IP Library Granted Patent US 8,444,384
Granted Patent B2
US 8,444,384 · App. 13/217,848 · Granted May 21, 2013

Rotor blade assembly and method for adjusting loading capability of rotor blade

Inventor: David Samuel Pesetsky (Greenville, SC)
Assignee: General Electric Company
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Quick Facts
Patent No.
US 8,444,384
App. No.
13/217,848
Granted
May 21, 2013
Kind
B2
Abstract

A rotor blade assembly and a method for adjusting a loading capability of a rotor blade are disclosed. The rotor blade assembly includes 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. The rotor blade further defines a span and a chord. The rotor blade assembly further includes a spoiler assembly operable to alter a flow past a surface of the rotor blade. The spoiler assembly is incrementally deployable from the surface along one of a length or a width of the spoiler assembly.

Claims (25)

1. A rotor blade assembly, 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, the rotor blade further defining a span and a chord; and,

a spoiler assembly operable to alter a flow past a surface of the rotor blade, the spoiler assembly comprising a spoiler and a plurality of actuators connected to the spoiler, the spoiler incrementally deployable from the surface along one of a length or a width of the spoiler assembly.

2. The rotor blade assembly of claim 1 , wherein the spoiler is incrementally deployable along the span.

3. The rotor blade assembly of claim 2 , wherein the spoiler is incrementally deployable from an inboard end to an outboard end.

4. The rotor blade assembly of claim 1 , further comprising a controller in operable communication with the spoiler assembly.

5. The rotor blade assembly of claim 1 , wherein the spoiler assembly is positioned adjacent the leading edge.

6. The rotor blade assembly of claim 1 , wherein the spoiler assembly is deployable from the suction side.

7. The rotor blade assembly of claim 1 , wherein the spoiler is incrementally deployable along the chord.

8. A wind turbine, comprising:

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

a spoiler assembly operable to alter a flow past a surface of one of the plurality of rotor blades, the spoiler assembly comprising a spoiler and a plurality of actuators connected to the spoiler, the spoiler incrementally deployable from the surface along one of a length or a width of the spoiler assembly.

9. The wind turbine of claim 8 , wherein the spoiler is incrementally deployable along the span.

10. The wind turbine of claim 9 , wherein the spoiler is incrementally deployable from an inboard end to an outboard end.

11. The wind turbine of claim 8 , further comprising a controller in operable communication with the spoiler assembly.

12. The wind turbine of claim 8 , wherein the spoiler is incrementally deployable along the chord.

13. A rotor blade assembly, 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, the rotor blade further defining a span and a chord; and,

a spoiler assembly operable to alter a flow past a surface of the rotor blade, the spoiler assembly comprising a plurality of spoilers and an actuator connected to the plurality of spoilers, the actuator comprising a movable track and a roller, wherein movement of the roller along the movable track causes incremental deployment of the spoiler assembly from the surface along one of a length or a width of the spoiler assembly.

14. The rotor blade assembly of claim 13 , wherein the spoiler is incrementally deployable along the span.

15. The rotor blade assembly of claim 13 , wherein the spoiler is incrementally deployable from an inboard end to an outboard end.

16. The rotor blade assembly of claim 13 , further comprising a controller in operable communication with the spoiler assembly.

17. The rotor blade assembly of claim 13 , wherein the spoiler assembly is positioned adjacent the leading edge.

18. The rotor blade assembly of claim 13 , wherein the spoiler assembly is deployable from the suction side.

19. The rotor blade assembly of claim 13 , wherein the spoiler assembly is incrementally deployable along the chord.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 22, 2024
From: LM WIND POWER US TECHNOLOGY APS
To: GE INFRASTRUCTURE TECHNOLOGY LLC
Reel/Frame 066869/0770 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 9, 2023
From: GENERAL ELECTRIC COMPANY
To: LM WIND POWER US TECHNOLOGY APS
Reel/Frame 065531/0160 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 25, 2011
From: PESETSKY, DAVID SAMUEL
To: GENERAL ELECTRIC COMPANY
Reel/Frame 026808/0648 →
Continuity (1)
Related Publication 20120141268A1 · Jun 7, 2012