Noise reducer for rotor blade in wind turbine

• US 8,414,261 B2
• Filed: 05/31/2011
• Issued: 04/09/2013
• Est. Priority Date: 05/31/2011
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (General Electric Company)
• Original Assignee: General Electric Company
• Inventors: Bonnet, Laurent
• Primary Examiner(s): Look, Edward
• Assistant Examiner(s): DAVIS, JASON GREGORY
• Application Number:
  US13/149,513
• Publication Number:
  US 20120027590A1
• Time in Patent Office: 679 Days
• Field of Search: 244/200.1, 244/215, 415/119, 416/62, 416/228, 416/235, 416/236.R
• US Class Current: 416/1
• CPC Class Codes: F03D 1/0641 of the section profile of the blades, i.e. aerofoil profile
• CPC Class Codes: F05B 2240/30 Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
• CPC Class Codes: F05B 2260/962 by means creating "anti-noise"
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction

Abstract

A rotor blade assembly and a method for reducing the noise of a rotor blade for a wind turbine are disclosed. The rotor blade has surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root. The rotor blade assembly further includes a noise reducer configured on a surface of the rotor blade, the noise reducer including a plurality of noise reduction features. Each of the plurality of noise reduction features includes a first surface and a second surface. The first surface includes a first portion mounted to one of the pressure side or the suction side and a second portion configured to interact with wind flowing past the other of the pressure side or the suction side. The second surface interrupts an aerodynamic contour of the one of the pressure side or the suction side.

Claims

1. A rotor blade assembly for a wind turbine, comprising:

a rotor blade having surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root; and

,

a noise reducer configured on a surface of the rotor blade, the noise reducer comprising a plurality of noise reduction features, each of the plurality of noise reduction features comprising;

a first surface comprising a first portion mounted to one of the pressure side or the suction side and a second portion configured to interact with wind flowing past the other of the pressure side or the suction side;

a second surface interrupting an aerodynamic contour of the one of the pressure side or the suction side, and

a first layer and a second layer, the first layer comprising the first portion and second surface of each of the plurality of noise reduction features and the second layer comprising the second portion, wherein the first layer is formed from an acoustic absorption material.

2. The rotor blade assembly of claim 1, wherein each of the plurality of second surfaces defines a width and a length, and wherein the width tapers in the direction of the wind flow through a portion of the length.

3. The rotor blade assembly of claim 1, wherein each of the plurality of second surfaces defines a height and a length, and wherein the height tapers in the direction of the wind flow through a portion of the length.

4. The rotor blade assembly of claim 1, wherein the second surface has a generally curvilinear cross-sectional profile.

5. The rotor blade assembly of claim 1, wherein the first portion is mounted to the suction side, the second portion is configured to interact with wind flowing past the pressure side, and the second surface interrupts the aerodynamic contour of the suction side.

6. The rotor blade assembly of claim 1, wherein the plurality of noise reduction features comprise a first noise reduction feature having a first aspect ratio and a second noise reduction feature having a second aspect ratio different from the first aspect ratio.

7. The rotor blade assembly of claim 1, wherein the noise reducer further comprises a base plate mounting each of the plurality of first portions to the one of the pressure side or the suction side.

8. The rotor blade assembly of claim 1, wherein the first portion is mounted within an outer board area of the rotor blade.

9. The rotor blade assembly of claim 1, wherein the noise reducer is configured adjacent the trailing edge of the rotor blade.

10. The rotor blade assembly of claim 1, wherein the second layer is at least one of stiffer or stronger than the first layer.

11. The rotor blade assembly of claim 1, wherein the first layer has an absorption coefficient in the range between approximately 0.6 and approximately 1.0.

12. The rotor blade assembly of claim 1, wherein the second layer is acoustically non-porous.

13. A wind turbine, comprising:

a plurality of rotor blades, each of the plurality of rotor blades having surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root; and

,

a noise reducer configured on a surface of at least one of the plurality of rotor blades, the noise reducer comprising a plurality of noise reduction features, each of the plurality of noise reduction features comprising;

a first surface comprising a first portion mounted to one of the pressure side or the suction side and a second portion configured to interact with wind flowing past the other of the pressure side or the suction side;

a second surface interrupting an aerodynamic contour of the one of the pressure side or the suction side; and

a first layer and a second layer, the first layer comprising the first portion and second surface of each of the plurality of noise reduction features and the second layer comprising the second portion, wherein the first layer is formed from an acoustic absorption material.

14. The wind turbine of claim 13, wherein the plurality of noise reduction features comprise a first noise reduction feature having a first aspect ratio and a second noise reduction feature having a second aspect ratio.

15. The wind turbine of claim 13, wherein the noise reducer further comprises a base plate mounting each of the plurality of first portions to the one of the pressure side or the suction side.

16. The wind turbine of claim 13, wherein the first portion is mounted within an outer board area of the rotor blade.

17. The wind turbine of claim 13, wherein the noise reducer is configured adjacent the trailing edge of the rotor blade.

18. A method for reducing the noise of a rotor blade for a wind turbine, the method comprising:

mounting a noise reducer on a rotor blade, the noise reducer comprising a plurality of noise reduction features, each of the plurality of noise reduction features comprising a first surface comprising a first portion mounted to one of a pressure side or a suction side of the rotor blade and a second portion configured to interact with wind flowing past the other of the pressure side or the suction side, a second surface interrupting an aerodynamic contour of the one of the pressure side or the suction side, and a first layer and a second layer, the first layer comprising the first portion and second surface of each of the plurality of noise reduction features and the second layer comprising the second portion, wherein the first layer is formed from an acoustic absorption material; and

,

rotating the rotor blade on the wind turbine.