CA2988834C - Wind turbine rotor blade with deflection units - Google Patents
Wind turbine rotor blade with deflection units Download PDFInfo
- Publication number
- CA2988834C CA2988834C CA2988834A CA2988834A CA2988834C CA 2988834 C CA2988834 C CA 2988834C CA 2988834 A CA2988834 A CA 2988834A CA 2988834 A CA2988834 A CA 2988834A CA 2988834 C CA2988834 C CA 2988834C
- Authority
- CA
- Canada
- Prior art keywords
- fin
- rotor blade
- wind turbine
- region
- deflection unit
- 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.)
- Active
Links
- 238000010438 heat treatment Methods 0.000 claims description 4
- 230000000644 propagated effect Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 claims 2
- 239000011324 bead Substances 0.000 abstract 1
- 239000006260 foam Substances 0.000 description 2
- 238000005192 partition Methods 0.000 description 1
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
- F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
- F03D80/40—Ice detection; De-icing means
-
- 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
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape of the blades
-
- 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
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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Wind Motors (AREA)
Abstract
The invention relates to a wind turbine rotor blade (200), comprising a rotor-blade root region (200a), a rotor-blade tip region (200b), a pressure side (200c), a suction side (200d), at least one fin (210, 211, 212), which extends along a longitudinal direction (L) of the rotor blade (200), and at least one deflecting unit (221, 222) between an end of the at least one fin (211, 212) and the rotor-blade tip region (200b). The at least one deflecting unit (221, 222) is designed to deflect an air flow traveling along the at least one fin (211, 212). Furthermore, at least one fin bead (300) is provided, which is arranged in the region of the at least one fin (210, 211, 212) in order to reduce turbulence of the air during the deflection.
Description
Wind turbine rotor blade with deflection units The present invention concerns a wind turbine rotor blade and a wind turbine having a corresponding rotor blade.
As the rotor blades of a wind turbine are unprotectedly exposed to all weather conditions icing of the rotor blades can occur at certain temperatures. A rotor blade heating system can be used to prevent that.
In that case either heating can be provided externally on the rotor blade or warmed air can be provided within the rotor blade.
On the German patent application from which priority is claimed the German Patent and Trade Mark Office searched the following documents:
DE 200 14 238 Ul, DE 10 2010 051 297 Al, DE 10 2011 086 603 Al, DE
10 2005 034 131 Al and DE 195 28 862 Al.
An object of the present invention is to provide a wind turbine rotor blade which permits improved heating of the rotor blade.
That object is attained by a wind turbine rotor blade as described below.
Thus there is provided a wind turbine rotor blade comprising a rotor blade root region, a rotor blade tip region, a pressure side, a suction side, at least one fin which extends along a longitudinal direction of the rotor blade and at least one deflection unit between an end of the at least one fin and the rotor blade tip region. The at least one deflection unit is adapted to deflect an air flow which is propagated along the at least one Fin.
According to an aspect of the present invention a first deflection unit is provided in the region of an end of the first fin.
According to a further aspect of the present invention a second deflection unit is provided between the first deflection unit and the rotor blade tip.
According to a further aspect of the present invention the first deflection unit has a first and a second end and is of a round or elliptical
As the rotor blades of a wind turbine are unprotectedly exposed to all weather conditions icing of the rotor blades can occur at certain temperatures. A rotor blade heating system can be used to prevent that.
In that case either heating can be provided externally on the rotor blade or warmed air can be provided within the rotor blade.
On the German patent application from which priority is claimed the German Patent and Trade Mark Office searched the following documents:
DE 200 14 238 Ul, DE 10 2010 051 297 Al, DE 10 2011 086 603 Al, DE
10 2005 034 131 Al and DE 195 28 862 Al.
An object of the present invention is to provide a wind turbine rotor blade which permits improved heating of the rotor blade.
That object is attained by a wind turbine rotor blade as described below.
Thus there is provided a wind turbine rotor blade comprising a rotor blade root region, a rotor blade tip region, a pressure side, a suction side, at least one fin which extends along a longitudinal direction of the rotor blade and at least one deflection unit between an end of the at least one fin and the rotor blade tip region. The at least one deflection unit is adapted to deflect an air flow which is propagated along the at least one Fin.
According to an aspect of the present invention a first deflection unit is provided in the region of an end of the first fin.
According to a further aspect of the present invention a second deflection unit is provided between the first deflection unit and the rotor blade tip.
According to a further aspect of the present invention the first deflection unit has a first and a second end and is of a round or elliptical
2 configuration. An end of the first or second fin projects beyond the first and second end into the deflection unit.
According to a further aspect of the present invention a drop-shaped portion is provided at an end of the first or second fin.
According to a further aspect of the present invention a deflection unit is provided in the region of an end of the first fin and a second deflection unit is provided between the end of the second fin and the rotor blade tip.
The invention concerns the notion of providing in the interior of a wind turbine rotor blade in the region of the rotor blade tip a deflection unit in the region of an end of a fin of the rotor blade and/or a deflection unit in the region of the rotor blade tip. Provided in the rotor blade is at least one fin which extends from the region of the rotor blade root in the direction of the rotor blade tip without in that respect reaching the rotor blade tip.
Warmed air can flow along the fin in the direction of the rotor blade tip and can be directed or deflected in the direction of the rotor blade root again by the deflection means.
According to an aspect of the present invention the deflection unit is in the form of a deflection plate. A main part of the air flow can be put into a uniform configuration by a guide means which is round or portion-wise ellipsoidal. The deflection plate can for example be made of foam.
Alternatively or additionally thereto fin drop-shaped portions can be provided whereby an additional volume can be introduced to avoid steep pressure gradients in the flow direction.
In addition or alternatively thereto a flow feed guide can be provided. This can be effected for example by positioning a partition or the fins in such a way that the intake flows (the warmed air) are combined in the flow convergence guide in parallel and at the same speed.
Additionally or alternatively thereto it is possible to provide a deflection element which has a change in cross-sectional area that is as slight as possible.
Further embodiments of the invention are described below.
According to a further aspect of the present invention a drop-shaped portion is provided at an end of the first or second fin.
According to a further aspect of the present invention a deflection unit is provided in the region of an end of the first fin and a second deflection unit is provided between the end of the second fin and the rotor blade tip.
The invention concerns the notion of providing in the interior of a wind turbine rotor blade in the region of the rotor blade tip a deflection unit in the region of an end of a fin of the rotor blade and/or a deflection unit in the region of the rotor blade tip. Provided in the rotor blade is at least one fin which extends from the region of the rotor blade root in the direction of the rotor blade tip without in that respect reaching the rotor blade tip.
Warmed air can flow along the fin in the direction of the rotor blade tip and can be directed or deflected in the direction of the rotor blade root again by the deflection means.
According to an aspect of the present invention the deflection unit is in the form of a deflection plate. A main part of the air flow can be put into a uniform configuration by a guide means which is round or portion-wise ellipsoidal. The deflection plate can for example be made of foam.
Alternatively or additionally thereto fin drop-shaped portions can be provided whereby an additional volume can be introduced to avoid steep pressure gradients in the flow direction.
In addition or alternatively thereto a flow feed guide can be provided. This can be effected for example by positioning a partition or the fins in such a way that the intake flows (the warmed air) are combined in the flow convergence guide in parallel and at the same speed.
Additionally or alternatively thereto it is possible to provide a deflection element which has a change in cross-sectional area that is as slight as possible.
Further embodiments of the invention are described below.
3 Advantages and embodiments by way of example of the invention are described in greater detail hereinafter with reference to the drawing.
Figure 1 shows a diagrammatic view of a wind turbine according to the invention, Figure 2 shows a diagrammatic view of a portion of a rotor blade of the wind turbine of Figure 1, Figure 3 shows a portion of the rotor blade of Figure 2, Figures 4A-4C show various views of a fin drop-shaped portion according to the invention, and Figure 5 shows a diagrammatic perspective view of a portion of a wind turbine rotor blade according to the invention.
Figure 1 shows a diagrammatic view of a wind turbine according to the invention. The wind turbine 100 has a tower 102 and a pod 104 on the tower 102. Provided on the pod 104 is an aerodynamic rotor 106 having three rotor blades 200 and a spinner 110. The aerodynamic rotor 106 is caused to rotate by the wind in operation of the wind turbine and thus also rotates a rotor or rotor member of a generator coupled directly or indirectly to the aerodynamic rotor 106. The electric generator is arranged in the pod 104 and generates electrical energy. The pitch angle of the rotor blades 200 can be altered by pitch motors at the rotor blade roots of the respective rotor blades 200.
Figure 2 shows a diagrammatic view of a portion of a rotor blade of the wind turbine of Figure 1. The rotor blade 200 has a rotor blade root region 200a, a rotor blade tip region 200b, a leading edge 201, a trailing edge 202, a pressure side 200c and a suction side 200d. At least one fin 210 extends within the rotor blade along a longitudinal direction of the rotor blade 200. For example there can be two fins 211, 212 which can initially be parallel and can be of a mutually converging configuration in the region of the rotor blade tip 200b. In that respect the length of the first fin 211 can be less than the length of the second fin 212. A first deflection unit 221 can be provided in the region of an end 212a of the second fin 212. A second deflection unit 222 can be provided in the region of the tip 200b of the rotor blade.
Figure 1 shows a diagrammatic view of a wind turbine according to the invention, Figure 2 shows a diagrammatic view of a portion of a rotor blade of the wind turbine of Figure 1, Figure 3 shows a portion of the rotor blade of Figure 2, Figures 4A-4C show various views of a fin drop-shaped portion according to the invention, and Figure 5 shows a diagrammatic perspective view of a portion of a wind turbine rotor blade according to the invention.
Figure 1 shows a diagrammatic view of a wind turbine according to the invention. The wind turbine 100 has a tower 102 and a pod 104 on the tower 102. Provided on the pod 104 is an aerodynamic rotor 106 having three rotor blades 200 and a spinner 110. The aerodynamic rotor 106 is caused to rotate by the wind in operation of the wind turbine and thus also rotates a rotor or rotor member of a generator coupled directly or indirectly to the aerodynamic rotor 106. The electric generator is arranged in the pod 104 and generates electrical energy. The pitch angle of the rotor blades 200 can be altered by pitch motors at the rotor blade roots of the respective rotor blades 200.
Figure 2 shows a diagrammatic view of a portion of a rotor blade of the wind turbine of Figure 1. The rotor blade 200 has a rotor blade root region 200a, a rotor blade tip region 200b, a leading edge 201, a trailing edge 202, a pressure side 200c and a suction side 200d. At least one fin 210 extends within the rotor blade along a longitudinal direction of the rotor blade 200. For example there can be two fins 211, 212 which can initially be parallel and can be of a mutually converging configuration in the region of the rotor blade tip 200b. In that respect the length of the first fin 211 can be less than the length of the second fin 212. A first deflection unit 221 can be provided in the region of an end 212a of the second fin 212. A second deflection unit 222 can be provided in the region of the tip 200b of the rotor blade.
4 Warmed air can be guided along the fins in the direction of the rotor blade tip and then deflected.
Figure 3 shows a portion of the rotor blade of Figure 2. Figure 3 shows the rotor blade tip region 200b of the rotor blade 200. In particular an end 212a of the fin 212 and the first and second deflection units 221, 222 are shown here.
According to the invention the first deflection unit 221, the second deflection unit 222 or both deflection units 221, 222 can be provided.
Optionally the first deflection unit 221 can be of a round or elliptical configuration and can have two ends 221a, 221b, wherein the end 212a of the fin 212 projects beyond the first and second ends 221a, 221b into the deflection unit 221. That can ensure that the air flow is effectively deflected by the first deflection unit 221. In that respect it is possible to achieve in particular a uniform configuration in respect of the main part of the flow.
According to an aspect of the present invention fin drop-shaped portions 300 can be provided at the fin end.
As can be seen from Figure 2 the spacing between the first and second fins 211, 212 reduces in the direction of the rotor blade tip 200b.
Flow convergence can be achieved in that way. In particular the intake flows can combine when the flows are brought together in parallel relationship and at the same speed.
Figures 4A-4C show various views of a fin drop-shaped portion according to the invention. Figure 4A is a plan view of a fin drop-shaped portion 300, Figure 4B shows a perspective view of the fin drop-shaped portion 300 and Figure 4C is a sectional view along line A-A in Figure 4B.
The fin drop-shaped portion 300 is provided or glued at a fin end as shown in Figure 3. That fin drop-shaped portion is intended to improve deflection of the warmed air in the region of the rotor blade nose and in the region of the rotor blade rear box structure. The warmed air is deflected and flows for example in the region between the fins back to the rotor blade root.
According to the invention the fin drop-shaped portion 300 can be arranged laterally at a fin end.
The drop-shaped portion 300 has a first end 310, a second end 320 and optionally a recess 330 at the side surfaces of the drop-shaped portion.
The first end 310 is of a pointed configuration while the second end 320 is of a round configuration.
Figure 3 shows a portion of the rotor blade of Figure 2. Figure 3 shows the rotor blade tip region 200b of the rotor blade 200. In particular an end 212a of the fin 212 and the first and second deflection units 221, 222 are shown here.
According to the invention the first deflection unit 221, the second deflection unit 222 or both deflection units 221, 222 can be provided.
Optionally the first deflection unit 221 can be of a round or elliptical configuration and can have two ends 221a, 221b, wherein the end 212a of the fin 212 projects beyond the first and second ends 221a, 221b into the deflection unit 221. That can ensure that the air flow is effectively deflected by the first deflection unit 221. In that respect it is possible to achieve in particular a uniform configuration in respect of the main part of the flow.
According to an aspect of the present invention fin drop-shaped portions 300 can be provided at the fin end.
As can be seen from Figure 2 the spacing between the first and second fins 211, 212 reduces in the direction of the rotor blade tip 200b.
Flow convergence can be achieved in that way. In particular the intake flows can combine when the flows are brought together in parallel relationship and at the same speed.
Figures 4A-4C show various views of a fin drop-shaped portion according to the invention. Figure 4A is a plan view of a fin drop-shaped portion 300, Figure 4B shows a perspective view of the fin drop-shaped portion 300 and Figure 4C is a sectional view along line A-A in Figure 4B.
The fin drop-shaped portion 300 is provided or glued at a fin end as shown in Figure 3. That fin drop-shaped portion is intended to improve deflection of the warmed air in the region of the rotor blade nose and in the region of the rotor blade rear box structure. The warmed air is deflected and flows for example in the region between the fins back to the rotor blade root.
According to the invention the fin drop-shaped portion 300 can be arranged laterally at a fin end.
The drop-shaped portion 300 has a first end 310, a second end 320 and optionally a recess 330 at the side surfaces of the drop-shaped portion.
The first end 310 is of a pointed configuration while the second end 320 is of a round configuration.
5 Figure 5 shows a diagrammatic perspective view of a portion of a wind turbine rotor blade according to the invention. The rotor blade 200 has a first and second fin 211, 212, a first and second deflection unit 221, 222 and a fin drop-shaped portion 300 at an end 211a of the first fin 211.
The first deflection unit 221 is provided in the region of the end 211a of the first fin 211 while the second deflection unit 222 is provided in the region of the end 212a of the second fin 212. According to the invention the fin drop-shaped portion 300 is provided laterally on the first fin 211. A fin drop-shaped portion 300 can be also be provided at the end 212a of the second fin 212.
The fin drop-shaped portion 300 can also be provided at other locations along the fins (for example in the centre). The deflection unit can be made for example from foam and forces the main part of the air flow into a uniform configuration. The fin drop-shaped portion serves as an additional volume for avoiding severe pressure gradients in the flow direction. In addition the fin drop-shaped portions serve to round off the corners.
The first deflection unit 221 is provided in the region of the end 211a of the first fin 211 while the second deflection unit 222 is provided in the region of the end 212a of the second fin 212. According to the invention the fin drop-shaped portion 300 is provided laterally on the first fin 211. A fin drop-shaped portion 300 can be also be provided at the end 212a of the second fin 212.
The fin drop-shaped portion 300 can also be provided at other locations along the fins (for example in the centre). The deflection unit can be made for example from foam and forces the main part of the air flow into a uniform configuration. The fin drop-shaped portion serves as an additional volume for avoiding severe pressure gradients in the flow direction. In addition the fin drop-shaped portions serve to round off the corners.
Claims (10)
1. A wind turbine rotor blade (200) comprising a rotor blade root region (200a), a rotor blade tip region (200b), a pressure side (200c), a suction side (200d), a leading edge (201), a trailing edge (202), at least one fin (210, 211, 212) which extends along a longitudinal direction (L) to the rotor blade (200), at least one deflection unit (221, 222) between an end of the at least one fin (211, 212) and the rotor blade tip region (200b), wherein the at least one deflection unit (221, 222) is adapted to deflect an air flow which is propagated along the at least one fin (211, 212), and at least one fin drop-shaped portion (300) arranged in the region of the at least one fin (210, 211, 212) to reduce turbulence of the air upon deflection.
2. A wind turbine rotor blade according to claim 1 wherein a first deflection unit (221) is arranged in the region of an end (212a) of the at least one fin (212).
3. A wind turbine rotor blade according to claim 1 or claim 2 wherein a second deflection unit (222) is provided between the first deflection unit (221) and the rotor blade tip region (200b).
4. A wind turbine rotor blade according to one of claims 1 to 3 wherein the first deflection unit (221) has a first and a second end (221a, 221b) and is of a round or elliptical configuration, wherein the end (212a) of the at least one fin (212) projects beyond the first and second end (221a, 221b) into the first deflection unit (221, 222).
5. A wind turbine rotor blade according to one of claims 1 to 4 wherein the first deflection unit (221) is provided in the region of the end (211a) of the first fin (211) and the second deflection unit (222) is provided between the end (212a) of the second fin (212) and the rotor blade tip region (200b).
6. A wind turbine rotor blade according to one of claims 1 to 5 wherein the at least one fin drop-shaped portion (300) has a first end (310), a second end (320) and a recess (330) at a side surface of the drop-shaped portion (300), wherein the first end (310) is of a pointed configuration and the second end (320) is of a round configuration.
7. A wind turbine rotor blade according to claim 6 wherein the recess (330) is provided laterally on the fin drop-shaped portion (300), and wherein the fin drop-shaped portion (300) is provided laterally on the first fin (211) and/or the fin drop-shaped portion is provided laterally at the end (212a) of the second fin (212).
8. A wind turbine rotor blade according to one of claims 1 to 6 wherein the at least one fin drop-shaped portion (300) is arranged at an end of at least one fin (211, 212), wherein the end is towards the rotor blade tip region (200b).
9. A method of heating a wind turbine rotor blade (200) which has a rotor blade root region (200a), a rotor blade tip region (200b), a pressure side (200c), a suction side (200d), a leading edge (201), a trailing edge (202), at least a first and a second fin (211, 212) which extends along a longitudinal direction of the rotor blade (200), and at least one fin drop-shaped portion (300) arranged in the region of the at least one fin (210, 211, 212) to reduce turbulence in the air upon deflection, comprising the steps:
introducing warmed air along the leading edge (201) and/or the trailing edge (202), and deflecting the warmed air which flows along the leading edge (201) and/or the trailing edge (202).
introducing warmed air along the leading edge (201) and/or the trailing edge (202), and deflecting the warmed air which flows along the leading edge (201) and/or the trailing edge (202).
10. The method according to claim 9 wherein deflecting the warmed air comprises deflecting the warmed air into a region between the first and second fins.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102015112643.5 | 2015-07-31 | ||
| DE102015112643.5A DE102015112643A1 (en) | 2015-07-31 | 2015-07-31 | Wind turbine rotor blade |
| PCT/EP2016/068286 WO2017021350A1 (en) | 2015-07-31 | 2016-08-01 | Wind turbine rotor blade |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2988834A1 CA2988834A1 (en) | 2017-02-09 |
| CA2988834C true CA2988834C (en) | 2020-09-22 |
Family
ID=56567592
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2988834A Active CA2988834C (en) | 2015-07-31 | 2016-08-01 | Wind turbine rotor blade with deflection units |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US10655608B2 (en) |
| EP (1) | EP3329120B1 (en) |
| JP (1) | JP6545892B2 (en) |
| CN (1) | CN107923369B (en) |
| BR (1) | BR112018000661A2 (en) |
| CA (1) | CA2988834C (en) |
| DE (1) | DE102015112643A1 (en) |
| DK (1) | DK3329120T3 (en) |
| ES (1) | ES2762968T3 (en) |
| PT (1) | PT3329120T (en) |
| WO (1) | WO2017021350A1 (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102017110797A1 (en) * | 2017-05-18 | 2018-11-22 | Wobben Properties Gmbh | Wind turbine rotor blade |
| DE102021123954A1 (en) | 2021-09-16 | 2023-03-16 | Wobben Properties Gmbh | Wind turbine rotor blade |
| EP4180654A1 (en) | 2021-11-16 | 2023-05-17 | Wobben Properties GmbH | Wind turbine rotor blade |
| EP4191053A1 (en) | 2021-12-06 | 2023-06-07 | Wobben Properties GmbH | Wind turbine rotor blade |
| EP4276300A1 (en) | 2022-05-12 | 2023-11-15 | Wobben Properties GmbH | Wind turbine blade rotor blade and wind turbine |
| EP4303436A1 (en) * | 2022-07-04 | 2024-01-10 | Wobben Properties GmbH | Wind turbine blade rotor blade and wind turbine |
| EP4306797A1 (en) | 2022-07-12 | 2024-01-17 | Wobben Properties GmbH | Wind turbine blade rotor blade and wind turbine |
| EP4357605A1 (en) * | 2022-10-17 | 2024-04-24 | Wobben Properties GmbH | Wind turbine rotor blade and wind turbine |
| CN118128689A (en) * | 2024-01-26 | 2024-06-04 | 三峡科技有限责任公司 | Wind generating set blade for offshore hydrogen production platform, wind generating set and offshore hydrogen production platform |
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| GB2165315B (en) * | 1984-10-04 | 1987-12-31 | Rolls Royce | Improvements in or relating to hollow fluid cooled turbine blades |
| GB9014762D0 (en) * | 1990-07-03 | 1990-10-17 | Rolls Royce Plc | Cooled aerofoil vane |
| US5498126A (en) * | 1994-04-28 | 1996-03-12 | United Technologies Corporation | Airfoil with dual source cooling |
| DE19528862A1 (en) * | 1995-08-05 | 1997-02-06 | Aloys Wobben | Process for de-icing a rotor blade of a wind turbine and rotor blade suitable for carrying out the process |
| JPH11241602A (en) * | 1998-02-26 | 1999-09-07 | Toshiba Corp | Gas turbine blade |
| DE69940948D1 (en) * | 1999-01-25 | 2009-07-16 | Gen Electric | Internal cooling circuit for a gas turbine blade |
| DE20014238U1 (en) * | 2000-08-17 | 2001-06-07 | Wonner, Matthias, Dipl.-Ing., 70190 Stuttgart | Heating system for defrosting rotor blades of wind turbines |
| EP1223308B1 (en) * | 2000-12-16 | 2007-01-24 | ALSTOM Technology Ltd | Turbomachine component |
| EP1456505A1 (en) * | 2001-12-10 | 2004-09-15 | ALSTOM Technology Ltd | Thermally loaded component |
| US6939102B2 (en) * | 2003-09-25 | 2005-09-06 | Siemens Westinghouse Power Corporation | Flow guide component with enhanced cooling |
| US7217091B2 (en) * | 2004-07-20 | 2007-05-15 | General Electric Company | Methods and apparatus for deicing airfoils or rotor blades |
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| DK2129908T3 (en) * | 2007-03-20 | 2011-03-21 | Vestas Wind Sys As | Wind turbine blades with vortex generators |
| CN201437756U (en) | 2009-05-20 | 2010-04-14 | 宁波银风能源科技股份有限公司 | Noise reduction leaf blade of wind power generator |
| DE102010030472A1 (en) * | 2010-06-24 | 2011-12-29 | Repower Systems Ag | Rotorblattenteisung |
| DE102010051297B4 (en) * | 2010-11-12 | 2017-04-06 | Nordex Energy Gmbh | Rotor blade of a wind turbine |
| GB201102719D0 (en) * | 2011-02-17 | 2011-03-30 | Rolls Royce Plc | Cooled component for the turbine of a gas turbine engine |
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| DE102011086603A1 (en) | 2011-11-17 | 2013-05-23 | Wobben Properties Gmbh | Wind turbine rotor blade and method for defrosting a wind turbine rotor blade |
| CN104169576B (en) * | 2012-01-20 | 2017-06-13 | 维斯塔斯风力系统集团公司 | The method that deicing is carried out to wind turbine blade |
| US8985940B2 (en) * | 2012-03-30 | 2015-03-24 | Solar Turbines Incorporated | Turbine cooling apparatus |
| JP6101144B2 (en) | 2013-05-09 | 2017-03-22 | 三菱重工業株式会社 | Windmill blade, its deicing device, and deicing method |
-
2015
- 2015-07-31 DE DE102015112643.5A patent/DE102015112643A1/en not_active Withdrawn
-
2016
- 2016-08-01 JP JP2018500669A patent/JP6545892B2/en not_active Expired - Fee Related
- 2016-08-01 CN CN201680044401.4A patent/CN107923369B/en active Active
- 2016-08-01 EP EP16747488.1A patent/EP3329120B1/en active Active
- 2016-08-01 DK DK16747488.1T patent/DK3329120T3/en active
- 2016-08-01 BR BR112018000661-0A patent/BR112018000661A2/en not_active Application Discontinuation
- 2016-08-01 PT PT167474881T patent/PT3329120T/en unknown
- 2016-08-01 CA CA2988834A patent/CA2988834C/en active Active
- 2016-08-01 US US15/747,396 patent/US10655608B2/en active Active
- 2016-08-01 WO PCT/EP2016/068286 patent/WO2017021350A1/en active Application Filing
- 2016-08-01 ES ES16747488T patent/ES2762968T3/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| DE102015112643A1 (en) | 2017-02-02 |
| US20180216603A1 (en) | 2018-08-02 |
| CN107923369B (en) | 2019-11-19 |
| EP3329120A1 (en) | 2018-06-06 |
| CN107923369A (en) | 2018-04-17 |
| US10655608B2 (en) | 2020-05-19 |
| PT3329120T (en) | 2020-01-09 |
| JP6545892B2 (en) | 2019-07-17 |
| DK3329120T3 (en) | 2020-01-06 |
| CA2988834A1 (en) | 2017-02-09 |
| ES2762968T3 (en) | 2020-05-26 |
| EP3329120B1 (en) | 2019-10-16 |
| BR112018000661A2 (en) | 2019-05-14 |
| WO2017021350A1 (en) | 2017-02-09 |
| JP2018520299A (en) | 2018-07-26 |
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| Date | Code | Title | Description |
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| EEER | Examination request |
Effective date: 20171208 |