Means for alleviating strain on a wind turbine rotor blade
US-2016369775-A1 · Dec 22, 2016 · US
US9945352B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9945352-B2 |
| Application number | US-201314414869-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 24, 2013 |
| Priority date | Jul 25, 2012 |
| Publication date | Apr 17, 2018 |
| Grant date | Apr 17, 2018 |
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A wind turbine blade is described wherein at least on planar member is provided on the blade surface, where the planar member is arranged such that it extends at an angle to the chord of the blade. The planar member acts to re-direct airflow over the blade, to improve wind turbine performance. The planar member may be a stall fence provided towards the blade root end, further acting to divert airflow towards the root end of the blade to prevent separation of attached airflow. Additionally or alternatively, the planar member may be a flow diverter provided towards the blade tip end, to increase airflow in the tip region for increased performance and/or to disrupt the formation of tip vortices.
Opening claim text (preview).
The invention claimed is: 1. A wind turbine blade for a rotor of a wind turbine having a substantially horizontal rotor shaft, said rotor comprising a hub, from which the blade extends substantially in a radial direction when mounted to the hub, the blade having a longitudinal direction with a tip end and a root end and a transverse direction, the blade further comprising: a profiled contour including a pressure side and a suction side, as well as a leading edge and a trailing edge with a chord line having a chord length extending there between, the chord line transverse to said longitudinal direction, the profiled contour, when being impacted by an incident air-flow, generating a lift, wherein the wind turbine further comprises first and second flow guide members provided on a surface of said wind turbine blade, wherein said first and second flow guide members extend in a direction substantially transverse to the longitudinal direction of the blade, said first and second flow guide members defining a flow channel between said leading edge and said trailing edge, said flow channel having a first end located towards said leading edge and a second end located towards said trailing edge, wherein at least a portion of one of said first and second flow guide members extends along the transverse direction of said blade at an angle to said chord line of between +/−[15 to 60] degrees, wherein said flow channel comprises at least one constricted section spaced from said first end towards said second end, wherein the distance between said first and second flow guide members at said at least one constricted section is less than the distance between said first and second flow guide members at the first end of said flow channel, such that attached flow in said flow channel between said first and second flow guide members from said first end to said second end is subjected to a Venturi effect by said at least one constricted section, and wherein the length between said first end and said second end of said flow channel is between approximately 50-100% of chord length of the wind turbine blade at the location of said flow channel. 2. The wind turbine blade of claim 1 , wherein said at least one constricted section is located at said second end of said flow channel. 3. The wind turbine blade of claim 1 , wherein the flow channel of the wind turbine blade comprises at least one constricted section located between said first end and said second end. 4. The wind turbine blade of claim 1 , wherein the wind turbine blade comprises a first constricted section located between said first end and said second end of said flow channel and a second constricted section located at said second end of said flow channel, wherein the width of said flow channel between said first and second flow guide members tapers from said first end to said first constricted section and subsequently widens towards said second end to provide a first Venturi effect on flow in said flow channel, and wherein the width of said flow channel between said first and second flow guide members subsequently tapers towards said second constricted section at the second end of said flow guide channel to provide a second Venturi effect. 5. The wind turbine blade of claim 4 , wherein said first constricted section of said flow channel is located between said leading edge and said trailing edge approximately at the area of maximum thickness of the profiled contour. 6. The wind turbine blade of claim 1 , wherein said first and second flow guide members comprise respective flow channel surfaces, the flow channel surfaces of said first flow guide facing the flow channel surface of said second flow guide across said flow channel, wherein at least a portion of at least one of said flow channel surfaces is curved. 7. The wind turbine blade of claim 1 , wherein at least a portion of said first and second flow guide members extend in a convergent direction towards the second end of said flow channel to form said at least one constricted section, such that attached flow in said flow channel between said first and second flow guide members is subjected to a Venturi effect. 8. The wind turbine blade of claim 1 , wherein one of said first and second flow guide members extends substantially along the transverse direction of said blade at an angle to said chord line of between +/−[15 to 60] degrees, wherein the other of said first and second flow guide members extends along the transverse direction of said blade parallel to said chord line. 9. The wind turbine blade of claim 1 , wherein the flow guide members are formed from planar members projecting from the surface of the wind turbine blade. 10. The wind turbine blade of claim 9 , wherein the planar members projecting from the surface of the wind turbine blade comprise a stall fence or stall barrier. 11. The wind turbine blade of claim 1 , wherein said flow channel is formed from flow guide members provided on the suction side of the wind turbine blade. 12. The wind turbine blade of claim 1 , wherein said first and second flow guide members are located on the inboard portion of the blade. 13. The wind turbine blade of claim 12 , wherein said first and second flow guide members are located on the inboard portion of the blade within 50% of the length of the blade from the root end of the blade. 14. The wind turbine blade of claim 1 , wherein the width of said flow channel at said at least one constricted section is between approximately 50-80% of the width of said flow channel at said first end. 15. The wind turbine blade of claim 1 , wherein said first end of said flow channel is located adjacent the leading edge of the blade. 16. The wind turbine blade of claim 15 , wherein said first end of said flow channel is located adjacent the leading edge of the blade within approximately 20% of chord length of the wind turbine blade at the location of said flow channel. 17. A wind turbine having at least one wind turbine blade as claimed in claim 1 . 18. A wind turbine blade for a rotor of a wind turbine having a substantially horizontal rotor shaft, said rotor comprising a hub, from which the blade extends substantially in a radial direction when mounted to the hub, the blade having a longitudinal direction with a tip end and a root end and a transverse direction, the blade further comprising: a profiled contour including a pressure side and a suction side, as well as a leading edge and a trailing edge with a chord line having a chord length extending there between, the chord line transverse to said longitudinal direction, the profiled contour, when being impacted by an incident air-flow, generating a lift, wherein the wind turbine further comprises first and second flow guide members provided on a surface of said wind turbine blade, wherein said first and second flow guide members extend in a direction substantially transverse to the longitudinal direction of the blade, said first and second flow guide members defining a flow channel between said leading edge and said trailing edge, said flow channel having a first end located towards said leading edge and a second end located towards said trailing edge, wherein at least a portion of one of said first and second flow guide members extends along the transverse direction of said blade at an angle to said chord line of between +/−[15 to 60] degrees, wherein said flow channel comprises at least one constricted section spaced from said first end towards said second end, wherein the distance between said first and second flow guide members at said at
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