Cyclic Pitch Control System for Wind Turbine Blades

• US 20130045098A1
• Filed: 08/18/2011
• Published: 02/21/2013
• Est. Priority Date: 08/18/2011
• Status: Abandoned Application

• Current Assignee: Clipper Windpower, LLC
• Original Assignee: Clipper Windpower, LLC
• Inventors: Taylor, Nathaniel Brook
• Application Number:
  US13/212,646
• Publication Number:
  US 20130045098A1
• Time in Patent Office: Days
• US Class Current: 416/1
• CPC Class Codes: F03D 7/0224 Adjusting blade pitch
• CPC Class Codes: F03D 7/024 of individual blades
• CPC Class Codes: F03D 7/043 characterised by the type of control logic
• CPC Class Codes: F05B 2270/17 to avoid excessive deflection of the blades
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction

Abstract

In a wind turbine, an open loop control algorithm for incrementally or positively adjusting the pitch angles of individual rotor blades may be used to increase spacing between the base of the turbine tower and an approaching blade tip. As each rotating blade passes in front of the tower base, a minimum clearance distance may be assured to avoid blade tip strikes of the base. In accordance with at least one embodiment of the control algorithm, as each blade approaches the tower base, it may be feathered to reduce its power loading, and to facilitate increased clearance beyond the normal unloading or feathering produced by the so-called tower shadow effect. To offset resultant loss of torque, the remaining blades may be correspondingly pitched toward power, i.e. into the wind, to balance and/or smooth out the overall rotor torque curve, and thus to avoid torque ripples.

Claims

1. A method of increasing the clearance between a blade tip and a base of a tower for tower-crossing rotor blades of a wind turbine having a tower and a plurality of wind-driven rotatable blades supported thereon, comprising:

a) providing a control system adapted to feather individual blades of said plurality of blades;

b) providing an azimuthal encoder for electronic communication with said control system;

c) having the azimuthal encoder provide input to said control system to sense the approach of any one of said plurality of blades to said base in real-time; and

,

d) having the control system respond to said encoder input by feathering each said approaching tower-crossing blade as a function of a sensed azimuthal position of said blade.

2. The method of claim 1, wherein said control system returns said blade to a power pitch position after said blade has traveled beyond said tower base.

3. The method of claim 1, wherein said control system is adapted to initiate said feathering of said approaching blade at a predetermined azimuthal position.

4. The method of claim 1, wherein said control system response to said azimuthal position is calculated by said control system as a function of operating conditions, including rotor speed.

5. The method of claim 2, wherein a maximum incremental pitch angle adjustment is a function of current operating conditions.

6. The method of claim 1, wherein said control system response to said azimuthal position is also a function of current operating conditions.

7. The method of claim 2, wherein said control system is adapted to have the blade fully returned to said power pitch position at a predetermined azimuthal position.

8. The method of claim 3, wherein said predetermined azimuthal position of said approaching blade is within a target range of 100°

to 160°

.

9. The method of claim 7, wherein said predetermined azimuthal position of said blade is within a target range of 200°

to 260 °

.

10. The method of claim 1, wherein said control system is an open loop system based on the azimuthal position of the blade being feathered.

11. The method of claim 1 wherein a peak incremental pitch angle adjustment occurs at an azimuthal position of less than 180°

.

12. A method of increasing the clearance between a blade tip and a base of a tower for tower-crossing rotor blades of a wind turbine having a tower and a plurality of wind-driven rotatable blades supported thereon, comprising:

a) providing a control system adapted to feather individual blades of said plurality of blades;

b) providing an azimuthal encoder for electronic communication with said control system;

c) having the azimuthal encoder provide input to said control system to sense the azimuthal position of the blades;

d) having the control system respond to said encoder input by feathering each said approaching tower-crossing blade as a function of a sensed azimuthal position of said blade; and

,

e) having the control system respond to said encoder input by over-pitching the remaining, non-tower crossing, blades as each tower-crossing blade is feathered, to compensate for loss of torque attributable to the feathering of the tower crossing blade.

13. The method of claim 12, wherein said control system returns said tower-crossing blade to a power pitch position after said blade has traveled beyond said tower base.

14. The method of claim 12, wherein said control system is adapted to initiate said feathering of said approaching blade at a predetermined azimuthal position.

15. The method of claim 13, wherein said control system is adapted to have the blade fully returned to said power pitch position at a predetermined azimuthal position.

16. The method of claim 14, wherein said predetermined azimuthal position of said approaching blade is within a target range of 100°

to 160°

.

17. The method of claim 15, wherein said predetermined azimuthal position of said blade is within a target range of 200°

to 260°

.

18. The method of claim 12, wherein said control system is an open loop system based on azimuthal position of the blade being feathered.

19. The method of claim 12 wherein a peak incremental pitch angle adjustment occurs at an azimuthal position of less than 180°

.