Rotor blade inspection system

Patent metadata

Field	Value
Publication number	US-12359672-B2
Application number	US-202318136137-A
Country	US
Kind code	B2
Filing date	Apr 18, 2023
Priority date	Apr 18, 2023
Publication date	Jul 15, 2025
Grant date	Jul 15, 2025

Abstract

An inspection system for rotating fan rotor blades is provided that includes a plurality of cameras and light sources and a system controller. The cameras are controllable to capture an image of a leading edge of a fan rotor blade and produce signals representative of the captured image. Each respective camera is mounted with an inlet guide vane disposed forward of the fan rotor blade stage. The light sources are each associated with a respective camera. The system controller is in communication with the cameras, the light sources, and a non-transitory memory storing instructions. The instructions when executed cause the system controller to: control the light sources to selectively illuminate the fan rotor blades, and control the cameras to image respective fan rotor blades and produce signals representative thereof, and provide inspection information representative of the leading edge of respective fan rotor blades.

First claim

The invention claimed is:

1. An inspection system for a fan rotor blade in a fan rotor blade stage of a gas turbine engine, the fan rotor blade having a leading edge, the system comprising:
a plurality of cameras, each camera of the plurality of cameras controllable to capture an image of at least a portion of the leading edge of the fan rotor blade and produce signals representative of the captured image, wherein each camera is mounted with an inlet guide vane disposed forward of the fan rotor blade stage;
a plurality of light sources, each light source of the plurality of light sources associated with a respective camera of the plurality of cameras; and
a system controller in communication with the plurality of cameras, the plurality of light sources, and a non-transitory memory storing instructions, which instructions when executed cause the system controller to:
control each of the plurality of light sources to selectively illuminate at least portions of the fan rotor blade;
control each of the plurality of cameras to capture images of said at least a portion of the leading edge of the fan rotor blade and produce signals representative of the captured images; and
provide inspection information representative of said at least a portion of the leading edge of the fan rotor blade using the signals representative of the captured images,

wherein said each camera mounted with an inlet guide vane is mounted in said inlet guide vane.

2. The inspection system of claim 1 , wherein each respective said light source is mounted with a respective said camera.

3. The inspection system of claim 1 , wherein multiple cameras among the plurality of cameras are mounted in a single inlet guide vane.

4. The inspection system of claim 3 , wherein all cameras of the plurality of cameras are mounted in said single inlet guide vane.

5. The inspection system of claim 4 , wherein at least one camera among the plurality of cameras is mounted in a housing, and the housing is mounted in said single inlet guide vane.

6. The inspection system of claim 5 , wherein the housing has an interior compartment and wherein the at least one camera is fixed in the interior compartment of the housing.

7. The inspection system of claim 5 , wherein the housing has an interior compartment and wherein the at least one camera is mounted to be selectively translatable in the interior compartment of the housing.

8. The inspection system of claim 1 , wherein a first camera among the plurality of cameras is mounted in a first inlet guide vane, and a second camera among the plurality of cameras is mounted in a second inlet guide vane.

9. The inspection system of claim 8 , wherein the first said camera is mounted in the first said inlet guide vane at a first radial position, and the second said camera is mounted in the second said inlet guide vane at a second radial position, wherein the first radial position is different from the second radial position.

10. The inspection system of claim 8 , wherein:
the first camera is mounted in a housing and the housing is mounted in the first inlet guide vane, and/or
the second camera is mounted in a housing, and the housing is mounted in the second inlet guide vane.

11. A fan inlet guide vane stage for use with a fan rotor stage having a plurality of fan rotor blades, each fan rotor blade having a respective leading edge, the fan inlet guide vane stage comprising:
a plurality of inlet guide vanes, each inlet guide vane having a respective trailing edge;
a plurality of cameras, each camera configured for imaging a respective leading edge of a fan rotor blade of the plurality of fan rotor blades; and
a plurality of light sources;
wherein each respective camera and each respective light source are mounted with an inlet guide vane of the plurality of inlet guide vanes, and
wherein each respective camera mounted with an inlet guide vane is mounted in said inlet guide vane.

12. The fan inlet guide vane stage of claim 11 , wherein each respective camera mounted with an inlet guide vane is mounted in said inlet guide vane proximate the respective trailing edge of said inlet guide vane.

13. The fan inlet guide vane stage of claim 11 , wherein all cameras of the plurality of cameras are mounted in a single inlet guide vane.

14. The fan inlet guide vane stage of claim 13 , wherein at least one camera among the plurality of cameras is mounted in a housing, and the housing is mounted in said single inlet guide vane.

15. The fan inlet guide vane stage of claim 14 , wherein said at least one camera is mounted in an interior compartment disposed in said single inlet guide vane.

16. The fan inlet guide vane stage of claim 11 , wherein a first camera among the plurality of cameras is mounted in a first inlet guide vane and a second camera among the plurality of cameras is mounted in a second inlet guide vane.

17. The fan inlet guide vane stage of claim 16 , wherein the first said camera is mounted in the first said inlet guide vane at a first radial position, and the second said camera is mounted in the second said inlet guide vane at a second radial position, wherein the first radial position is different from the second radial position.

Assignees

• Raytheon Tech Corp
• Rtx Corp

Inventors

• Goyette Scott
• Shaw Janet
• Hagen Gregory S
• Attridge Paul
• Chaudhry Zaffir A
• Lincoln David L
• King Jeffrey P

Classifications

• F05D2270/8041

  Cameras · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title

• F04D29/542

  Bladed diffusers (fixing blades to stators F01D9/042) · CPC title

• F04D27/001 Primary

  Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring · CPC title