Data acquisition devices, systems and method for analyzing passive strain indicators and monitoring turbine component strain

• US 10,132,615 B2
• Filed: 01/16/2018
• Issued: 11/20/2018
• Est. Priority Date: 12/20/2016
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (GE Vernova, Inc.)
• Original Assignee: General Electric Company
• Inventors: Burnside, Jason Lee, Hovis, Gregory Lee, Ranson, William Farris
• Primary Examiner(s): Punnoose, Roy M
• Application Number:
  US15/872,034
• Publication Number:
  US 20180172434A1
• Time in Patent Office: 308 Days
• Field of Search: 356 32
• CPC Class Codes: G01B 11/165 by means of a grating deformed by the object
• CPC Class Codes: G01M 15/14 Testing gas-turbine engines or jet-propulsion engines
• CPC Class Codes: G01M 5/0016 of aircraft wings or blades
• CPC Class Codes: G01M 5/0041 by determining deflection or stress
• CPC Class Codes: G01M 5/0091 by using electromagnetic excitation or detection
• CPC Class Codes: G06T 2207/30164 Workpiece; Machine component
• CPC Class Codes: G06T 7/001 using an image reference approach

Abstract

Data acquisition devices for analyzing reference objects and systems for monitoring turbine component deformation are provided. A data acquisition device has a longitudinal axis and includes a lens assembly and an image capture device in communication with the lens assembly for receiving and processing light from the lens assembly to generate images. The data acquisition device further includes a light source and a light tube coupled at a rear end to the light source. The light tube extends along the longitudinal axis between a front end and the rear end, and is operable to transport light from the light source therethrough and emit the light from the front end. The data acquisition device further includes an actuator operable to activate the image capture device and the light source.

Claims

1. A system for monitoring turbine component deformation, the turbine component having an exterior surface, the system comprising:

a passive strain indicator configurable on the exterior surface of the turbine component; and

a data acquisition device for analyzing the passive strain indicator, the data acquisition device comprising;

a lens assembly;

an image capture device in communication with the lens assembly for receiving and processing light from the lens assembly to generate images;

a light source;

a light tube coupled at a rear end to the light source and extending along a longitudinal axis between a front end and the rear end, the light tube operable to transport light from the light source therethrough and emit the light from the front end;

an actuator operable to activate the image capture device and the light source;

a shell, the shell surrounding the lens assembly, the image capture device, the light source, and the light tube; and

a plurality of spacers disposed proximate the front end of the light tube, each of the plurality of spacers extending from the shell and sized to space the front end of the light tube from the exterior surface of the turbine component when the data acquisition device is in an operative position in contact with the exterior surface of the turbine component.

2. The system of claim 1, wherein the data acquisition device further comprises an outer shroud surrounding at least a portion of an outer surface of the light tube.

3. The system of claim 1, wherein an outer surface of the light tube comprises a chamfered portion, the chamfered portion tapering towards an inner surface of the light tube along the longitudinal axis.

4. The system of claim 3, wherein the chamfered portion includes the front end.

5. The system of claim 1, wherein light is emitted from the front end of the light tube at an angle of incidence of between approximately 20 degrees and approximately 50 degrees.

6. The system of claim 1, wherein each of the plurality of spacers is sized to space the front end of the light tube from the exterior surface of the turbine component by a distance along the longitudinal axis of between approximately 0.25 inches and approximately 0.75 inches when the data acquisition device is in an operative position in contact with the exterior surface of the turbine component.

7. The system of claim 1, wherein the data acquisition device further comprises a processor, the processor configured for:

locating a passive strain indicator portion relative to a background portion within an image of the passive strain indicator by performing a first analysis of the image;

identifying passive strain indicator indicia of the passive strain indicator portion by performing a second analysis of the image; and

conducting a quality analysis of the passive strain indicator portion by performing a third analysis of the passive strain indicator portion of the image, the third analysis utilizing a higher bit-depth than the first analysis.