Flexible flap arrangement for a wind turbine rotor blade

US9945357B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9945357-B2
Application numberUS-201313763786-A
CountryUS
Kind codeB2
Filing dateFeb 11, 2013
Priority dateApr 4, 2012
Publication dateApr 17, 2018
Grant dateApr 17, 2018

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A flap arrangement for a wind turbine rotor blade, which includes a leading edge, a trailing edge and a chord line between the leading edge and the trailing edge, is described. The flap arrangement includes a support portion and a flap portion which is passively moveable with respect to an angle between a surface normal of a surface of the flap portion and the chord line. The support portion and the flap portion are positioned relatively to each other such that the support portion provides a limit to the movement of the flap portion. Also described are a wind turbine rotor blade including the flap arrangement and a method of enhancing the aerodynamic performance of a blade.

First claim

Opening claim text (preview).

The invention claimed is: 1. A flap arrangement for a wind turbine rotor blade, comprising a leading edge, a trailing edge and a chord line between the leading edge and the trailing edge, the flap arrangement comprising: a support portion adapted to prolong a suction side of the wind turbine rotor blade; and a flap portion adapted to prolong a pressure side of the wind turbine rotor blade and passively moveable with respect to an angle between a surface normal of a surface of the flap portion and the chord line, wherein the support portion and the flap portion are positioned relative to each other such that the support portion provides a limit to the movement of the flap portion. 2. The flap arrangement as claimed in claim 1 , wherein the support portion comprises a pressure side surface and a suction side surface, and the suction side surface of the support portion prolongs the suction side of the wind turbine rotor blade, and wherein the flap portion comprises a suction side surface and a pressure side surface, and the pressure side surface of the flap portion prolongs the pressure side of the wind turbine rotor blade. 3. The flap arrangement as claimed in claim 2 , wherein the suction side surface of the flap portion and the pressure side surface of the support portion faces towards each other. 4. The flap arrangement as claimed in claim 1 , the support portion and/or the flap portion is connectable to a wind turbine rotor blade at the trailing edge of the blade or at a portion of the blade close to the trailing edge, and/or at a position between the tip of the blade and one half of the span length of the blade measured from the tip. 5. The flap arrangement as claimed in claim 1 , the flap portion comprises a flexible or hinged flap connection for connecting the flap portion to a wind turbine rotor blade. 6. The flap arrangement as claimed in claim 1 , wherein the flap portion comprises a flexible sheet. 7. The flap arrangement as claimed in claim 1 , the flap portion and/or the support portion comprises a serrated trailing edge. 8. The flap arrangement as claimed in claim 1 , the flap portion and the support portion are made as one piece or several pieces. 9. The flap arrangement as claimed in any claim 1 , the support portion comprises a vortex generator. 10. The flap arrangement as claimed in claim 1 the support portion has a bend shape. 11. A wind turbine rotor blade comprising a flap arrangement as claimed in claim 1 . 12. The wind turbine rotor blade as claimed in claim 11 wherein the support portion comprises a vortex generator. 13. The wind turbine rotor blade as claimed in claim 11 , a plurality of flap arrangements are mounted next to one another along the trailing edge of the blade. 14. The wind turbine rotor blade as claimed in claim 11 , support portion is an integral part of the blade. 15. A wind turbine comprising a wind turbine rotor blade as claimed in claim 11 . 16. A method for enhancing the aerodynamic performance of a wind turbine rotor blade comprising a trailing edge, comprising: connecting a flap arrangement as claimed in claim 1 along the trailing edge of the blade. 17. A flap arrangement for a wind turbine rotor blade, comprising a leading edge, a trailing edge and a chord line between the leading edge and the trailing edge, the flap arrangement comprising: a support portion adapted to prolong a suction side of the blade; and a flap portion adapted to prolong a pressures side of the blade and passively moveable with respect to the support portion and with respect to an angle between a surface normal of a surface of the flap portion and the chord line, wherein the support portion and the flap portion are positioned relative to each other such that the support portion provides a limit to the movement of the flap portion, and wherein in a first state the flap portion is in contact with the support portion and in a second state a gap occurs between the flap portion. 18. The flap arrangement as claimed in claim 17 , wherein the support portion comprises a pressure side surface and a suction side surface, and the suction side surface of the support portion prolongs the suction side of the wind turbine rotor blade, and wherein the flap portion comprises a suction side surface and a pressure side surface, and the pressure side surface of the flap portion prolongs a pressure side of a wind turbine rotor blade. 19. The flap arrangement as claimed in claim 18 , wherein the gap in the second state occurs between the pressure side surface of the support portion and the suction side surface of the flap portion. 20. A wind turbine rotor blade comprising a flap arrangement as claimed in claim 19 .

Assignees

Inventors

Classifications

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

  • Cross-Sectional Technologies · mapped topic

  • F03D7/0232Primary

    with flaps or slats (with aerodynamic drag devices on the blades for braking F03D7/0252) · CPC title

  • for orientation in relation to wind direction · CPC title

  • Vortex generators, turbulators, or the like, for mixing · CPC title

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Frequently asked questions

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What does patent US9945357B2 cover?
A flap arrangement for a wind turbine rotor blade, which includes a leading edge, a trailing edge and a chord line between the leading edge and the trailing edge, is described. The flap arrangement includes a support portion and a flap portion which is passively moveable with respect to an angle between a surface normal of a surface of the flap portion and the chord line. The support portion an…
Who is the assignee on this patent?
Enevoldsen Peder Bay, Siemens Ag
What technology area does this patent fall under?
Primary CPC classification F03D7/0232. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 17 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).