WO2006029496A1 - Flow enhancement for underwater turbine generator - Google Patents

Flow enhancement for underwater turbine generator Download PDF

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Publication number
WO2006029496A1
WO2006029496A1 PCT/CA2005/000267 CA2005000267W WO2006029496A1 WO 2006029496 A1 WO2006029496 A1 WO 2006029496A1 CA 2005000267 W CA2005000267 W CA 2005000267W WO 2006029496 A1 WO2006029496 A1 WO 2006029496A1
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WO
WIPO (PCT)
Prior art keywords
turbine
hub
improvement
area
flow
Prior art date
Application number
PCT/CA2005/000267
Other languages
French (fr)
Inventor
Russell Stothers
Emmanuel Grillos
Original Assignee
Clean Current Power Systems Incorporated
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 Clean Current Power Systems Incorporated filed Critical Clean Current Power Systems Incorporated
Priority to JP2007531548A priority Critical patent/JP2008513650A/en
Priority to EP05714509A priority patent/EP1789676A1/en
Priority to AU2005284617A priority patent/AU2005284617B2/en
Priority to NZ553511A priority patent/NZ553511A/en
Priority to CA002549376A priority patent/CA2549376C/en
Priority to CN2005800313363A priority patent/CN101023264B/en
Priority to US11/663,001 priority patent/US7874788B2/en
Publication of WO2006029496A1 publication Critical patent/WO2006029496A1/en
Priority to NO20071909A priority patent/NO20071909L/en
Priority to US12/976,338 priority patent/US20110115228A1/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B17/00—Other machines or engines
    • F03B17/06—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head"
    • F03B17/061—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially in flow direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/04—Machines or engines of reaction type; Parts or details peculiar thereto with substantially axial flow throughout rotors, e.g. propeller turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/12—Blades; Blade-carrying rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/16—Stators
    • F03B3/18—Stator blades; Guide conduits or vanes, e.g. adjustable
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/10—Stators
    • F05B2240/12—Fluid guiding means, e.g. vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/10—Stators
    • F05B2240/13—Stators to collect or cause flow towards or away from turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/10—Stators
    • F05B2240/14—Casings, housings, nacelles, gondels or the like, protecting or supporting assemblies there within
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/90—Mounting on supporting structures or systems
    • F05B2240/97—Mounting on supporting structures or systems on a submerged structure
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/20—Hydro energy
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/30—Energy from the sea, e.g. using wave energy or salinity gradient
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/905—Natural fluid current motor
    • Y10S415/908—Axial flow runner

Definitions

  • the present invenj ⁇ on relates generally to underwater ducted turbines for hydrokinetic electrical power generation. More specifically, a dual augmentor duct structure defining a ⁇ slot and a longitudinal hole through the hub of the turbine which enhances water.ilow are disclosed.
  • Bi-directional, rim generating, ducted underwater turbines for generating electrical power are known, such as the applicant's PCT application PCT/CA02/01413 to Davis et al. There is a desire to improve the flow characteristics, and therefore, the efficiency of such designs. Fixed augmentors are known to increase flow through the turbine.
  • United States Patent 4,219,303 to Mouton et al. disclosed a rigid inner primary nozzle within a flexible outer nozzle which slightly overlaps the primary nozzle, creating a space between the nozzles for uni-directional flow.
  • United States Patent 6,406,251Bl to Vauthier disclosed a mechanically complicated and inefficient system of pivoting flaps on the exterior surface of a hydroturbine accepting bi-directional flow.
  • United States Patent RE38,336E (Reissue of 5,592,816) to Williams disclosed a hydroelectric turbine with a central open area of unrestricted flow surrounded by the blades which proposed reducing down current turbulence.
  • United States Patent 6,648,589B2 also to Williams, disclosed a hydroelectric turbine with a central open area of unrestricted flow surrounded by the blades to aid in increasing the velocity of the water flowing through the single blade and to eliminate the turbulence that occurs behind the hub in traditional hub generator hydroelectric turbines.
  • the Williams patents employ complicated hydraulic and mechanically driven generators with a uni-directional turbine blade configuration without ducting nor hydrodynamic structures to direct water flow in an efficient manner.
  • the Williams patents do not incorporate a set of bearings at the hub to improve the structural integrity of the unit and reduce blade deflection.
  • the present invention satisfies the need for a structurally and mechanically simple and inexpensive to manufacture flow enhancement design which increases water flow, provides a bypass for sea life and debris thereby reducing the environmental impact of the unit, reduces vibration and hydrodynamic drag and increases the operating efficiency of underwater ducted turbines.
  • the augmentor device optimally has an inlet and an outlet which are substantially similar in area and a narrower central throat portion, thereby increasing the efficiency of the turbine.
  • Specific optimal ratios of the throat area, slot area and the blade area to the inlet area are disclosed which further optimize the efficiency of the turbine.
  • the augmentor may be partial, or a complete second duct disposed about substantially all of the outer surface of the first duct, thereby creating a dual duct structure.
  • Another object of the present invention is to provide an augmentor which is axi-symmetric, with leading edges having hydrodynamic profiles, thereby minimizing turbulent water flow past the inlet and outlet and performing optimally in bi-directional water flow.
  • the dual duct structure may be coated with an anti- fouling coating and may include buoyancy material, thereby achieving greater noise suppression, ensuring minimal environmental impact and providing corrosion resistance and high lubricity.
  • Another object of the present invention is to provide a flow enhancement structure in a turbine comprising a longitudinal hole substantially along the longitudinal axis of the turbine in a hub having specific shape, structural and material characteristics, thereby improving the efficiency of the turbine. Specific ratios of the hole area to the blade area are disclosed. The hole, combined with the flow characteristics of the hub, renders the turbine safe in relation to marine life.
  • FIG. 1 is an isometric view of the dual augmentor duct underwater turbine generator with slot and hollow hub flow enhancement structures according to the invention.
  • FIG. 2 is a front elevation view of the dual duct underwater turbine generator with slot and hollow hub flow enhancement structures according to the invention.
  • FIG. 3 is a cut-away perspective view of the dual augmentor duct underwater turbine generator with slot and hollow hub flow enhancement structures according to the invention.
  • FIG. 4 is a side elevation sectional view of the hub and outer and augmentor ducts defining the slot and hole and showing flow streamlines according to the invention.
  • FIG. 5 is a side elevation detail view of the leading edges of the hollow hub and outer augmentor ducts.
  • FIG. 6 is a side elevation sectional view of a dual augmentor duct open slot variation of the invention.
  • FIG. 7 is a side elevation sectional view of a cylindrical dual augmentor duct slot variation of the invention.
  • the underwater ducted turbine 10 is of the type disclosed in the applicants' earlier invention the subject of PCT/CA02/01413 application to Davis et al., with the present improvement being directed towards a hollow hub 20 design and second, augmentor duct 41 disposed about the outer duct 40 with a slot 200 between the two ducts 43, which together enhance water flow 100 and increase efficiency of the turbine generator 10.
  • the dual augmentor duct structure 43 is a fore and aft symmetric structure, namely it is symmetrical about a central vertical plane which transects the turbine generator 10 laterally.
  • the dual duct structure 43 is disposed about the turbine rotor 50 and all generator components which are housed in the outer duct 40.
  • the augmentor duct 41 has symmetrical inlet portions 45 and 46 creating a highly efficient duct for bi-directional flow.
  • the central hole 240 may also be employed in units 10 without a hub, for instance with cantilevered blades disposed radially towards a central portion of the turbine generator.
  • the central hole 240 may also be employed in non-ducted turbine generators 10.
  • the dual duct structure 43 is secured to the hub 20 by a plurality of struts 24 which also act as guide vanes in the annulus 51 area.
  • the struts 24 are merely struts in the slot 200 area and not curved guide vanes. In the preferred embodiment there are five guide vanes 24 at each of the two ends of the turbine generator 10.
  • the vanes 24 are preferably evenly spaced radially about the hub 20 axis.
  • two counter-rotating rotor disks 50 are rotatably attached to the hub 20 and a plurality of blades 30, optimally symmetric hydrofoil blades, extend radially from said hub 20 to a rotor rim 54 which seats in a groove (not shown) in the interior surface of the outer duct 40 and is rotatable in a bearing race, or in a variation, a magnet bearing race.
  • a rotor rim 54 which seats in a groove (not shown) in the interior surface of the outer duct 40 and is rotatable in a bearing race, or in a variation, a magnet bearing race.
  • single or multiple rotor disks 50 may be employed.
  • the flow enhancement slot 200 and hole 240 structures may be employed not only for tidal applications, but also for other turbine generation applications, as one skilled in the art can appreciate.
  • the dual augmentor duct 43 is a rigid structure manufactured from composite material.
  • the dual augmentor duct 43 may be made from any composite material such as fiberglass, KevlarTM, carbon fiber, fiber- reinforced concrete or any other combination known in the art.
  • Advantages of the rigid, symmetrical dual duct 43 arrangement include simplicity of manufacture, installation and maintenance and low capital cost.
  • a stainless steel rigid frame covered by a flexible composite material is used.
  • the interior wall of the augmentor duct 41 diverges towards the augmentor duct rim 62, thereby producing a decelerating effect downstream of the turbine blades as the water 100 flows through the duct 20.
  • the outer surface of the augmentor duct 41 is concave in the preferred embodiment, but may be convex or cylindrical. Both ends of the dual augmentor duct 43 are effectively inlets as the turbine generator 10 is bidirectional.
  • the central portion of the augmentor duct 41 is cylindrical. In operation, water flow 100 converges as it passes the inlet rim 62 and follows the profile of the augmentor duct 41 and outer duct 40.
  • the gap or slot 200 between the outer duct 40 and augmentor ducts 41 is a smooth annular flow area.
  • the blade tips 30 and rotor rim 54 are contained in annulus 51 and are not disposed in the slot 200.
  • the outer duct 40 and augmentor duct 41 diverge again, to allow for the smooth diffusion of the water flow 100 back to free stream conditions.
  • the symmetry of the dual augmentor duct 43 achieves high hydraulic efficiencies in a bi-directional tidal environment.
  • the duct entry 45 and exit 46 are axi- symmetric. Alternate configurations such as square, rectangular or any other arbitrary shape may be employed as dictated by the parameters of specific sites or applications such as tidal regime and local bathymetry. The optimal shape for each site is determined by performing a computational fluid dynamic analysis of the site.
  • the preferred embodiment is axi-symmetric.
  • the optimal design is further characterized by an inlet area 45 (augmentor duct rim 62) equal to the exit area 46 (opposite augmentor duct rim 62) and a throat area, turbine blade area, or annulus 51 (cylindrical section) that is optimally between nine-tenths (0.9) to one quarter (0.25) of the exit area 46 depending on the site- specific tidal conditions.
  • the annulus 51 is the area between the inner surface of the outer duct 40 and the outer surface of the hub 20 through which the turbine blades 30 pass.
  • the ratio of the central throat or inner surface of the outer duct 40 central portion to the augmentor duct rim 62 diameter is 0.5. In variations the ratio may be between 0.1 and 0.9.
  • both ducts 43 (including outer duct 40 rim 64) optimally have a hydrodynamic profile with a cross section that is similar in shape to an airplane wing. This profile increases the flow 100 into the turbine annulus as well as creates a smooth transition of the flow 100 into the adjacent slot 200 and around the entire tidal turbine generator 10.
  • an anti-fouling coating such as Si-Coat 560TM, is applied to the ducts 43.
  • specific areas susceptible to the buildup of aquatic organisms are coated.
  • the anti-foul coating has the additional benefit of providing a high lubricity surface which facilitates laminar flow, thereby improving the efficiency of the turbine generator 10.
  • Buoyancy material is incorporated into the internal structure of the dual augmentor duct 43 and the generator housing 92 in order to increase the overall buoyancy of the tidal turbine generator 10.
  • Neutral buoyancy is a key characteristic of the unit as it facilitates the process of unit removal and maintenance.
  • the ducts 43 are comprised of a composite shell structure filled with poly vinyl chloride closed cell marine foam (not shown) in order to achieve neutral buoyancy for the entire tidal turbine generator 10.
  • Other closed cell foams as known in the art, may also be employed.
  • the closed cell foam acts as a noise suppression device by attenuating the hydrodynamic and electrical noise produced by the tidal generator 10, thus mitigating any possible acoustic impacts of the tidal turbine generator 10 on cetaceans and other marine mammals.
  • the second unique flow characteristic is a longitudinal hole 240 through the hub 20.
  • the inner surface of the hub 20 is optimally cylindrical.
  • the outer surface of the hub is optimally elliptical, or barrel shaped, rising from the hub rim 27 to an apex in the flat central portion of the hub 20.
  • the inner surface of the hub 20 defines the longitudinal hole 240 along the hub 20 axis.
  • the profiles are varied as determined by a computational fluid dynamic analysis of the specific tidal site. Referring now to Figure 2, a front elevation view of the dual augmentor duct underwater turbine generator with slot 200 and hollow hub 240 flow enhancement structure is shown.
  • FIG. 3 a cut away perspective view of the slot 200 through the tidal turbine generator 10 is shown.
  • the slot 200 is defined by an upper surface, which is formed by the inner surface of the augmentor duct 41, and a lower surface formed by the outer surface of the outer duct 40, which encloses the generator housing 92.
  • the augmentor duct 41 is comprised of an inlet area 45, throat area 47 and exit area 46, which reverse with each flow 100 reversal.
  • the lower surface of the slot 200 in the preferred embodiment, is cylindrical with leading edge or outer duct rim 64 providing a smooth entry for the water flow 100 into both the slot 200 and the turbine annulus or rotor disk area 51.
  • the blades 30 are disposed in a rotor rim or ring 54.
  • the contours of the slot surface 200 may be varied.
  • the leading 34 and trailing 35 edges have a hydrodynamic profile with a cross section that is similar in shape to an airplane wing. This edge profile increases the flow 100 into the annulus area 51 as well as creates a smooth transition of the flow 100 into the central opening 240.
  • the central hole 240 is a region where the conservation of fluid momentum is maintained. This feature both eliminates the region of separation that previously existed behind the hub 20, and in addition, draws additional flow 100 through the surrounding turbine rotor disk area 51. Elimination of the region of separation also reduces the vibratory loading on the structure 10 resulting in improved reliability and therefore reduced maintenance cost. This central hole 240 increases both the output torque, and therefore the overall efficiency of the tidal turbine 10.
  • the central hole 240 concept also has a positive environmental benefit in addition to its performance enhancing effects.
  • This central region 240 provides a fish and marine mammal bypass in the event that this sea life enters the tidal turbine generator 10.
  • the hole 240 through the centre is large enough to accommodate all types of fish, and the majority of other marine mammals (with the exclusion of large whales).
  • the area occupied by the central hole 240 is less than or equal to the area occupied by the turbine rotor disk 51.
  • the exact ratio of these areas is determined by CFD analysis performed using site-specific parameters.
  • the optimal hole 240 to turbine rotor disk area 51 ratio is between 1:15 and 1:1, but in variations other ratios may be employed to some advantage.
  • the hub 20 that defines the central hole 240 is an integral structural member of the tidal turbine generator 10. The radial load or force on the turbine 10 is transferred from the hub 20 to the guide vanes or struts 24 and then through to the primary structural member, the outer duct 40. This produces a very stiff and robust structure.
  • the hub 20 houses a series of bearings 58 that provide the principal radial alignment and thrust support for the turbine rotor 50.
  • Water lubricated, low friction bearings 58 are mounted at the turbine rotor hub 20.
  • a central journal bearing 58 (or bearings) provides radial support for the rotor 50 and two thrust bearings 58 are located on either side of the rotor 50 to accommodate axial excursions resulting from the bi-directional hydrodynamic load on the turbine 10.
  • An additional set of water lubricated bearings 58 is also employed at the blade (rotor ) rim 54 location to counteract the axial thrust load of the rotor 50.
  • This complete bearing arrangement 58 reduces the susceptibility of the turbine rotor 50 to racking.
  • a magnetic bearing system or any other bearing system that is well known in the art can be employed.
  • the hub 20 consists of marine grade stainless steel.
  • An alternate embodiment includes a hub 20 manufactured from a composite material such as fiberglass, KevlarTM, Carbon fiber or any combination known in the art.
  • FIG 4 a side elevation sectional view of the hub and outer and augmentor ducts defining the slot and hole and showing flow streamlines 102 is shown.
  • the flow streamlines 102 illustrate the flow enhancement features of this design.
  • the geometry of the profile is varied in order to improve the flow characteristics for site-specific installations.
  • the slot 200 geometry is a function of the characteristics of the tidal stream at the specific site; however, the slot area 200, or effective gap has a normal range of 10% - 50% of the turbine rotor area or annulus 51.
  • Figure 4 illustrates the deflection of the flow streamlines 102 from the hole 240 and slot 200 area into the annulus 51 , thereby increasing the flow onto the rotor 50 and thereby increasing the power output.
  • the slot 200 and hole 240 are also shown.
  • Figure 6 a side elevation sectional view of a dual duct with an open slot variation is shown.
  • the slot 200 is discontinuous, and each augmentor duct rim 62 is supported by the struts 24.
  • the water flow 100 is also shown.
  • FIG. 7 a side elevation sectional view of a dual cylindrical duct covered slot 200 variation of the invention is shown.
  • the outer surface of the outer duct 40 is cylindrical in this variation.
  • the reduced vibrational loading on the tidal turbine generator 10, smoother laminar flow, increased water flow 100 through the rotor disks 50 due to the slot 200 and hole 240 features increase the output torque of the rotor disk 50 by above 50% in comparison to a similar turbine generator without the above-described flow enhancement structure, depending on the unit 10 type and site parameters, which in turn translates into an overall efficiency improvement of greater than 10%.

Abstract

A flow enhancement improvement for an underwater turbine generator is disclosed wherein a longitudinal hole is disposed in the central area, typically a hub of the generator, and a second, augmentor duct, preferably rigid, is disposed about the outer duct or housing of the unit to create a slot area. The slot and hollow hub create areas of smooth, laminar fluid flow. The leading edges of the hub or central ring and the augmentor and outer ducts are elliptical to enhance the fluid dynamics of the structure.

Description

FLOW ENHANCEMENT FOR UNDERWATER TURBINE GENERATOR
1. TECHNICAL FIELD
The present invenj^on relates generally to underwater ducted turbines for hydrokinetic electrical power generation. More specifically, a dual augmentor duct structure defining a^slot and a longitudinal hole through the hub of the turbine which enhances water.ilow are disclosed.
2. BACKGROUND OF THE INVENTION
Bi-directional, rim generating, ducted underwater turbines for generating electrical power are known, such as the applicant's PCT application PCT/CA02/01413 to Davis et al. There is a desire to improve the flow characteristics, and therefore, the efficiency of such designs. Fixed augmentors are known to increase flow through the turbine.
United States Patent 4,219,303 to Mouton et al. disclosed a rigid inner primary nozzle within a flexible outer nozzle which slightly overlaps the primary nozzle, creating a space between the nozzles for uni-directional flow. United States Patent 6,406,251Bl to Vauthier disclosed a mechanically complicated and inefficient system of pivoting flaps on the exterior surface of a hydroturbine accepting bi-directional flow.
The theoretical advantage of a slot in the duct of a conventional, uni¬ directional flow turbine with single duct was discussed in Kirke, B. Developments in Ducted Water Current Turbines, School of Engineering, Griffiths University.
It is also known to have a central space through a hydroturbine generator. United States Patent 4,509,442 to Matheisel disclosed a ducted propeller turbine with no hub or root section to the blade which is prone to excessive deflection, vibration and high cycle fatigue, particularly as without an inner support ring the blades are cantilevered towards the centre of the unit from the housing.
United States Patent RE38,336E (Reissue of 5,592,816) to Williams disclosed a hydroelectric turbine with a central open area of unrestricted flow surrounded by the blades which proposed reducing down current turbulence. United States Patent 6,648,589B2, also to Williams, disclosed a hydroelectric turbine with a central open area of unrestricted flow surrounded by the blades to aid in increasing the velocity of the water flowing through the single blade and to eliminate the turbulence that occurs behind the hub in traditional hub generator hydroelectric turbines. The Williams patents employ complicated hydraulic and mechanically driven generators with a uni-directional turbine blade configuration without ducting nor hydrodynamic structures to direct water flow in an efficient manner. The Williams patents do not incorporate a set of bearings at the hub to improve the structural integrity of the unit and reduce blade deflection. The present invention satisfies the need for a structurally and mechanically simple and inexpensive to manufacture flow enhancement design which increases water flow, provides a bypass for sea life and debris thereby reducing the environmental impact of the unit, reduces vibration and hydrodynamic drag and increases the operating efficiency of underwater ducted turbines.
3. SUMMARY OF THE INVENTION
It is an object of the present invention to implement an improved hydro turbine generator and method of flow enhancement wherein the improvement comprises a slot between a duct or housing and an augmentor device which is disposed about the duct. The augmentor device optimally has an inlet and an outlet which are substantially similar in area and a narrower central throat portion, thereby increasing the efficiency of the turbine. Specific optimal ratios of the throat area, slot area and the blade area to the inlet area are disclosed which further optimize the efficiency of the turbine.
The augmentor may be partial, or a complete second duct disposed about substantially all of the outer surface of the first duct, thereby creating a dual duct structure.
Another object of the present invention is to provide an augmentor which is axi-symmetric, with leading edges having hydrodynamic profiles, thereby minimizing turbulent water flow past the inlet and outlet and performing optimally in bi-directional water flow. The dual duct structure may be coated with an anti- fouling coating and may include buoyancy material, thereby achieving greater noise suppression, ensuring minimal environmental impact and providing corrosion resistance and high lubricity.
Another object of the present invention is to provide a flow enhancement structure in a turbine comprising a longitudinal hole substantially along the longitudinal axis of the turbine in a hub having specific shape, structural and material characteristics, thereby improving the efficiency of the turbine. Specific ratios of the hole area to the blade area are disclosed. The hole, combined with the flow characteristics of the hub, renders the turbine safe in relation to marine life.
4. BRIEF DESCRIPTION OF THE DRAWINGS
The apparatus and method of the present invention will now be described with reference to the accompanying drawing figures, in which:
FIG. 1 is an isometric view of the dual augmentor duct underwater turbine generator with slot and hollow hub flow enhancement structures according to the invention.
FIG. 2 is a front elevation view of the dual duct underwater turbine generator with slot and hollow hub flow enhancement structures according to the invention.
FIG. 3 is a cut-away perspective view of the dual augmentor duct underwater turbine generator with slot and hollow hub flow enhancement structures according to the invention.
FIG. 4 is a side elevation sectional view of the hub and outer and augmentor ducts defining the slot and hole and showing flow streamlines according to the invention.
FIG. 5 is a side elevation detail view of the leading edges of the hollow hub and outer augmentor ducts.
FIG. 6 is a side elevation sectional view of a dual augmentor duct open slot variation of the invention.
FIG. 7 is a side elevation sectional view of a cylindrical dual augmentor duct slot variation of the invention.
5. DETAILED DESCRIPTION OF THE INVENTION
Referring to Figure 1, an isometric view of the dual augmentor duct underwater turbine generator 10 with slot 200 and hollow hub 240 flow enhancement structures of the preferred embodiment is shown. In the preferred embodiment, the underwater ducted turbine 10 is of the type disclosed in the applicants' earlier invention the subject of PCT/CA02/01413 application to Davis et al., with the present improvement being directed towards a hollow hub 20 design and second, augmentor duct 41 disposed about the outer duct 40 with a slot 200 between the two ducts 43, which together enhance water flow 100 and increase efficiency of the turbine generator 10. The dual augmentor duct structure 43 is a fore and aft symmetric structure, namely it is symmetrical about a central vertical plane which transects the turbine generator 10 laterally. The dual duct structure 43 is disposed about the turbine rotor 50 and all generator components which are housed in the outer duct 40. The augmentor duct 41 has symmetrical inlet portions 45 and 46 creating a highly efficient duct for bi-directional flow. The central hole 240 may also be employed in units 10 without a hub, for instance with cantilevered blades disposed radially towards a central portion of the turbine generator. The central hole 240 may also be employed in non-ducted turbine generators 10.
The dual duct structure 43 is secured to the hub 20 by a plurality of struts 24 which also act as guide vanes in the annulus 51 area. The struts 24 are merely struts in the slot 200 area and not curved guide vanes. In the preferred embodiment there are five guide vanes 24 at each of the two ends of the turbine generator 10. The vanes 24 are preferably evenly spaced radially about the hub 20 axis. In the preferred embodiment, two counter-rotating rotor disks 50 are rotatably attached to the hub 20 and a plurality of blades 30, optimally symmetric hydrofoil blades, extend radially from said hub 20 to a rotor rim 54 which seats in a groove (not shown) in the interior surface of the outer duct 40 and is rotatable in a bearing race, or in a variation, a magnet bearing race. In other variations, single or multiple rotor disks 50 may be employed. The flow enhancement slot 200 and hole 240 structures may be employed not only for tidal applications, but also for other turbine generation applications, as one skilled in the art can appreciate.
In the preferred embodiment the dual augmentor duct 43 is a rigid structure manufactured from composite material. The dual augmentor duct 43 may be made from any composite material such as fiberglass, Kevlar™, carbon fiber, fiber- reinforced concrete or any other combination known in the art. Advantages of the rigid, symmetrical dual duct 43 arrangement include simplicity of manufacture, installation and maintenance and low capital cost. In a variation, a stainless steel rigid frame covered by a flexible composite material is used.
The interior wall of the augmentor duct 41 diverges towards the augmentor duct rim 62, thereby producing a decelerating effect downstream of the turbine blades as the water 100 flows through the duct 20. The outer surface of the augmentor duct 41 is concave in the preferred embodiment, but may be convex or cylindrical. Both ends of the dual augmentor duct 43 are effectively inlets as the turbine generator 10 is bidirectional. The central portion of the augmentor duct 41, is cylindrical. In operation, water flow 100 converges as it passes the inlet rim 62 and follows the profile of the augmentor duct 41 and outer duct 40. The gap or slot 200 between the outer duct 40 and augmentor ducts 41 is a smooth annular flow area. The blade tips 30 and rotor rim 54 (not shown here) are contained in annulus 51 and are not disposed in the slot 200. After the water flow 100 passes the rotor disks 50, the outer duct 40 and augmentor duct 41 diverge again, to allow for the smooth diffusion of the water flow 100 back to free stream conditions. The symmetry of the dual augmentor duct 43 achieves high hydraulic efficiencies in a bi-directional tidal environment. In the preferred embodiment, the duct entry 45 and exit 46 are axi- symmetric. Alternate configurations such as square, rectangular or any other arbitrary shape may be employed as dictated by the parameters of specific sites or applications such as tidal regime and local bathymetry. The optimal shape for each site is determined by performing a computational fluid dynamic analysis of the site. The preferred embodiment, however, is axi-symmetric. The optimal design is further characterized by an inlet area 45 (augmentor duct rim 62) equal to the exit area 46 (opposite augmentor duct rim 62) and a throat area, turbine blade area, or annulus 51 (cylindrical section) that is optimally between nine-tenths (0.9) to one quarter (0.25) of the exit area 46 depending on the site- specific tidal conditions. The annulus 51 is the area between the inner surface of the outer duct 40 and the outer surface of the hub 20 through which the turbine blades 30 pass. In the preferred embodiment, for general applications, the ratio of the central throat or inner surface of the outer duct 40 central portion to the augmentor duct rim 62 diameter is 0.5. In variations the ratio may be between 0.1 and 0.9.
The leading and trailing edges or rims of both ducts 43 (including outer duct 40 rim 64) optimally have a hydrodynamic profile with a cross section that is similar in shape to an airplane wing. This profile increases the flow 100 into the turbine annulus as well as creates a smooth transition of the flow 100 into the adjacent slot 200 and around the entire tidal turbine generator 10.
In the preferred embodiment, an anti-fouling coating, such as Si-Coat 560™, is applied to the ducts 43. In a variation, specific areas susceptible to the buildup of aquatic organisms are coated. The anti-foul coating has the additional benefit of providing a high lubricity surface which facilitates laminar flow, thereby improving the efficiency of the turbine generator 10.
Buoyancy material is incorporated into the internal structure of the dual augmentor duct 43 and the generator housing 92 in order to increase the overall buoyancy of the tidal turbine generator 10. Neutral buoyancy is a key characteristic of the unit as it facilitates the process of unit removal and maintenance. In the preferred embodiment, the ducts 43 are comprised of a composite shell structure filled with poly vinyl chloride closed cell marine foam (not shown) in order to achieve neutral buoyancy for the entire tidal turbine generator 10. Other closed cell foams, as known in the art, may also be employed. In addition to the buoyancy function, the closed cell foam acts as a noise suppression device by attenuating the hydrodynamic and electrical noise produced by the tidal generator 10, thus mitigating any possible acoustic impacts of the tidal turbine generator 10 on cetaceans and other marine mammals.
The second unique flow characteristic is a longitudinal hole 240 through the hub 20. The inner surface of the hub 20 is optimally cylindrical. The outer surface of the hub is optimally elliptical, or barrel shaped, rising from the hub rim 27 to an apex in the flat central portion of the hub 20. The inner surface of the hub 20 defines the longitudinal hole 240 along the hub 20 axis. In other variations, the profiles are varied as determined by a computational fluid dynamic analysis of the specific tidal site. Referring now to Figure 2, a front elevation view of the dual augmentor duct underwater turbine generator with slot 200 and hollow hub 240 flow enhancement structure is shown. The leading edge of the outer duct rim 64, hub rim 27, curved nature of the guide vanes 24 in the preferred embodiment, followed by the blades 30 and surrounded by the outer duct 40 are shown. Now referring to Figure 3, a cut away perspective view of the slot 200 through the tidal turbine generator 10 is shown. The slot 200 is defined by an upper surface, which is formed by the inner surface of the augmentor duct 41, and a lower surface formed by the outer surface of the outer duct 40, which encloses the generator housing 92. The augmentor duct 41 is comprised of an inlet area 45, throat area 47 and exit area 46, which reverse with each flow 100 reversal. The lower surface of the slot 200, in the preferred embodiment, is cylindrical with leading edge or outer duct rim 64 providing a smooth entry for the water flow 100 into both the slot 200 and the turbine annulus or rotor disk area 51. The blades 30 are disposed in a rotor rim or ring 54.
In variations, depending on the results from specific computational fluid dynamics ("CFD") analyses, the contours of the slot surface 200 may be varied. The leading 34 and trailing 35 edges have a hydrodynamic profile with a cross section that is similar in shape to an airplane wing. This edge profile increases the flow 100 into the annulus area 51 as well as creates a smooth transition of the flow 100 into the central opening 240.
The central hole 240 is a region where the conservation of fluid momentum is maintained. This feature both eliminates the region of separation that previously existed behind the hub 20, and in addition, draws additional flow 100 through the surrounding turbine rotor disk area 51. Elimination of the region of separation also reduces the vibratory loading on the structure 10 resulting in improved reliability and therefore reduced maintenance cost. This central hole 240 increases both the output torque, and therefore the overall efficiency of the tidal turbine 10.
The central hole 240 concept also has a positive environmental benefit in addition to its performance enhancing effects. This central region 240 provides a fish and marine mammal bypass in the event that this sea life enters the tidal turbine generator 10. The hole 240 through the centre is large enough to accommodate all types of fish, and the majority of other marine mammals (with the exclusion of large whales).
The area occupied by the central hole 240 is less than or equal to the area occupied by the turbine rotor disk 51. The exact ratio of these areas is determined by CFD analysis performed using site-specific parameters. The optimal hole 240 to turbine rotor disk area 51 ratio is between 1:15 and 1:1, but in variations other ratios may be employed to some advantage. The hub 20 that defines the central hole 240 is an integral structural member of the tidal turbine generator 10. The radial load or force on the turbine 10 is transferred from the hub 20 to the guide vanes or struts 24 and then through to the primary structural member, the outer duct 40. This produces a very stiff and robust structure. The hub 20 houses a series of bearings 58 that provide the principal radial alignment and thrust support for the turbine rotor 50. Water lubricated, low friction bearings 58 are mounted at the turbine rotor hub 20. A central journal bearing 58 (or bearings) provides radial support for the rotor 50 and two thrust bearings 58 are located on either side of the rotor 50 to accommodate axial excursions resulting from the bi-directional hydrodynamic load on the turbine 10. An additional set of water lubricated bearings 58 is also employed at the blade (rotor ) rim 54 location to counteract the axial thrust load of the rotor 50. This complete bearing arrangement 58 reduces the susceptibility of the turbine rotor 50 to racking. Optionally, a magnetic bearing system or any other bearing system that is well known in the art can be employed.
In the preferred embodiment, the hub 20 consists of marine grade stainless steel. An alternate embodiment includes a hub 20 manufactured from a composite material such as fiberglass, Kevlar™, Carbon fiber or any combination known in the art. Referring now to Figure 4, a side elevation sectional view of the hub and outer and augmentor ducts defining the slot and hole and showing flow streamlines 102 is shown. The flow streamlines 102 illustrate the flow enhancement features of this design. In variations, the geometry of the profile is varied in order to improve the flow characteristics for site-specific installations. The slot 200 geometry is a function of the characteristics of the tidal stream at the specific site; however, the slot area 200, or effective gap has a normal range of 10% - 50% of the turbine rotor area or annulus 51. Figure 4 illustrates the deflection of the flow streamlines 102 from the hole 240 and slot 200 area into the annulus 51 , thereby increasing the flow onto the rotor 50 and thereby increasing the power output.
The fluid that enters the slot 200 maintains its momentum through the slot 200 and then imparts this momentum into the boundary layer of the diverging section of the dual augmentor duct 43. This injection of fluid has the effect of both delaying the region of separation on the divergent portion of the duct 43 as well as drawing additional flow through the enclosed annulus 51 area. The net result of these effects is a significant increase in performance in blade 30 torque, and therefore an overall efficiency improvement of the tidal turbine generator 10. Now referring to Figure 5, a side elevation detail view of the leading edges of the hollow hub and outer and augmentor ducts is shown. The elliptical, fluid dynamic shape of the hub 20 rim 27, outer duct 40 rim 64, and the augmentor duct 41 rim 62, promote laminar flow and generator efficiency. The slot 200 and hole 240 are also shown. Now referring to Figure 6, a side elevation sectional view of a dual duct with an open slot variation is shown. The slot 200 is discontinuous, and each augmentor duct rim 62 is supported by the struts 24. The water flow 100 is also shown.
Now referring to Figure 7, a side elevation sectional view of a dual cylindrical duct covered slot 200 variation of the invention is shown. The outer surface of the outer duct 40 is cylindrical in this variation.
In operation, the reduced vibrational loading on the tidal turbine generator 10, smoother laminar flow, increased water flow 100 through the rotor disks 50 due to the slot 200 and hole 240 features increase the output torque of the rotor disk 50 by above 50% in comparison to a similar turbine generator without the above-described flow enhancement structure, depending on the unit 10 type and site parameters, which in turn translates into an overall efficiency improvement of greater than 10%.
As will be apparent to those skilled in the art in light of the foregoing disclosure, many alterations and modifications are possible in the practice of this invention without departing from the spirit or scope thereof. Accordingly, the scope of the invention is to be construed in accordance with the substance defined by the following claims.

Claims

WHAT IS CLAIMED IS:
1. An improved turbine generator including at least one blade and a housing disposed about said turbine, wherein the improvement comprises a slot defined by an outer surface of said housing and an inner surface of an augmentor disposed about said housing, said augmentor device having an inlet and an outlet which are substantially similar in area, thereby enhancing the flow characteristics of said turbine generator.
2. The improvement of claim 1 wherein said augmentor comprises a central throat portion disposed between said inlet and said outlet and having an area less than that of said inlet and said outlet, thereby creating a decelerating flow effect downstream of said slot and increasing the efficiency of said turbine.
3. The improvement of claim 2 wherein the ratio of the area of said throat portion to said inlet and said outlet area is between 0.1 and 0.9.
4. The improvement of claim 3 wherein said ratio is 0.5, thereby reaching maximum efficiency for said turbine.
5. The improvement of claim 1 wherein said augmentor is a second duct disposed about substantially all of said outer surface of said housing, thereby creating a dual duct structure.
6. The improvement of claim 5 wherein said augmentor is symmetrical about the vertical center of said generator, thereby maximizing efficiency for bi¬ directional flow.
7. The improvement of claim 1 further comprising leading edges on said inlet and said outlet, at least one of which has a hydrodynamic profile thereby minimizing turbulent water flow past said inlet and said outlet.
8. The improvement of claim 1 further comprising an anti-fouling coating on at least some of the surface defining said slot thereby maintaining said enhanced flow characteristics.
9. The improvement of claim 1 wherein the ratio of the area occupied by the rotating said blades to said inlet and outlet areas is between 0.25 - 0.5, thereby increasing the flow characteristics of said turbine.
10. The improvement of claim 1 wherein said duct and said augmentor together form a dual duct structure which comprises buoyancy material such that said turbine generator is neutrally buoyant.
11. The improvement of claim 10 wherein said dual duct structure is comprised of hard shell ducts filled with buoyant, hardened foam.
12. The improvement of claim 1 wherein said turbine generator comprises noise suppression means.
13. The improvement of claim 1 wherein said slot area is 10 - 50% of an area described by a path of said at least one blade.
14. A flow enhancement structure in a turbine having a hub and at least one blade projecting from a longitudinal axis therethrough and sweeping a blade area during rotation, said hub comprising a longitudinal hole substantially along said longitudinal axis and defined by an interior surface of said hub, said hub also comprising two ends and an outer surface, said ends having a diameter equal to or lesser than the diameter of said hub at any other point, and the ratio of the area of said longitudinal hole to said blade area being between 1 : 1 and 1 :15, thereby creating a hydrodynamic shape and improving the efficiency of said turbine.
15. The flow enhancement structure of claim 14 further comprising a plurality of struts projecting radially from said hub to a housing disposed about said turbine, thereby reinforcing said turbine against vibration caused by increased water flow through said hole.
16. The flow enhancement structure of claim 14 wherein said hub is comprised of one of stainless steel, fiberglass, Kevlar™ or carbon fiber material.
17. The flow enhancement structure of claim 14 wherein said hole is of a dimension sufficient for sealife to bypass said at least one blade, thereby rendering said turbine safe in relation to marine life.
18. An improved bidirectional hydro turbine generator having a water flow area through at least one rotor disk, said improvement comprising, outer slot and inner hole areas defined by dual ducts and a hub respectively thereby increasing the water flow through said turbine generator and rendering said turbine generator more efficient.
19. The improvement of claim 18 wherein the exterior of said dual ducts is flared at both ends, thereby creating a central throat area in said turbine which is narrower than said ends and thereby optimizes the bidirectional flow characteristics of said hydro turbine generator.
20. The improvement of claim 19 wherein said hub comprises curved edges at each end of said hub thereby rendering said hub hydrodynamic.
PCT/CA2005/000267 2004-09-17 2005-02-24 Flow enhancement for underwater turbine generator WO2006029496A1 (en)

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JP2007531548A JP2008513650A (en) 2004-09-17 2005-02-24 Increased flow for underwater turbine generators.
EP05714509A EP1789676A1 (en) 2004-09-17 2005-02-24 Flow enhancement for underwater turbine generator
AU2005284617A AU2005284617B2 (en) 2004-09-17 2005-02-24 Flow enhancement for underwater turbine generator
NZ553511A NZ553511A (en) 2004-09-17 2005-02-24 Flow enhancement for underwater turbine generator
CA002549376A CA2549376C (en) 2004-09-17 2005-02-24 Flow enhancement for underwater turbine generator
CN2005800313363A CN101023264B (en) 2004-09-17 2005-02-24 Flow enhancement for underwater turbine generator
US11/663,001 US7874788B2 (en) 2004-09-17 2005-02-24 Flow enhancement for underwater turbine
NO20071909A NO20071909L (en) 2004-09-17 2007-04-16 Two way hydro turbine generator
US12/976,338 US20110115228A1 (en) 2004-09-17 2010-12-22 Flow enhancement for underwater turbine generator

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