USRE41326E1 - Reinforced hub for the rotor of a wind energy turbine - Google Patents
Reinforced hub for the rotor of a wind energy turbine Download PDFInfo
- Publication number
- USRE41326E1 USRE41326E1 US12/148,774 US14877403A USRE41326E US RE41326 E1 USRE41326 E1 US RE41326E1 US 14877403 A US14877403 A US 14877403A US RE41326 E USRE41326 E US RE41326E
- Authority
- US
- United States
- Prior art keywords
- hollow body
- stiffening webs
- hub according
- hub
- flange
- 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.)
- Expired - Lifetime
Links
- 239000007787 solid Substances 0.000 claims description 3
- 230000007423 decrease Effects 0.000 claims 2
- 238000010276 construction Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 238000005266 casting Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Images
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
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0658—Arrangements for fixing wind-engaging parts to a hub
-
- 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
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0691—Rotors characterised by their construction elements of the hub
-
- 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
-
- 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
- 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 invention relates to a hub for the rotor of a wind energy turbine and, in particular, to a new construction of such a hub resulting in a light-weighted overall design of the hub.
- One approach for reducing weight is to reduce the wall thickness of the rotating elements of the nacelle.
- reducing the wall thickness does result in a reduced strength and stiffness of the rotating element.
- the hub of the rotor is subjected to forces resulting from wind acting on the rotor blades and forces resulting from loads due to the rotation of the hub.
- the hub must be stiff enough so that these forces do not cause deformations.
- the hub must be designed rather stiff so that an ovalization can be prevented which in turn would damage the rotor blade bearings and pitch drives.
- an object of the present invention is to provide a hub for the rotor of a wind energy turbine which has a relative low weight and is stiff enough in order to withstand the loads which during operation of the wind energy turbine acts on the hub.
- a hub for the rotor of a wind energy turbine comprising
- the hub according to the invention is provided with a hollow body which is rotatable around a rotation axis.
- the hollow body is provided with at least one flange to which a rotor blade bearing can be mounted.
- the flange defines a flange area which normally is defined by a hole.
- the hole there are arranged at least two stiffening or strengthening or reinforcing webs integrally formed with the hollow body and radially extending from the flange to the center of the flange area.
- the webs are arranged within the flange area like spokes of a wheel and provide stiffening, strengthening and reinforcing of the flange.
- the at least two stiffening webs divide the flange area into at least two openings separated by the stiffening webs.
- stiffening webs are provided within each flange area and build an angle between each other of substantially 180°. It is preferred that these two stiffening webs are arranged parallel to the rotation axis of the hub. As an alternative it is also possible that the stiffening webs are arranged such that they extend perpendicular to the rotation axis.
- the stiffening webs are homogeneously distributed within the flange area and are displaced relative to each other by an angle substantially equal to 360° divided by a number of the stiffening webs.
- the angles therebetween are substantially 120° and in case of four stiffening webs the angle therebetween is substantially 90°.
- one of the stiffening webs extends substantially parallel to the rotation axis of the hollow body.
- one of the stiffening webs extends substantially parallel to the rotation axis of the hollow body.
- four stiffening webs it is preferred to have two or them extending parallel to the rotation axis and the other two of them extending perpendicular to the rotation axis.
- the stiffening webs can be solid or hollow and can have a decreasing width and/or thickness towards the center of the flange area.
- the stiffening webs at the center of the flange area are smaller in width and/or thickness than at its radially outer ends adjacent the flange.
- stiffening webs of the individual sets are not connected among each other or are connected.
- the stiffening webs of the flange area not necessarily are arranged in a common plane but are arranged in different adjacent planes.
- stiffening webs of the individual sets of stiffening webs are rotated against each other from set to set around the rotor blade pitch access.
- a pitch drive can be mounted to at least one of the stiffening webs.
- This individual stiffening web is provided with an aperture for a rotor shaft of a pitch drive for rotating a rotor blade. Within the area of this aperture, the width or thickness or both of the individual stiffening web is increased in order to increase the stiffness of the web within the area of the pitch drive.
- the present invention can be used in a hub irrespective of the number of rotor blades.
- the hub according to the invention can be for a rotor with one, two or three rotor blades. Also more than three rotor blades can be mounted to the hub according to the invention which is provided with a number of flanges identical to the number of rotor blades.
- the hollow body of the hub comprises at least two or three flanges each defining a flange area.
- Each flange area is provided with at least two stiffening webs wherein the shape, design, number and/or relative arrangement of the stiffening webs within each flange area is identical or different from flange area to flange area.
- additional apertures can be provided within areas between adjacent flanges and the first and the second end of the hollow body both arranged in the direction of the rotation axis.
- These first and second ends also comprise openings or holes wherein the hole at the second end opposite to the shaft of the rotor is designed as a man hole. It is preferred that this man hole is located within a deepened portion of the hub located at the second end. This design provides increased stiffness of the hub at its man hole end.
- the first end of the hub to which the hollow shaft of the wind energy turbine is mounted preferably is also provided with a hole but can be closed as an alternative.
- FIG. 1 shows a side view of a wind energy turbine the rotor of which is provided with a hub according to the invention
- FIG. 2 is an enlarged view of the hub of the wind energy turbine of FIG. 1 according to a first embodiment of the invention
- FIG. 3 is a view when looking at the hub in the direction of arrows III of FIGS. 1 and 2 ,
- FIG. 4 is a view of the hub similar to that of FIG. 2 but with the hub being rotated by 120°,
- FIG. 5 is a perspective view of the hub according to FIGS. 2 to 4 .
- FIG. 6 is a view to an alternative embodiment of a hub according to the invention.
- FIG. 7 is a view to a hub according to another embodiment of the invention.
- FIG. 8 is a view of a hub according to a further embodiment of the invention.
- FIG. 9 is a cross-sectional view taken along line IX-IX of FIG. 8 .
- FIG. 10 is a perspective view of a hub according to a last embodiment of the invention.
- FIG. 1 shows the overall construction of a wind energy turbine 10 comprising a tower 12 and a nacelle 14 arranged on top of the tower 12 and rotatable around vertical axis 16 .
- the nacelle 14 comprises a housing 18 within which a shaft (not shown) is rotatably arranged around a horizontal axis 20 .
- a rotor 22 mounted to the shaft is a rotor 22 comprising a hub 24 and three rotor blades 26 radially extending from the hub 24 .
- the horizontal axis 20 is identical to the rotation axis of the rotor 22 .
- the hub 24 comprises a hollow body 28 made of a suitable cast material which is basically known to persons skilled in the art. Other materials providing the required rigidity can also be used.
- the hollow body 28 comprises a first end 30 and a second end 32 wherein the hollow shaft (not shown) of the wind energy turbine 10 is mounted to the first end 30 of the hollow body 28 .
- Three flanges 34 are arranged at the outside of the hollow body 28 wherein these three flanges 34 are displaced by 120°. Each flange 34 defines a flange area 36 within the respective flange 34 and extending in a plane.
- each flange area 36 there are provided three stiffening webs 38 integrally formed with the wall of the hollow body 28 and extending from the flange 34 radially inwardly to the center 40 of the flange area 36 where the three stiffening webs 36 are integrally connected to each other.
- the hollow body 28 including the stiffening webs 38 are formed according to a casting process which processes are basically known for the manufacture of hubs of the rotors of wind energy turbines. Other manufacturing processes for making the hub are also possible.
- the three stiffening webs 38 together are forming the shape of a three-arm-star wherein one of the stiffening webs extend parallel to the rotation axis 20 with an angle of 120° between adjacent stiffening webs 38 .
- One of the stiffening webs 38 comprises an aperture 42 through which the rotor shaft of a rotor blade pitch drive (both not shown) extends for rotating the rotor blade.
- the pitch drive can be mounted to that specific stiffening web 38 .
- additional apertures 44 are arranged in the wall of the hollow body 28 within areas defined by two adjacent flanges 34 and the openings at the first and second ends 30 , 32 , respectively. Providing these six holes 44 in these areas further reduces the overall weight of the hollow body 28 .
- FIGS. 4 and 5 show further views of the hub 24 making more evident the specific design of the hub 24 resulting a light-weighted but stiff overall construction of the hub 24 .
- FIGS. 6 to 10 show other embodiments of a hub according to the invention.
- the same reference numerals are used.
- Hub 24 of FIG. 6 comprises four stiffening webs 38 per each flange area 36 wherein one of the stiffening webs 38 is provided with a hole 42 for a pitch drive shaft wherein the thickness of the stiffening web 38 within the area of this aperture 42 is increased.
- the four stiffening webs 38 are displaced relative to each other by 90° so that the four stiffening webs 38 are in the form of a cross.
- the remaining design of the hub 24 of FIG. 6 is similar to that of the hub of FIGS. 2 to 5 .
- FIG. 7 shows a hub 24 the hollow body 28 of which comprises two stiffening webs 38 which extend parallel to the rotation axis 20 of the hub 24 and which are increased in width and/or thickness within the areas adjacent to the flange 34 .
- the hub 24 has a design similar to that of the hub of FIGS. 2 to 5 .
- FIGS. 8 and 9 Another embodiment of a hub 24 is shown in FIGS. 8 and 9 .
- two sets of stiffening webs 38 arranged as shown in FIG. 2 are located within each flange area.
- the two sets of stiffening elements are displaced along a rotor blade pitch axis 46 .
- FIG. 10 shows a perspective view to another hub 24 from the direction of the second end 32 thereof in which one can see that the man hole 48 arranged at this second end 32 is located within a deepened portion 50 of the wall of the hollow body 28 .
- This deepened portion increases stiffness and rigidity of the hollow body 28 .
- the design of the stiffening webs of the hub 24 of FIG. 10 is similar to that of the embodiment of FIG. 7 . However, also other stiffening web designs can be used in a hub 24 having a deepened portion 50 for the man hole 48 at the second end 32 of the hollow body 28 .
Landscapes
- 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)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/148,774 USRE41326E1 (en) | 2003-04-12 | 2003-04-12 | Reinforced hub for the rotor of a wind energy turbine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/148,774 USRE41326E1 (en) | 2003-04-12 | 2003-04-12 | Reinforced hub for the rotor of a wind energy turbine |
PCT/EP2003/003813 WO2004090326A1 (fr) | 2003-04-12 | 2003-04-12 | Moyeu renforce du rotor d'une turbine d'energie eolienne |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/517,690 Reissue US7244102B2 (en) | 2003-04-12 | 2003-04-12 | Reinforced hub for the rotor of a wind energy turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
USRE41326E1 true USRE41326E1 (en) | 2010-05-11 |
Family
ID=33154988
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/148,774 Expired - Lifetime USRE41326E1 (en) | 2003-04-12 | 2003-04-12 | Reinforced hub for the rotor of a wind energy turbine |
US10/517,690 Ceased US7244102B2 (en) | 2003-04-12 | 2003-04-12 | Reinforced hub for the rotor of a wind energy turbine |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/517,690 Ceased US7244102B2 (en) | 2003-04-12 | 2003-04-12 | Reinforced hub for the rotor of a wind energy turbine |
Country Status (7)
Country | Link |
---|---|
US (2) | USRE41326E1 (fr) |
EP (2) | EP2309120B1 (fr) |
CN (1) | CN1329657C (fr) |
AU (1) | AU2003224066A1 (fr) |
DK (2) | DK2309120T3 (fr) |
ES (2) | ES2364641T3 (fr) |
WO (1) | WO2004090326A1 (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080118356A1 (en) * | 2006-11-22 | 2008-05-22 | Fuji Jukogyo Kabushiki Kaisha | Hub for a horizontal axis wind turbine |
US20090004009A1 (en) * | 2007-06-28 | 2009-01-01 | Siemens Aktiengesellschaft | Method for controlling of at least one element of a first component of a wind turbine, control device and use of the control device |
US8246312B2 (en) | 2011-06-24 | 2012-08-21 | General Electric Company | Hub assembly for use with a wind turbine and method of making the same |
US20140064971A1 (en) * | 2012-08-29 | 2014-03-06 | General Electric Company | Stiffener plate for a wind turbine |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007002773A (ja) * | 2005-06-24 | 2007-01-11 | Fuji Heavy Ind Ltd | 水平軸風車 |
EP1907692B2 (fr) * | 2005-07-05 | 2022-12-07 | Vestas Wind Systems A/S | Articulation de pas d'éolienne, et son utilisation |
US7740450B2 (en) * | 2005-11-23 | 2010-06-22 | General Electric Company | Lightweight hub for rotors |
DE102006031174B3 (de) | 2006-07-03 | 2007-10-25 | Repower Systems Ag | Rotornabe einer Windenergieanlage |
US7614850B2 (en) * | 2006-07-11 | 2009-11-10 | General Electric Company | Apparatus for assembling rotary machines |
EP2047099A1 (fr) * | 2006-07-14 | 2009-04-15 | Vestas Wind Systems A/S | Éolienne comprenant une structure d'enceinte formée en tant que cage de faraday |
DE102006055091A1 (de) | 2006-11-21 | 2008-05-29 | Repower Systems Ag | Schott einer Windenergieanlage |
PL1933027T3 (pl) * | 2006-12-08 | 2011-10-31 | Stx Heavy Ind Co Ltd | Piasta wirnika turbiny wiatrowej |
ATE477417T1 (de) | 2007-01-24 | 2010-08-15 | Vestas Wind Sys As | Verfahren zum bewegen eines windturbinenbauteils, wie zum beispiel einer windturbinennabe, aus einer transportposition in eine windturbinenmontageposition in oder an der gondel,hauptwelle oder nabe, handhabungseinheit, windturbinennabe und verwendung davon |
DE102007008167C5 (de) | 2007-02-14 | 2016-07-07 | Nordex Energy Gmbh | Windenergieanlage mit einer Rotornabe |
DE102007008166A1 (de) * | 2007-02-14 | 2008-08-21 | Nordex Energy Gmbh | Windenergieanlage mit einer Pitchdrehverbindung |
US7871034B2 (en) * | 2008-04-23 | 2011-01-18 | Abe Karem | Rotor hub systems and methods |
US8061999B2 (en) * | 2008-11-21 | 2011-11-22 | General Electric Company | Spinner-less hub access and lifting system for a wind turbine |
DE102009015073A1 (de) | 2009-03-30 | 2010-10-07 | Würthele, Klaus | Versteifung des Nabenkörpers einer Windkraftanlage |
IT1394509B1 (it) * | 2009-05-20 | 2012-07-05 | Mait Spa | Turbina eolica e relativo dispositivo di regolazione del passo delle pale. |
ES2359310B2 (es) * | 2009-11-10 | 2012-05-16 | Gamesa Innovation & Technology S.L. | Aerogenerador con v�?as internas de acceso mejoradas. |
CN102822507B (zh) * | 2009-12-21 | 2015-05-20 | 维斯塔斯风力系统有限公司 | 用于风轮机的轮毂和制造所述轮毂的方法 |
DK2752577T3 (da) | 2010-01-14 | 2020-06-08 | Senvion Gmbh | Vindmøllerotorbladkomponenter og fremgangsmåder til fremstilling heraf |
US10137542B2 (en) | 2010-01-14 | 2018-11-27 | Senvion Gmbh | Wind turbine rotor blade components and machine for making same |
CN102182625B (zh) * | 2011-01-24 | 2012-12-26 | 江苏兴盛风能科技有限公司 | 风力发电机组的轮毂毛坯件 |
EP2691646B1 (fr) * | 2011-03-30 | 2017-07-12 | Vestas Wind Systems A/S | Moyeu pour turbine éolienne |
EP2532882A1 (fr) * | 2011-06-10 | 2012-12-12 | General Electric Company | Système et procédés pour assembler une éolienne avec un ensemble formant pas |
CN102384043A (zh) * | 2011-10-19 | 2012-03-21 | 北京工商大学 | 一种钻孔轮毂及其制造方法 |
US8449263B2 (en) | 2011-12-07 | 2013-05-28 | General Electric Company | Segmented rotor hub assembly |
CA2859695A1 (fr) * | 2011-12-21 | 2013-06-27 | Vestas Wind Systems A/S | Pale d'eolienne |
US9759198B2 (en) * | 2011-12-21 | 2017-09-12 | Vestas Wind Systems A/S | Wind turbine blade |
USD669012S1 (en) * | 2011-12-22 | 2012-10-16 | Pegasus Helicopter, Inc. | High efficiency hub for pressure jet helicopters |
US9115698B2 (en) | 2012-03-06 | 2015-08-25 | General Electric Company | Wind turbine with access features for gaining access to the interior of a rotor hub |
US9175668B2 (en) * | 2012-04-19 | 2015-11-03 | General Electric Company | Hub for wind turbine rotor |
WO2013185765A1 (fr) * | 2012-06-10 | 2013-12-19 | Vestas Wind Systems A/S | Améliorations concernant des turbines éoliennes |
ES2435340B1 (es) * | 2012-06-15 | 2014-12-05 | Gamesa Innovation & Technology, S.L. | Sistema de fijación para aerogeneradores y método de colocación del mismo |
EP2679805B1 (fr) * | 2012-06-29 | 2015-02-18 | General Electric Company | Insert de l'angle de cône pour rotor de turbine éolienne |
EP2778403A1 (fr) * | 2013-03-13 | 2014-09-17 | Siemens Aktiengesellschaft | Palier avec un élément de support et procédé de support d'une première bague de palier |
US9719489B2 (en) * | 2013-05-22 | 2017-08-01 | General Electric Company | Wind turbine rotor blade assembly having reinforcement assembly |
DK2886857T3 (en) * | 2013-12-17 | 2017-10-02 | Alstom Renovables Espana Sl | Wind turbine hub |
US9404473B2 (en) * | 2014-10-09 | 2016-08-02 | Michael Zuteck | Strain isolated attachment for one-piece wind turbine rotor hub |
US10598159B2 (en) | 2016-05-06 | 2020-03-24 | General Electric Company | Wind turbine bearings |
EP3690232B1 (fr) * | 2019-01-31 | 2023-01-04 | Siemens Gamesa Renewable Energy A/S | Moyeu pour une éolienne, éolienne et procédé de mise à niveau du moyeu d'une éolienne |
EP3786443A1 (fr) * | 2019-08-30 | 2021-03-03 | General Electric Renovables España S.L. | Ensemble de moyeu pour un rotor d'une éolienne |
EP4337856A1 (fr) * | 2021-05-10 | 2024-03-20 | Vestas Wind Systems A/S | Système de pas destiné à une pale d'éolienne |
CN114233567B (zh) * | 2022-01-25 | 2023-12-26 | 北京三力新能科技有限公司 | 一种鼓形轮毂、叶轮及风力发电机组 |
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US4112693A (en) | 1976-09-30 | 1978-09-12 | Kaiser Steel Corporation | Mine roof support plate |
US4668109A (en) | 1986-07-31 | 1987-05-26 | Basso Robert J | Journal with spring loaded bearings |
US4759459A (en) | 1985-01-17 | 1988-07-26 | Ford Motor Company | Fillable tank with filler pipe retainer |
US4863352A (en) | 1984-11-02 | 1989-09-05 | General Electric Company | Blade carrying means |
US4995023A (en) | 1989-01-13 | 1991-02-19 | Eta Sa Fabriques D'ebauches | Watchcase and watch provided with such case |
EP0546307A1 (fr) | 1991-12-12 | 1993-06-16 | Dr.Ing.h.c. F. Porsche Aktiengesellschaft | Roue d'alliage léger pour véhicule à moteur |
WO2003064854A1 (fr) * | 2002-01-31 | 2003-08-07 | Neg Micon A/S | Moyeu de pale pour eolienne |
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US4236873A (en) * | 1978-09-20 | 1980-12-02 | United Technologies Corporation | Wind turbine blade retention device |
US4260332A (en) * | 1979-03-22 | 1981-04-07 | Structural Composite Industries, Inc. | Composite spar structure having integral fitting for rotational hub mounting |
US5327647A (en) * | 1991-11-22 | 1994-07-12 | Energy Unlimited | Method for setting pitch on a windmill airfoil |
DE19916453A1 (de) * | 1999-04-12 | 2000-10-19 | Flender A F & Co | Windkraftanlage |
NL1013807C2 (nl) * | 1999-12-09 | 2001-07-05 | Aerpac Holding B V | Windturbinerotor, alsmede naaf en extender daarvoor. |
-
2003
- 2003-04-12 CN CNB038134632A patent/CN1329657C/zh not_active Expired - Lifetime
- 2003-04-12 ES ES03720457T patent/ES2364641T3/es not_active Expired - Lifetime
- 2003-04-12 ES ES11151473.3T patent/ES2605679T3/es not_active Expired - Lifetime
- 2003-04-12 EP EP11151473.3A patent/EP2309120B1/fr not_active Expired - Lifetime
- 2003-04-12 EP EP03720457A patent/EP1616094B1/fr not_active Expired - Lifetime
- 2003-04-12 DK DK11151473.3T patent/DK2309120T3/da active
- 2003-04-12 WO PCT/EP2003/003813 patent/WO2004090326A1/fr not_active Application Discontinuation
- 2003-04-12 DK DK03720457.5T patent/DK1616094T3/da active
- 2003-04-12 US US12/148,774 patent/USRE41326E1/en not_active Expired - Lifetime
- 2003-04-12 US US10/517,690 patent/US7244102B2/en not_active Ceased
- 2003-04-12 AU AU2003224066A patent/AU2003224066A1/en not_active Abandoned
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4112693A (en) | 1976-09-30 | 1978-09-12 | Kaiser Steel Corporation | Mine roof support plate |
US4863352A (en) | 1984-11-02 | 1989-09-05 | General Electric Company | Blade carrying means |
US4759459A (en) | 1985-01-17 | 1988-07-26 | Ford Motor Company | Fillable tank with filler pipe retainer |
US4668109A (en) | 1986-07-31 | 1987-05-26 | Basso Robert J | Journal with spring loaded bearings |
US4995023A (en) | 1989-01-13 | 1991-02-19 | Eta Sa Fabriques D'ebauches | Watchcase and watch provided with such case |
EP0546307A1 (fr) | 1991-12-12 | 1993-06-16 | Dr.Ing.h.c. F. Porsche Aktiengesellschaft | Roue d'alliage léger pour véhicule à moteur |
WO2003064854A1 (fr) * | 2002-01-31 | 2003-08-07 | Neg Micon A/S | Moyeu de pale pour eolienne |
Non-Patent Citations (1)
Title |
---|
PCT International Search Report, PCT/EP2003/03813 filed on Apr. 12, 2003, mailed on Dec. 29, 2003, pp. 3 total. |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080118356A1 (en) * | 2006-11-22 | 2008-05-22 | Fuji Jukogyo Kabushiki Kaisha | Hub for a horizontal axis wind turbine |
US8142166B2 (en) * | 2006-11-22 | 2012-03-27 | Fuji Jukogyo Kabushiki Kaisha | Hub for a horizontal axis wind turbine |
US20090004009A1 (en) * | 2007-06-28 | 2009-01-01 | Siemens Aktiengesellschaft | Method for controlling of at least one element of a first component of a wind turbine, control device and use of the control device |
US8342801B2 (en) * | 2007-06-28 | 2013-01-01 | Siemens Aktiengesellschaft | Method for controlling of at least one element of a first component of a wind turbine, control device and use of the control device |
US8246312B2 (en) | 2011-06-24 | 2012-08-21 | General Electric Company | Hub assembly for use with a wind turbine and method of making the same |
US20140064971A1 (en) * | 2012-08-29 | 2014-03-06 | General Electric Company | Stiffener plate for a wind turbine |
Also Published As
Publication number | Publication date |
---|---|
EP2309120A2 (fr) | 2011-04-13 |
ES2364641T3 (es) | 2011-09-08 |
EP2309120B1 (fr) | 2016-10-26 |
CN1659377A (zh) | 2005-08-24 |
ES2605679T3 (es) | 2017-03-15 |
WO2004090326A1 (fr) | 2004-10-21 |
EP1616094B1 (fr) | 2011-06-15 |
CN1329657C (zh) | 2007-08-01 |
AU2003224066A8 (en) | 2004-11-01 |
AU2003224066A1 (en) | 2004-11-01 |
DK1616094T3 (da) | 2011-08-29 |
EP2309120A3 (fr) | 2014-04-16 |
DK2309120T3 (da) | 2017-01-02 |
US7244102B2 (en) | 2007-07-17 |
EP1616094A1 (fr) | 2006-01-18 |
US20060104820A1 (en) | 2006-05-18 |
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