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WO2000075507A1 - Turbine a entrainement fluidique perfectionnee avec diffuseur - Google Patents

Turbine a entrainement fluidique perfectionnee avec diffuseur Download PDF

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Publication number
WO2000075507A1
WO2000075507A1 PCT/AU2000/000642 AU0000642W WO0075507A1 WO 2000075507 A1 WO2000075507 A1 WO 2000075507A1 AU 0000642 W AU0000642 W AU 0000642W WO 0075507 A1 WO0075507 A1 WO 0075507A1
Authority
WO
WIPO (PCT)
Prior art keywords
fluid
driven turbine
diffuser
assembly
shroud
Prior art date
Application number
PCT/AU2000/000642
Other languages
English (en)
Inventor
Bruce Justin Smith
Original Assignee
Bruce Justin Smith
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 Bruce Justin Smith filed Critical Bruce Justin Smith
Priority to AU2000249017A priority Critical patent/AU2000249017A1/en
Publication of WO2000075507A1 publication Critical patent/WO2000075507A1/fr

Links

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
    • F03D—WIND MOTORS
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/04—Wind motors with rotation axis substantially parallel to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • 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
    • F03D—WIND MOTORS
    • F03D13/00—Assembly, mounting or commissioning of wind motors; Arrangements specially adapted for transporting wind motor components
    • F03D13/20—Arrangements for mounting or supporting wind motors; Masts or towers for wind motors
    • 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
    • F05B2210/00—Working fluid
    • F05B2210/16—Air or water being indistinctly used as working fluid, i.e. the machine can work equally with air or water without any modification
    • 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
    • F05B2240/133—Stators to collect or cause flow towards or away from turbines with a convergent-divergent guiding structure, e.g. a Venturi conduit
    • 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
    • F05B2240/20—Rotors
    • F05B2240/21—Rotors for wind turbines
    • F05B2240/221—Rotors for wind turbines with horizontal axis
    • F05B2240/2213—Rotors for wind turbines with horizontal axis and with the rotor downwind from the yaw pivot axis
    • 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
    • F05B2240/20—Rotors
    • F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/31—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape
    • F05B2240/311—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape flexible or elastic
    • 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
    • F05B2240/91—Mounting on supporting structures or systems on a stationary structure
    • F05B2240/912—Mounting on supporting structures or systems on a stationary structure on a tower
    • 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
    • F05B2280/00—Materials; Properties thereof
    • F05B2280/60—Properties or characteristics given to material by treatment or manufacturing
    • F05B2280/6001—Fabrics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2253/00—Other material characteristics; Treatment of material
    • F05C2253/02—Fabric
    • 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
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction
    • 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
    • Y02E10/70—Wind energy
    • Y02E10/728—Onshore wind turbines

Definitions

  • TECHNICAL FIELD relates to a turbine for recovering energy from a fluid stream, in particular, the invention concerns a diffuser augmented fluid-driven turbine having a fabric shroud.
  • the invention has been primarily developed for use in recovering energy from air streams and will therefore be described in this context. However, it is to be appreciated that the invention can also be used to recover energy from other fluid streams, such as water currents. BACKGROUND ART
  • Diffuser augmented wind turbines characteristically comprise wind-driven rotor blades housed within a throat of a shroud, the shroud having an air intake section that converges towards the throat and an air outlet section (diffuser section) that diverges from the throat.
  • the conical shape of the diffuser section helps air that has passed through the rotor blades (ie. turbine wake) to remain at a pressure below atmospheric pressure, thus encouraging more air to be drawn through the blades.
  • the wake As the wake flows towards an exit of the diffuser section it gradually undergoes a change back to atmospheric pressure. This event can cause the wake to separate from an inner surface of the diffuser section (ie.
  • boundary layer separation and consequently to reduce turbine efficiency. It is possible to minimize this event by reducing the included angle of the conical section or by channeling air from outside of the shroud directly into the diffuser section for re-energizing the boundary layer. This can also provide an additional power augmentation effect to the turbine.
  • a diffuser augmented fluid-driven turbine comprising: fluid-driven rotor blades contained in a housing; at least one support ring assembly spaced from said housing and axially mounted with respect to said blades; a fabric shroud extending between said housing and said support ring assembly that when tensioned forms a diffuser section; and a spar assembly about which said blades rotate, with said spar assembly extending axially to said blades, and said housing and/or support ring assembly are adjustably mounted to said spar assembly so that said shroud can be tensioned.
  • the spar assembly can have a passage for channeling fluid into the diffuser section for mixing with a wake of the turbine, without having to pass through the rotor blades, so as to minimize premature separation of the wake from an inner surface of the diffuser section and also to provide a power augmentation effect.
  • the passage can have an inlet upstream of the blades and at least one outlet within the diffuser section. Preferably, the passage has multiple outlets.
  • the flow of fluid through the passage outlet can be regulated by varying the size of the outlet.
  • the size of the outlet can be varied by a slideable collar mounted to the spar assembly.
  • the collar can be slid manually, or, for instance, using hydraulic or pneumatic means. If desired, the collar can have projections for creating additional turbulence in the fluid flowing through the outlet, which can result in enhanced mixing with the turbine wake.
  • the blade housing can have a blade retaining ring for keeping the shroud from contacting the rotor blades and a plurality of stator blades for mounting the blade retaining ring to the spar assembly.
  • the housing is rigidly mounted to the spar assembly.
  • the stator blades can be adjusted to direct the flow of fluid to the rotor blades.
  • the diffuser augmented fluid-driven turbine can have a plurality of blades mounted for rotation about the spar assembly. Rotation can be effected with bearings.
  • the blades can rotate with at least one portion of the spar assembly. For instance, a portion of the spar assembly that has the passage outlet can rotate with the blades relative to the remainder of the spar assembly.
  • the diffuser augmented fluid-driven turbine can be coupled in numerous ways to machinery for generating electrical or mechanical energy from the recovered energy.
  • the rotor blades can be coupled to an electric generator by way of a gear assembly.
  • the support ring assembly can comprise: a ring that is attached to the shroud; a collar that is slideably mounted to the spar assembly; a first set of radial stays that attach the collar to the ring within the plane of the ring; and, a second set of radial stays that adjustably attach the ring to a region of the spar assembly located outside the shroud.
  • the second set of radial stays are attached to a cap that is adjustably mounted to an end of the spar assembly, and the shroud is tensioned by increasing the distance between the cap and the spar assembly end.
  • the cap can be mounted by any suitable method, but preferably, by adjustably bolting the cap to the spar assembly end.
  • the shroud can be tensioned in others ways.
  • the length of the second set of stays of the support ring assembly can be shortened, perhaps by using turnbuckles, instead of adjusting the position of the cap.
  • the spar assembly can be adjusted in length to tension the shroud.
  • a portion of the spar assembly between the first and second sets of radial stays could be lengthened to tension the shroud and shortened to relax the shroud.
  • the diffuser augmented fluid-driven turbine can have a further support ring assembly adjustably mounted to the spar assembly and spaced from the blade housing, and the shroud can extend between the housing and a ring of the further support ring assembly.
  • the further support ring assembly can be mounted to the spar assembly as for the support ring assembly of the diffuser section.
  • the shroud between the further support ring assembly and the housing can form a fluid intake section having an inner surface converging towards the housing.
  • the fluid inlet of the spar assembly is located upstream of the fluid intake section of the shroud.
  • the diffuser augmented fluid-driven turbine is lightweight yet sufficiently strong to tolerate strong fluid streams.
  • the fluid stream can comprise an air current or a water current.
  • the turbine is most suitable for recovering energy from wind.
  • the ring of the support ring assembly and spar assembly are of substantially hollow construction and that they comprise high strength material, such as steel.
  • the stays of the support ring assembly can be tensioned cables of any suitable material, or if desired, the stays can be rigid, perhaps tubular sections.
  • the diffuser augmented fluid- driven turbine can be submerged facing into the flow, as for recovering energy from wind.
  • the turbine should be constructed of materials that are tolerant of marine conditions and the turbine may lack an air intake section.
  • the diffuser augmented fluid-driven turbine can be mounted on top of a suitably designed chamber. Waves flowing into the chamber can force air out of the chamber through the turbine. As the wave recedes, the opposite occurs.
  • the shroud can consist of any thin, flexible material made of any combination of cloth, fiber, polymeric film, sheet or foam, and is preferably a durable, weatherproof and lightweight fabric, such as PVC coated polyester.
  • the shroud can be prefabricated so that when tensioned it adopts an appropriate "hourglass" shape, compete with sections that form the fluid intake section, the throat and the diffuser section. In this instance, the shroud need not necessarily be attached to the blade retaining ring.
  • the shroud can be attached to the ring of the support ring assembly using any suitable means, for instance, by stitching an edge of the fabric, or strengthened edge of the fabric to the ring or by clamping the fabric between a two-piece ring having identical halves.
  • the stays of the support ring assembly can be attached to the collar or spar assembly by any suitable means, such as a shackle arrangement, or lugs with eyes.
  • a sheath can be used to envelop the shroud so that drag forces on an outer surface of the diffuser section are reduced.
  • fabric of substantially cylindrical shape can be tensioned between the rings of the support ring assemblies such that the hourglass shape of the shroud is cloaked from the fluid current.
  • the diffuser augmented fluid-driven turbine can be supported by a ground-supporting structure by attaching the rings of the support ring assemblies to support arms of the structure.
  • the ground supporting structure can have other points of contact with the turbine.
  • a support arm can be further attached to the blade housing through the shroud to minimize the effect of rotor imbalance.
  • the blade housing, ring/s and spar assembly can be attached to the support arms in a number of ways, but a preferred way is the use of brackets fitted to the rings of the support ring assemblies and/or blade housing, whereby the brackets can accommodate movement of the rings when tensioning the shroud. If the turbine has only one support ring assembly, then a further point of contact is preferably at the blade housing.
  • Figure 1 is a partial longitudinal sectional view of a diffuser augmented fluid-driven turbine attached to a ground-supporting tower, according to an embodiment of the invention
  • Figure 2 is a partial end elevational view of the diffuser augmented fluid-driven turbine of Figure 1 ;
  • Figure 3 is a longitudinal sectional view of a diffuser augmented fluid- driven turbine according to an embodiment of the invention
  • Figure 4 is a detailed longitudinal sectional view of part of the turbine of Figure 3;
  • Figure 5 is a detailed end view of part of the turbine of Figure 4;
  • Figure 6 is a detailed longitudinal sectional view of part of a spar assembly of a diffuser augmented fluid-driven turbine, according to an embodiment of the invention;
  • Figure 7 is a detailed end view of part of the spar assembly of Figure 6;
  • Figure 8 is a detailed longitudinal sectional view of part of a spar assembly of a diffuser augmented fluid-driven turbine, according to an embodiment of the invention;
  • Figure 9 is a detailed end view of part of the spar assembly of Figure 8.
  • Figure 10 is a partial longitudinal sectional view of a diffuser augmented fluid-driven turbine attached to a ground-supporting tower, according to an embodiment of the invention.
  • FIG. 1 there is shown a diffuser augmented wind turbine 1 ("wind turbine") attached to a ground-supporting tower 2 according to an embodiment of the invention.
  • the wind turbine 1 comprises: wind-driven rotor blades 3 contained in a housing 4, 5; two support ring assemblies 8, 10, 11 and 7, 10, 11 positioned on either side of the housing 4, 5 and axially mounted with respect to the blades 3; a fabric shroud 6 extending between rings 7 and 8 of the support ring assemblies; and, a spar assembly 9 that extends longitudinally to the blades 3 and which is adjustably mounted to rings 7 and 8.
  • the wind turbine 1 has blades 3 in a housing comprising a blade retaining ring 4, that stops the shroud 6 from contacting the blades 3, and a plurality of stator blades 5 for mounting the blade retaining ring 4 to the spar assembly 9.
  • the blades 3 rotate about the spar assembly 9.
  • Figures 1 and 2 show that the shroud 6 can be tensioned to form an air intake section 14 between ring 8 and retaining ring 4, and a diffuser section 15 between retaining ring 4 and ring 7.
  • the air intake section 14 has an inner surface 22 converging towards retaining ring 4 and the diffuser section 15 has an inner surface 23 diverging away from retaining ring 4.
  • FIGs 1 and 10 which represent different embodiments of the wind turbine 1 , illustrate that the shroud 6 can be attached to the retaining ring 4.
  • Figure 3 which represents another embodiment of the wind turbine 1 , shows that the shroud 6 is not attached to the retaining ring 4. However, in this case, the shroud 6 would be prefabricated so that when tensioned it will form the air intake section 14, diffuser section 15 and throat.
  • FIG. 3 shows further details of the support ring assemblies 8, 10, 11 and 7, 10, 11 that were only partly illustrated in Figures 1 and 2.
  • Each support ring assembly comprises: a ring (7 or 8) that is attached to the shroud 6; a collar 16 that is slideably mounted to the spar assembly 9; a first set of radial stays 10 that attach the collar 16 to the ring (7 or 8) within the plane of the ring (7 or 8); and, a second set of stays 11 that are attached to end 27 or end 32 of the spar assembly 9.
  • FIG. 2 shows that the collar 16 has lugs 43 with eyes 44 from which extend the stays 10.
  • Each ring 7, 8 has a number of attached lugs 19 that have a first eye 20 for attaching to a stay of the first set of stays 10 and a second eye 21 for attaching to a stay of the second set of stays 11.
  • FIG 3 shows that stays 11 , located near the diffuser section 15, are attached to an adjustably mounted cap 24 that engages spar assembly end 27.
  • the cap 24 has lugs 25 with eyes 26 from which extend stays 11.
  • the shroud 6 is tensioned by increasing the distance between the cap 24 and end 27.
  • Better views of how cap 24 can be mounted to end 27 are shown in Figures 4 and 5.
  • the distance between the cap 24 and end 27 can be adjusted by screwing retaining nuts 29 along bolts 28.
  • the second set of stays 11 extending from ring 8 can be attached to spar assembly end 32 by means of lugs 30 with eyes 31.
  • spar assembly end 32 has a passage 33 for injecting air into the diffuser section 15 for mixing with the wake of the turbine, without having to pass through the rotating blades 3, so as to minimize premature separation of the wake from the inner surface 23 of the diffuser section 15 and also to provide a power augmentation effect.
  • the passage 33 extends longitudinally within the spar assembly 9 and has an inlet
  • the inlet 34 is located upstream of the blades 3.
  • Figures 3, 6 and 8 represent different embodiments of the spar assembly 9. The construction of the spar assembly 9 depends on how the blades 3 are to rotate about the spar assembly 9 and how the passage outlets
  • Figure 35 are to be configured.
  • a portion 45 of the spar assembly 9 having the passage outlets 35 also has a hub 46 of the blades 3.
  • Blades 3 are attached to the hub 46 with fasteners that pass through apertures 48.
  • Spar portion 45 rotates about another portion 47 of the spar assembly 9 by means of bearings 49.
  • Hub 46 only partially obstructs the air flowing through passage 33, as evident from Figure 9.
  • the spar assembly 9 has an adjustably mounted sliding collar 36 that regulates the amount of air that is able to exit the outlets 35.
  • This collar 36 does not appear in the embodiment of Figure 3.
  • the collar 36 is slid using a hydraulic cylinder 37 that is further attached to the spar assembly 9.
  • Figure 6 also shows that the collar 36 has finger-like projections 38 for creating additional turbulence in the exiting air, which can result in enhanced mixing with the turbine wake.
  • the spar assembly portion containing passage 33 is attached to the spar assembly portion not containing the passage by a core structural member 42, which in this embodiment produces four separate outlets 35 (best viewed in Figure 7).
  • drag forces on an outer surface of the shroud 6 can be reduced by rendering a region between the air intake section 14 and diffuser section 15 substantially cylindrical in shape.
  • a tensioned fabric sheath 40 extends from ring 8 to item 39 on shroud 6 at the diffuser section 15.
  • the diffuser augmented wind turbine 1 of Figure 1 is supported by a tower 2 at four points of contact with the rings 7, 8, two of which can be seen at items 12 and 13. Details of these contact points are not illustrated but preferably involve adjustable brackets attached to the rings 7, 8.
  • Figure 3 illustrates the light weightiness of the wind turbine 1 , as the spar assembly 9 is substantially hollow, rings 7, 8 are hollow (not clearly shown), and the shroud 6 comprises PVC coated polyester.
  • FIG 10 there is shown a diffuser augmented wind turbine 1 attached to a ground-supporting tower 2 according to another embodiment of the invention.
  • the wind turbine 1 is essentially identical to that of the wind turbine of Figures 1 and 3, except for the fact that it does not have an air intake section 14.
  • This wind turbine 1 has four points of contact with the tower 2, two of the contact points being to the blade retaining ring 4 and the other two being to ring 7. Only two points of contact 41 , 13 can be seen in this figure.

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

L'invention concerne une turbine (1) à entraînement fluidique perfectionnée avec diffuseur, destinée à récupérer l'énergie d'un courant fluidique et comprenant des auges mobiles (3) à entraînement fluidique contenues dans un logement (4, 5), deux ensembles anneau de suport (8, 19, 11 et 7, 10, 11) positionnés de chaque côté du logement (4, 5) et montés axialement par rapport aux auges (3), un anneau de renforcement tendu (6) en tissu s'étendant entre les anneaux (7 et 8) des ensembles anneaux de support, et un ensemble longeron (9) s'étendant longitudinalement vers les auges (3) et fixé de manière amovible sur les anneaux (7 et 8) des ensembles anneaux de support. L'ensemble longeron (9) comprend un passage (33) par lequel le fluide en amont des auges mobiles (3) peut être injecté dans une section diffuseur (15) de la turbine (1), sans avoir à passer par les auges (3). La turbine (1) a pour support une tour (2).
PCT/AU2000/000642 1999-06-08 2000-06-07 Turbine a entrainement fluidique perfectionnee avec diffuseur WO2000075507A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2000249017A AU2000249017A1 (en) 1999-06-08 2000-06-07 Diffuser augmented fluid-driven turbine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AUPQ0852 1999-06-08
AUPQ0852A AUPQ085299A0 (en) 1999-06-08 1999-06-08 Diffuser augmented wind turbine

Publications (1)

Publication Number Publication Date
WO2000075507A1 true WO2000075507A1 (fr) 2000-12-14

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ID=3815049

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PCT/AU2000/000642 WO2000075507A1 (fr) 1999-06-08 2000-06-07 Turbine a entrainement fluidique perfectionnee avec diffuseur

Country Status (2)

Country Link
AU (1) AUPQ085299A0 (fr)
WO (1) WO2000075507A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2832465A1 (fr) * 2001-11-19 2003-05-23 Cie Internationale Des Turbine Diffuseur statique pour eolienne
WO2003102411A1 (fr) * 2002-05-30 2003-12-11 Arthur Benjamin O'connor Turbine amelioree
EP1941159A2 (fr) * 2005-09-23 2008-07-09 C. Raymond Green Aerogenerateur
WO2010006427A1 (fr) 2008-07-17 2010-01-21 Slingshot Wind Energy Systems Inc. Réseau d'ailes rogallo à nervures intégrées
WO2017026894A1 (fr) * 2015-08-11 2017-02-16 Jaarsma Freerk Éolienne

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL7705793A (en) * 1977-05-26 1978-11-28 Johan Adriaan Joseph Van Den B Wind energy recovery unit - comprises open ducts with hexagonal ends and round throats, accommodating propellers
DE29617306U1 (de) * 1996-10-04 1996-12-12 Freimund, Wolfgang, 22179 Hamburg Mantelwindturbine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL7705793A (en) * 1977-05-26 1978-11-28 Johan Adriaan Joseph Van Den B Wind energy recovery unit - comprises open ducts with hexagonal ends and round throats, accommodating propellers
DE29617306U1 (de) * 1996-10-04 1996-12-12 Freimund, Wolfgang, 22179 Hamburg Mantelwindturbine

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2832465A1 (fr) * 2001-11-19 2003-05-23 Cie Internationale Des Turbine Diffuseur statique pour eolienne
WO2003044361A1 (fr) * 2001-11-19 2003-05-30 Cita Diffuseur pour eolienne
WO2003102411A1 (fr) * 2002-05-30 2003-12-11 Arthur Benjamin O'connor Turbine amelioree
US6786697B2 (en) 2002-05-30 2004-09-07 Arthur Benjamin O'Connor Turbine
CN100390406C (zh) * 2002-05-30 2008-05-28 阿瑟·本杰明·奥康纳 涡轮机
EP1941159A4 (fr) * 2005-09-23 2012-12-19 C Raymond Green Aerogenerateur
EP1941159A2 (fr) * 2005-09-23 2008-07-09 C. Raymond Green Aerogenerateur
WO2010006427A1 (fr) 2008-07-17 2010-01-21 Slingshot Wind Energy Systems Inc. Réseau d'ailes rogallo à nervures intégrées
EP2310262A1 (fr) * 2008-07-17 2011-04-20 Slingshot Wind Energy Systems Inc. Réseau d'ailes rogallo à nervures intégrées
JP2011528077A (ja) * 2008-07-17 2011-11-10 スリングショット ウインド エナジー システム インコーポレイテッド 一体型リブ付きロガロ翼の配列
EP2310262A4 (fr) * 2008-07-17 2013-08-21 Slingshot Wind Energy Systems Inc Réseau d'ailes rogallo à nervures intégrées
WO2017026894A1 (fr) * 2015-08-11 2017-02-16 Jaarsma Freerk Éolienne
NL2015290B1 (nl) * 2015-08-11 2017-02-28 Jaarsma Freerk Windturbine.

Also Published As

Publication number Publication date
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