intrusive ultrasonic level sensing |
US6738566B2 (en) * | 2001-07-03 | 2004-05-18 | Nordson Corporation | Insulated hose for transmitting hot liquids |
-
2003
- 2003-05-09 US US10/434,649 patent/US20030210902A1/en not_active Abandoned
- 2003-05-09 DE DE60333323T patent/DE60333323D1/en not_active Expired - Lifetime
- 2003-05-09 EP EP03252919A patent/EP1367859B1/en not_active Expired - Fee Related
- 2003-05-12 CA CA2428530A patent/CA2428530C/en not_active Expired - Fee Related
-
2007
- 2007-01-10 US US11/621,681 patent/US7277628B2/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT202100015587A1 (en) * | 2021-06-15 | 2022-12-15 | Alfonso Sacco | AIRCRAFT INCLUDING A SYSTEM AND PROCEDURE FOR THE STORAGE OF WATER WITHDRAWN FROM THE ATMOSPHERIC ENVIRONMENT |
Also Published As
Publication number | Publication date |
---|---|
US7277628B2 (en) | 2007-10-02 |
US20070127900A1 (en) | 2007-06-07 |
EP1367859A3 (en) | 2007-10-17 |
CA2428530A1 (en) | 2003-11-10 |
EP1367859A2 (en) | 2003-12-03 |
US20030210902A1 (en) | 2003-11-13 |
DE60333323D1 (en) | 2010-08-26 |
EP1367859B1 (en) | 2010-07-14 |
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Effective date: 20210512 |