Secondary airfoil mounted on stall fence on wind turbine blade
View Patent ↗An airfoil ( 26, 62, 64 ) is mounted on a chordwise stall fence ( 28 ) of a wind turbine blade ( 22 ). The airfoil may be an aerodynamic slat ( 26 ) positioned over a forward portion of the suction side ( 38 ) of the blade or a flap ( 63 ) disposed near a trailing edge ( 34 ) of the blade. The stall fence may be at least as high as the thickness of the boundary layer ( 39 ) of air passing over the blade. The slat or flap may be twisted between an inboard end ( 26 A) and an outboard end ( 26 B) to compensate for the radially varying angle of the relative air inflow ( 46 A, 46 B).
1. A wind turbine blade comprising:
a main element;
a stall fence extending over at least most of a chordwise length of the main element; and
a slat mounted on the stall fence over a forward portion of a suction side of the main element;
wherein the slat is positioned to reduce a separation of airflow from the suction side of the airfoil; and
wherein the slat is twisted between an inboard end and an outboard end of the slat such that an angle between a chord of the slat and a rotation plane of the blade decreases with distance from a center of rotation of the blade.
2. The wind turbine blade of claim 1 , further comprising an intermediate airfoil disposed on the stall fence over an intermediate position of the chordwise length of the main element.
3. The wind turbine blade of claim 1 , wherein the slat inboard end is positioned over a leading edge of the wind turbine blade.
4. The wind turbine blade of claim 1 , further comprising a flap disposed on the stall fence partially or completely behind a trailing edge of the main element.
5. The wind turbine blade of claim 4 , wherein the stall fence extends over at least a portion of a suction side of the flap.
6. The wind turbine blade of claim 4 , wherein at least a portion of a leading edge of the flap is disposed below the trailing edge of the main element such that a portion of an airflow flows from a pressure side of the main element to a suction side of the flap.
7. A wind turbine blade comprising:
a radially inboard portion with a stall fence extending over at least most of a chordwise length of a suction side of the blade; and
an aerodynamic slat mounted on and across the stall fence with a clearance over a forward portion of the suction side of the blade effective to reduce a separation of an airflow over the suction side of the airfoil;
wherein the slat is twisted between an inboard end and an outboard end of the slat such that an angle between a chord of the slat and a rotation plane of the blade decreases with distance from a center of rotation of the blade.
8. The wind turbine blade of claim 7 , wherein the stall fence is at least as tall as an aerodynamic boundary layer on the suction side of the blade.
9. The wind turbine blade of claim 7 , wherein the stall fence has a median height of 2-8% of a chord length of the blade at the stall fence, and the stall fence has a height under the slat of 4-12% of said chord length, defining the clearance of the slat.
10. The wind turbine blade of claim 7 , wherein the stall fence varies gradually in height from a maximum height under the slat to a lesser height remote from under the slat.
11. The wind turbine blade of claim 7 , wherein the stall fence extends behind the trailing edge of the blade.
12. The wind turbine blade of claim 11 , further comprising a flap disposed on the stall fence partially or completely behind the trailing edge.
13. The wind turbine blade of claim 7 , wherein the slat extends beyond the fence in both radial directions by at least a median height of the fence.
14. A wind turbine blade comprising:
a radially inboard portion with a plurality of chordwise stall fences extending over at least most of a chordwise length of a suction side of a main element of the blade; and
an aerodynamic slat mounted on and across the stall fences with a clearance over a forward portion of the suction side of the main element that is effective to reduce an airflow separation over the suction side of the airfoil;
wherein the slat is twisted between an inboard end and an outboard end of the slat such that an angle between a chord of the slat and a rotation plane of the blade decreases with distance from a center of rotation of the blade.
15. The wind turbine blade of claim 14 , wherein each of the stall fences extends behind a trailing edge of the main element, and further comprising a flap disposed on the stall fences partially or completely behind the trailing edge.
16. The wind turbine blade of claim 15 , further comprising at least a portion of a leading edge of the flap being disposed below the trailing edge of the main element such that a portion of an airflow flows from a pressure side of the main element to a suction side of the flap.
17. The wind turbine blade of claim 1 , wherein the twist of the slat causes the inboard end of the slat to be positioned over the leading edge of the blade, and the outboard end of the slat to be positioned farther back from the leading edge.
18. The wind turbine blade of claim 7 , wherein the twist of the slat causes the inboard end of the slat to be positioned more toward or over the leading edge of the blade, and the outboard end of the slat to be positioned farther back from the leading edge.