Granted Patent B2

US 12,372,063 · App. 16/981,372 · Granted Jul 29, 2025

Inventors: Donato Girolamo (Voorhout, NL); Esben Orlowitz (Grindsted, DK); Nevena Stevanovic (Vejle, DK)

Assignee: SIEMENS GAMESA RENEWABLE ENERGY A/S

F03D17/00H04N23/54F05B2260/80F05B2270/8041

Abstract

Claims (31)

1. A rotor blade for a wind turbine, comprising:

a plurality of cameras mounted to an inner surface of the rotor blade, wherein the plurality of cameras are arranged inside the rotor blade;

wherein the plurality of cameras includes a first camera and a second camera, wherein the first camera is configured to acquire a first image of a first portion of the inner surface of the rotor blade, wherein the second camera is configured to capture a second image of a second portion of the inner surface of the rotor blade;

at least one light source mounted inside the rotor blade, wherein the at least one light source is configured to generate illumination light and is arranged to illuminate the first portion of the inner surface of the rotor blade and/or the second portion of the inner surface of the rotor blade;

at least one frame, wherein the first camera and the at least one light source are mounted on the at least one frame that is mounted on the inner surface of the rotor blade;

wherein the at least one frame has a mounting surface fit to a shape of a mounting portion of the inner surface;

wherein the mounting surface of the at least one frame is fit complementary to the shape of the mounting portion of the inner surface;

wherein the mounting portion of the inner surface is a back surface of an airfoil portion of the rotor blade.

2. A rotor blade monitoring system, comprising:

the rotor blade according to claim 1 ; and

an analysis module comprising image processing capability to process the first image and/or the second image to recognize features indicating damage of the inner surface of the rotor blade.

3. A wind turbine comprising:

a rotation shaft; and

the rotor blade or the rotor blade monitoring system according to claim 2 ,

wherein the rotor blade is mounted at the rotation shaft.

4. The rotor blade according to claim 1 , wherein the first camera, the second camera, and/or the at least one light source is mounted at the mounting portion of the inner surface of the rotor blade using an adhesive.

5. The rotor blade according to claim 1 , wherein the at least one light source is a plurality of light sources mounted inside the rotor blade and arranged to illuminate the first portion of the inner surface of the rotor blade and the second portion of the inner surface of the rotor blade.

6. The rotor blade according to claim 1 , wherein at least one image acquisition unit is formed by an assembly of the first camera, the second camera, and the at least one light source all mounted on at least one mounting frame inside the rotor blade, wherein the at least one image acquisition unit is a plurality of image acquisition units, wherein the plurality of image acquisition units are arranged in sets facing each other.

7. The rotor blade according to claim 1 , wherein the first camera and the second camera are mounted on at least one image acquisition unit, wherein the viewing direction of the first camera and the second camera differ are oriented to have viewing directions differing by at least 20°, by between 25° and 70°, by between 35° and 40°, and/or mounted close to each other.

8. The rotor blade according to claim 1 , wherein the first portion of the inner surface of the rotor blade and the second portion of the inner surface of the rotor blade cover a longitudinal extent of the rotor blade.

9. The rotor blade according to claim 1 , wherein at least one of the first camera and the second camera is sensitive to at least a portion of visual light and/or to at least a portion of infrared light and/or to at least a portion of ultraviolet light.

10. The rotor blade according to claim 1 , further comprising:

a wireless or wire based communication interface for communicating control signals and/or image data between the first camera, the second camera, and/or the at least one light source and a control module outside the rotor blade.

11. The rotor blade according to claim 1 , wherein a viewing direction of the first camera or the second camera is perpendicular to a longitudinal axis of the rotor blade.

12. The rotor blade according to claim 1 , wherein the first camera and the first portion are located at a same position along a longitudinal axis of the rotor blade, inside the rotor blade, and the second camera and the second portion are located at a same position along the longitudinal axis of the rotor blade, inside the rotor blade.

13. The rotor blade according to claim 1 , wherein all viewing directions of the first camera and the second camera intersect with a longitudinal axis of the rotor blade.

14. The rotor blade according to claim 1 , wherein the first camera is mounted over and faces the first portion and the second camera is mounted over and faces the second portion.

15. A method of monitoring a structural state of a rotor blade of a wind turbine, the method comprising:

providing a first camera mounted to an inner surface of the rotor blade and a second camera mounted to the inner surface of the rotor blade, wherein the first camera and the second camera are arranged inside the rotor blade, at least one light source mounted inside the rotor blade, wherein the at least one light source is configured to generate illumination light and is arranged to illuminate the first portion of the inner surface of the rotor blade and/or the second portion of the inner surface of the rotor blade, and at least one frame, wherein the first camera and the at least one light source are mounted on the at least one frame that is mounted on the inner surface of the rotor blade, wherein the at least one frame has a mounting surface fit to a shape of a mounting portion of the inner surface, wherein the mounting surface of the at least one frame is fit complementary to the shape of the mounting portion of the inner surface, wherein the mounting portion of the inner surface is a back surface of an airfoil portion of the rotor blade;

acquiring a first image of a first portion of the inner surface of the rotor blade and a second image of a second portion of the inner surface of the rotor blade; and

analysing the first image and/or the second image to determine a structural state of the rotor blade.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (58)