초록 ▼

A rotor blade 1 includes a main blade section 10, and an extension flap 20. The extension flap 20 is moveable relative to the main blade section 10. At least the main blade section 10 and the extension flap 20 form an airfoil lifting surface of the blade. A dimension of the airfoil lifting surface i

A rotor blade 1 includes a main blade section 10, and an extension flap 20. The extension flap 20 is moveable relative to the main blade section 10. At least the main blade section 10 and the extension flap 20 form an airfoil lifting surface of the blade. A dimension of the airfoil lifting surface is variable by moving the extension flap 20 relative to the main blade section 10.

대표청구항 ▼

What is claimed is: 1. A rotor blade for a wind turbine, the rotor blade comprising: a main blade section comprising a trailing edge side and a root end; an extension flap provided at the root end of the trailing edge side of the main blade section and movable relative to the main blade section alo

What is claimed is: 1. A rotor blade for a wind turbine, the rotor blade comprising: a main blade section comprising a trailing edge side and a root end; an extension flap provided at the root end of the trailing edge side of the main blade section and movable relative to the main blade section along a chord direction of the rotor blade; and wherein a length of the extension flap is less than one-half of a length of the main blade section. 2. The rotor blade of claim 1, wherein the extension flap is movable relative to the main blade section in the chord direction between a retracted position and a deployed position. 3. The rotor blade of claim 2, wherein the trailing edge side of the main blade section comprises a portion having a substantially straight edge in a span wide direction, and wherein the extension flap is provided at the portion having the substantially straight edge. 4. The rotor blade of claim 2, wherein the extension flap has a chord length that is more than a tenth of a maximum chord length of the main blade section. 5. The rotor blade of claim 2, wherein the rotor blade has a maximum chord length that is variable by more than a fifth of a maximum chord length of the main blade section. 6. The rotor blade of claim 2, wherein a maximum chord length of the rotor blade is less than about 4.2 meters when the extension flap is in the retraced position, and wherein the maximum chord length is more than about 4.2 meters when the extension flap is in the deployed position. 7. The rotor blade of claim 2, further comprising a driving mechanism for moving the extension flap relative to the main blade section in the chord direction. 8. The rotor blade of to claim 7, wherein the driving mechanism comprises a retraction system that is adapted for retracting the extension flap towards the main blade section. 9. The rotor blade of claim 2, wherein the extension flap has a curvature that matches approximately a curvature associated with the main blade section. 10. The rotor blade of to claim 9, wherein the curvature matches approximately a curvature of a camber line of the main blade section, or matches approximately a curvature of one of a pressure side surface and a suction side surface of the main blade section. 11. The rotor blade of claim 2, wherein the extension flap is slidable relative to the main blade section in the chord direction. 12. The rotor blade of claim 11, wherein the main blade section comprises a sliding guide for guiding the extension flap. 13. The rotor blade of claim 12, wherein the sliding guide is formed for allowing a sliding motion of the extension flap substantially along a curved external surface of the main blade section. 14. The rotor blade of claim 2, wherein the extension flap is at least partially retractable inside the main blade section. 15. The rotor blade of to claim 2, wherein in the retracted position the extension flap is retractable to an external surface of the main blade section. 16. The rotor blade of claim 1, wherein the extension flap is connected to the main blade section by at least one pivot linkage. 17. The rotor blade of claim 9, wherein an upper surface of the extension flap substantially lies on a same plane of an upper surface of the main blade section. 18. The rotor blade of claim 1, wherein a trailing edge of the extension flap aligns with a trailing edge of the main blade section. 19. A wind turbine comprising: a rotor blade comprising: a main blade section comprising a trailing edge side and a root end; an extension flap provided at the root end of the trailing edge side of the main blade section and movable relative to the main blade section along a chord direction of the rotor blade; and wherein a length of the extension flap is less than one-half of a length of the main blade section. 20. The wind turbine according to claim 19, further comprising: a first driving mechanism for moving the extension flap relative to the main blade section in the chord direction; and a second driving mechanism for adjusting a pitch angle of the rotor blade. 21. The wind turbine according to claim 20, further comprising: a wind data sensing system; and a controller adapted for controlling the first driving mechanism and the second driving mechanism in response to wind data received from the wind data sensing system. 22. A method of controlling a wind turbine having at least one rotor blade, the method comprising: collecting wind data; moving, in response to the collected wind data, an extension flap of the at least one rotor blade of the wind turbine relative to a main blade section of the at least one rotor blade along a chord direction of the at least one rotor blade, the extension flap being connected to the main blade section along a root end of a trailing edge side of the main blade section, thereby varying a dimension of an airfoil lifting surface of the at least one rotor blade in response to the collected wind data; and wherein a length of the extension flap is less than one-half of a length of the main blade section.