Lift influencing device for a rotor blade of a wind turbine

Patent metadata

Field	Value
Publication number	US-10408192-B2
Application number	US-201514806913-A
Country	US
Kind code	B2
Filing date	Jul 23, 2015
Priority date	Sep 19, 2014
Publication date	Sep 10, 2019
Grant date	Sep 10, 2019

Abstract

A rotor blade of a wind turbine, wherein the rotor blade includes a lift modifying device, is provided. The lift modifying device is a part of the trailing edge section of the rotor blade. The lift modifying device is configured such that, at a predetermined loading of the trailing edge section, an air channel opens up a flow path from the pressure side to the suction side and vice versa in the trailing edge section. As a consequence, airflow flowing from the leading edge section of the rotor blade to the trailing edge section is at least partly deflected by the open air channel, which results in a modification of the lift of the rotor blade. A method to modify the lift of a rotor blade of a wind turbine is also provided.

First claim

The invention claimed is:

1. A rotor blade of a wind turbine with a lift modifying device, comprising:
a pressure side;
a suction side;
a leading edge section with a leading edge; and
a trailing edge section with a trailing edge,
wherein the lift modifying device is a part of the trailing edge section, and the lift modifying device is configured such that, at a predetermined loading of the trailing edge section when forces due to airflow that is flowing from the leading edge to the trailing edge acting on the trailing edge section exceed a threshold, an air channel opens up a flow path from the pressure side to the suction side and vice versa in the trailing edge section, such that airflow flowing from the leading edge section to the trailing edge section is at least partly deflected by the open air channel, which results in a modification of the lift of the rotor blade;
wherein the lift modifying device is located upstream of the trailing edge of the trailing edge section of the rotor blade;
wherein the lift modifying device is a single component that is flush with a surface of the pressure side and a surface of the suction side when in a closed position;
wherein the trailing edge section comprises an extension part which is separate from a remaining trailing edge section, the extension part being attached to the pressure side of the rotor blade and the remaining trailing edge section, and the lift modifying device being a part of the extension part.

2. The rotor blade according to claim 1 , wherein the trailing edge section with the lift modifying device is built as one, single piece.

3. The rotor blade according to claim 1 , wherein the rotor blade comprises a plurality of lift modifying devices, which are arranged in a spanwise direction along the trailing edge section, such that the lift of the rotor blade is modified locally with regard to a spanwise position along the rotor blade.

4. The rotor blade according to claim 1 , wherein at a first predetermined loading, a force from the suction side is applied on the trailing edge section of the rotor blade, thus opening up the lift modifying device towards the pressure side of the rotor blade.

5. The rotor blade according to claim 1 , wherein at a second predetermined loading, a force from the pressure side is applied on the trailing edge section of the rotor blade, thus opening up the lift modifying device towards the suction side of the rotor blade.

6. The rotor blade according claim 1 , wherein the lift modifying device comprises a mechanism that prevents the lift modifying device from opening up towards the pressure side, thus only allowing the lift modifying device to open up towards the suction side, or that prevents the lift modifying device from opening up towards the suction side, thus only allowing that the lift modifying device open up towards the pressure side.

7. The rotor blade according to claim 6 , wherein the mechanism includes a rim of the lift modifying device that at least partly overlaps with a rim of the air channel in a closed state of the air channel.

8. The rotor blade according to claim 1 , wherein the lift modifying device comprises a leading edge device portion facing towards the leading edge section of the rotor blade and a trailing edge device portion being opposite to the leading edge device portion, the lift modifying device opening up at either the leading edge device portion or the trailing edge device portion.

9. The rotor blade according to claim 1 , wherein the lift modifying device is attached to the remaining trailing edge section by a mechanical hinge, which comprises a torsional spring, thus the lift modifying device is arranged and prepared for passively opening up the air channel at a predetermined loading of the trailing edge section.

10. The rotor blade according to claim 1 , wherein the lift modifying device is firmly attached to the trailing edge section, and the lift modifying device is flexible such that it elastically deflects for passively opening up the air channel at a predetermined loading of the trailing edge section.

11. The rotor blade according to claim 1 , wherein the air channel is opened up passively.

12. A method comprising: modifying a lift of the rotor blade of the wind turbine, wherein the rotor blade is configured according to claim 1 , and at the predetermined loading of the trailing edge section, the air channel opens up, and the airflow flowing from the leading edge section to the trailing edge section is at least partly deflected by the open air channel, which results in a modification of the lift of the rotor blade.

Assignees

• Siemens Gamesa Renewable Energy As

Inventors

• Gonzalez Alejandro Gomez
• Laursen Jesper Monrad

Classifications

• F05B2240/31

  of changeable form or shape · CPC title

• F03D1/065

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

• F03D1/0641

  of the section profile of the blades, i.e. aerofoil profile · CPC title

• F03D1/0633 Primary

  of the blades · CPC title

• F03D1/0675

  of the blades · CPC title