System and method for trailing edge noise reduction of a wind turbine blade

Patent metadata

Field	Value
Publication number	US-9951749-B2
Application number	US-201314437641-A
Country	US
Kind code	B2
Filing date	Oct 24, 2013
Priority date	Oct 26, 2012
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

A system and method for reducing the operational noise of a blunt trailing edge of a wind turbine blade is described. The system involves increasing the trailing edge solid angle at the blade trailing edge by providing a wedge element or projection adjacent the trailing edge of the blade, the wedge element acting to provide improved mixing of the suction side and pressure side flows at the blunt trailing edge, thereby reducing the strength of vortex shedding at the trailing edge and the associated operational noise.

First claim

The invention claimed is:

1. A method of reducing a trailing edge noise of a wind turbine blade having a trailing edge, the wind turbine blade having a trailing edge solid angle at the trailing edge, wherein the trailing edge is a blunt trailing edge, and wherein at least one wedge element is located on an inboard portion of the wind turbine blade within 50% of a blade length from a root end of the wind turbine blade, the method comprising the steps of:
increasing the trailing edge solid angle of the trailing edge to reduce the strength of vortex shedding formed behind the trailing edge of the wind turbine blade.

2. The method of claim 1 , wherein a pressure-side airflow and a suction side airflow over an airfoil profile of the wind turbine blade intersect in a wake of the trailing edge at an intersecting flow angle, and wherein the step of increasing the trailing edge solid angle of the blade acts to increase the intersecting flow angle.

3. The method of claim 1 , wherein the method comprises the steps of:
providing a wind turbine blade having an airfoil profile comprising a trailing edge, the airfoil trailing edge having a trailing edge solid angle Ψ 1 ; and
providing a wedge element adjacent the trailing edge, the wedge element having a first inclined or curved or sloped surface, the first inclined or curved or sloped surface tapered towards a first end provided at the trailing edge, the wedge element having a solid angle Ψ 2 at the first end,
such that the wind turbine blade comprises an effective trailing edge solid angle Ψ′, wherein Ψ′=Ψ 1 +Ψ 2 .

4. The method of claim 3 , wherein the wedge element is provided on a pressure side or an upwind side of the airfoil profile.

5. The method of claim 3 , wherein the wedge element is provided wherein Ψ 2 is between 5-15 degrees.

6. The method of claim 3 , wherein the wedge element is provided as an add-on device which can be attached to an existing wind turbine blade.

7. The method of claim 3 , wherein the wedge element is provided as an integral part of a wind turbine blade body.

8. The method of claim 3 , wherein the airfoil profile and the wedge element are selected such that Ψ′ is less than 90 degrees.

9. The method of claim 8 , wherein Ψ′ is less than 60 degrees.

10. A wind turbine blade for a rotor of a wind turbine having a substantially horizontal rotor shaft, the rotor comprising a hub, from which the wind turbine blade extends substantially in a radial direction when mounted to the hub, the wind turbine blade extending in a longitudinal direction parallel to a longitudinal axis and having a tip end and a root end,
the wind turbine blade further comprising a profiled airfoil contour including a pressure side and a suction side, as well as a leading edge and a trailing edge with a chord having a chord length extending therebetween, the profiled airfoil contour, when being impacted by an incident airflow, generating a lift, wherein the profiled airfoil contour comprises a trailing edge solid angle Ψ 1 at said trailing edge,
wherein the wind turbine blade is configured to have an increased trailing edge solid angle at the trailing edge, compared to the trailing edge solid angle Ψ 1 , to reduce the strength of vortex shedding formed behind the trailing edge of the wind turbine blade,
wherein the trailing edge is a blunt trailing edge, and
wherein at least one wedge element is located on an inboard portion of the wind turbine blade within 50% of a blade length from the root end of the wind turbine blade.

11. The wind turbine blade of claim 10 , wherein the wind turbine blade further comprises at least one wedge element provided on the pressure side and/or the suction side of the blade towards the trailing edge, the at least one wedge element having a first inclined or curved or sloped surface, the first inclined or curved or sloped surface tapered towards a first end provided at the trailing edge, and the wedge element having a solid angle Ψ 2 at the first end,
such that the wind turbine blade comprises an effective trailing edge solid angle Ψ′ at the trailing edge of the wind turbine blade, wherein Ψ′=Ψ 1 +Ψ 2 .

12. The wind turbine blade of claim 11 , wherein the at least one wedge element is provided on the pressure side or upwind side of the profiled airfoil contour.

13. The wind turbine blade of claim 11 , wherein Ψ 2 is between 5-15 degrees.

14. The wind turbine blade of claim 11 , wherein each of the at least one wedge elements comprise at least one projection extending from the first end provided at the trailing edge, the projection acting to reduce vortex shedding in a wake of the wind turbine blade trailing edge.

15. The wind turbine blade of claim 11 , wherein the at least one wedge element has a substantially triangular-shaped cross-section, wherein the at least one wedge element comprises:
a first end located towards the trailing edge;
a second end located towards the leading edge;
a base side extending between the first end and the second end adjacent a surface of the profiled airfoil contour; and
a distal apex point located between the first end and the second end opposite the base side, wherein the at least one wedge element further comprises a first inclined or curved or sloped surface extending between the distal apex point and the first end and a second inclined or curved or sloped surface extending between the distal apex point and the second end, and wherein the first and second surfaces are shaped to provide attached flow over the at least one wedge element.

16. The wind turbine blade of claim 15 , wherein the distal apex point is located at a distance h from the base side, wherein distance h may vary along a length of the at least one wedge element.

17. The wind turbine blade of claim 10 , wherein the at least one wedge element has a substantially triangular-shaped cross-section, wherein the at least one wedge element comprises:
a first end located towards the trailing edge;
a second end located towards the leading edge;
a base side extending between the first end and the second end adjacent a surface of the profiled airfoil contour; and
a distal apex point located between the first end and the second end opposite the base side, and wherein
L te is the distance along the base side between the first end of the wedge element and a projection of the distal apex point onto the base side,
L le is the distance along the base side between the second end of the wedge element and the projection of the distal apex point onto the base side, and
L is the length of the base side between the first end and the second end, wherein
L=L te +L le , 5%<L<15% of the chord length of the blade airfoil profile.

18. The wind turbine blade of claim 11 , wherein the profiled airfoil contour and the wedge element are selected such that Ψ′ is less than 90 degrees.

19. A wind turbine comprising at least one wind turbine blade as claimed in claim 10 .

20. The wind turbine blade of claim 17 , wherein L=L te +L le , 5%<L<10% of the chord length of the blade airfoil profile.

21. The wind turbine blade of claim 18 , wherein Ψ′ is less than 60 degrees.

Assignees

• Lm Wp Patent Holding As

Inventors

• Singh Ashish
• Ramanathan Ganesh
• Bijlani Jitendra
• Parihar Naveen

Classifications

• F03D1/065 Primary

  characterised by their construction elements (F03D13/10 takes precedence) · CPC title

• Y02E10/723

  Cross-Sectional Technologies · mapped topic

• F03D7/0296

  to prevent, counteract or reduce noise emissions · CPC title

• F03D1/0683

  Mechanical Engineering · mapped topic

• F03D1/0641 Primary

  of the section profile of the blades, i.e. aerofoil profile · CPC title