Wind turbine blade flow regulation

Patent metadata

Field	Value
Publication number	US-2022018329-A1
Application number	US-201917311009-A
Country	US
Kind code	A1
Filing date	Oct 31, 2019
Priority date	Dec 13, 2018
Publication date	Jan 20, 2022
Grant date	—

Abstract

A wind turbine including:at least a rotor blade including an aerodynamic device for influencing the airflow flowing from the leading edge section of the rotor blade to the trailing edge section of the rotor blade, wherein the aerodynamic device is mounted at a surface of the rotor blade,an actuator of the aerodynamic device for actuating the aerodynamic device at least between a first protruded configuration and a second retracted configuration,a pressure supply system for operating the actuator by means of a pressurized fluid,an acoustic receiver for measuring an acoustic signal in the pressure supply system, anda diagnostic unit connected to the acoustic receiver and configured for deriving an operative status of the aerodynamic device based on the acoustic signal, is provided.

First claim

What is claimed:

1 . A wind turbine comprising:
a rotor blade comprising an aerodynamic device for influencing an airflow flowing from a leading edge section of the rotor blade to a trailing edge section of the rotor blade, wherein the aerodynamic device is mounted at a surface of the rotor blade; an actuator of the aerodynamic device for actuating the aerodynamic device at least between a first protruded configuration and a second retracted configuration; a pressure supply system for operating the actuator by means of a pressurized fluid; an acoustic receiver for measuring an acoustic signal in the pressure supply system; and a diagnostic unit connected to the acoustic receiver and configured for deriving an operative status of the aerodynamic device based on the acoustic signal.

2 . The wind turbine according to claim 1 , wherein the wind turbine comprises an acoustic transmitter for transmitting the acoustic signal in the pressure supply system, the acoustic transmitter being connected to the diagnostic unit.

3 . The wind turbine according to claim 1 , wherein the actuator is operated between an inflated configuration corresponding to the first protruded configuration of the aerodynamic device and a deflated configuration corresponding to the second retracted configuration of the aerodynamic device, the actuator in the inflated configuration providing a first path for the acoustic signal in the pressure supply system, the actuator in the deflated configuration providing a second path for the acoustic signal in the pressure supply system, the second path being different from the first path.

4 . A wind turbine according to claim 1 , wherein the pressure supply system comprises at least a first pressure line for providing the pressurized fluid to the actuator of the aerodynamic device, the acoustic transmitter being provided at the first pressure line.

5 . A wind turbine according to claim 4 , wherein the pressure supply system comprises at least a second pressure return line for receiving the pressurized fluid from the actuator of the aerodynamic device, the acoustic receiver being provided at the second pressure return line.

6 . The wind turbine according to claim 1 , wherein the first pressure line extends between a first end where the acoustic receiver and/or the acoustic transmitter are provided and a second end connected to the actuator of the aerodynamic device, a sound absorption device being provided at the first end for acoustically isolating the first pressure line from acoustical noise generated in the pressure supply system.

7 . A wind turbine according to claim 1 , wherein the actuator is an inflatable hose.

8 . A wind turbine according to claim 1 , wherein the acoustic receiver is a microphone.

9 . A wind turbine according to claim 1 , wherein the acoustic transmitter is a loudspeaker.

10 . A rotor blade for a wind turbine comprising:
an aerodynamic device for influencing an airflow flowing from a leading edge section of the rotor blade to a trailing edge section of the rotor blade, wherein the aerodynamic device is mounted at a surface of the rotor blade; an actuator of the aerodynamic device for actuating the aerodynamic device at least between a first protruded configuration and a second retracted configuration; a pressure supply system for operating the actuator by means of a pressurized fluid; an acoustic receiver for measuring an acoustic signal in the pressure supply system; and a diagnostic unit connected to the acoustic receiver and configured for deriving an operative status of the aerodynamic device based on the acoustic signal.

11 . A method for detecting an operative status of an aerodynamic device for influencing an airflow flowing from a leading edge of a rotor blade for a wind turbine to a trailing edge of the rotor blade, the aerodynamic device being movable by an actuator between a first protruded configuration and a second retracted configuration by means of a pressurized fluid, the method comprising:
measuring an acoustic signal in the pressure supply system; and deriving the operative status of the aerodynamic device based on the acoustic signal.

12 . The method according to claim 11 , wherein the acoustic signal is compared with a desired acoustic signal, the operative status of the aerodynamic device being derived based on the comparison between the measured acoustic signal and the desired acoustic signal.

13 . The method according to claim 11 , the operative status of the aerodynamic device being derived based on a time between the emission of the acoustic signal and the reception of the acoustic signal.

14 . The method according to claim 11 , further comprising:
calculating a frequency spectrum of the acoustic signal; and deriving the operative status of the aerodynamic device based on the frequency spectrum.

Assignees

• Siemens Gamesa Renewable Energy As

Inventors

• Egedal Per
• Enevoldsen Peder Bay
• Fiedel Moritz
• Gonzalez Alejandro Gomez
• Hoegh Gustav
• Kristensen Mikkel Aggersbjerg

Classifications

• F05B2270/81

  Microphones · CPC title

• F05B2270/806

  Sonars · CPC title

• F05B2270/333

  Noise or sound levels · CPC title

• F05B2240/306

  Surface measures · CPC title

• F03D7/022 Primary

  Adjusting aerodynamic properties of the blades · CPC title