Passive strain indicator

• US 10,345,179 B2
• Filed: 02/14/2017
• Issued: 07/09/2019
• Est. Priority Date: 02/14/2017
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (General Electric Company)
• Original Assignee: General Electric Company
• Inventors: Hovis, Gregory Lee, Ranson, William F.
• Primary Examiner(s): Williams, Jamel E
• Application Number:
  US15/432,148
• Publication Number:
  US 20180231428A1
• Time in Patent Office: 875 Days
• CPC Class Codes: F01D 17/04 responsive to load
• CPC Class Codes: F05D 2260/80 Diagnostics
• CPC Class Codes: G01B 11/16 for measuring the deformation in a solid, e.g. optical strain gauge
• CPC Class Codes: G01B 5/30 for measuring the deformation in a solid, e.g. mechanical strain gauge
• CPC Class Codes: G01L 19/08 Means for indicating or recording, e.g. for remote indication
• CPC Class Codes: G01M 5/0016 of aircraft wings or blades

Abstract

A method of making a component with a passive strain indicator includes forming the component including an outer surface thereof. The passive strain indicator includes a shim with a plurality of fiducial markers. The method also includes forming the plurality of fiducial markers on the shim by deforming selected locations on the shim. The method further includes attaching a portion of the shim to the outer surface of the component. Forming the component and forming the passive strain indicator are performed separately prior to attaching the shim to the outer surface of the component. A system for monitoring strain includes a component and a passive strain indicator. A portion of the passive strain indicator is integrally joined with the outer surface of the component. The passive strain indicator includes a shim and a plurality of fiducial markers. Each fiducial marker is a discrete three-dimensional feature on the shim.

Claims

1. A method of making a component with a passive strain indicator, the method comprising:

forming the component, the component comprising an outer surface;

forming a shim into the passive strain indicator, the passive strain indicator comprising the shim and a plurality of fiducial markers on the shim, the plurality of fiducial markers formed on the shim by deforming selected locations on the shim; and

attaching at least a portion of the shim to the outer surface of the component;

wherein forming the component and forming the passive strain indicator are performed separately prior to attaching at least a portion of the shim to the outer surface of the component, and, wherein the plurality of fiducial markers are arranged in a predetermined pattern; and

,

wherein the predetermined pattern comprises an analysis region, a locator region, and a serial region, and wherein at least one of the plurality of fiducial markers is formed in each of the analysis region, the locator region, and the serial region.

2. The method of claim 1, wherein the predetermined pattern includes binary-encoded data.

3. The method of claim 1, wherein deforming selected locations on the shim comprises dot peening.

4. The method of claim 1, wherein deforming selected locations on the shim comprises forming indentations in selected locations on a front surface of the shim.

5. The method of claim 4, wherein the front surface of the shim comprises a reference portion and a peripheral welding region, and wherein deforming selected locations on the shim comprises deforming selected locations within the reference portion.

6. The method of claim 5, wherein, the peripheral welding region is distinct from the reference portion, no fiducial markers are formed on the peripheral welding region, and attaching at least a portion of the shim to the outer surface of the component comprises spot welding only the peripheral welding region of the shim to the outer surface of the component.

7. The method of claim 6, wherein the shim defines a length and a width, the product of the length and the width defines an area of the front surface, and the reference portion occupies between about forty percent of the area of the front surface and about seventy percent of the area of the front surface.

8. The method of claim 7, wherein the peripheral welding region occupies between about thirty percent of the area of the front surface and about sixty percent of the area of the front surface.

9. The method of claim 1, wherein the shim defines a length and a width, the length of the shim is between about two tenths of an inch and about one and a half inches and the width of the shim is between about one tenth of an inch and about three quarters of an inch.

10. A system for monitoring strain, comprising:

a component comprising an outer surface; and

a passive strain indicator formed on a shim, at least a portion of the passive strain indicator integrally joined with the outer surface of the component, the passive strain indicator comprising the shim and a plurality of fiducial markers, each fiducial marker of the plurality of fiducial markers comprising a discrete three-dimensional feature formed on the shim, and wherein the plurality of fiducial markers are arranged in a predetermined pattern, wherein the predetermined pattern comprises an analysis region, a locator region, and a serial region, and wherein at least one of the plurality of fiducial markers is positioned in each of the analysis region, the locator region, and the serial region.

11. The system of claim 10, wherein the predetermined pattern includes binary-encoded data.

12. The system of claim 10, wherein each fiducial marker comprises an indentation in a front surface of the shim.

13. The system of claim 10, wherein the shim comprises:

a front surface, the plurality of fiducial markers formed in a reference portion of the front surface of the shim;

a peripheral attachment region on the front surface, the peripheral attachment region distinct from the reference portion and integrally joined to the outer surface of the component; and

wherein no fiducial markers are formed on the peripheral attachment region.

14. The system of claim 13, wherein the shim defines a length and a width, the product of the length and the width defines an area of the front surface, and the reference portion occupies between about forty percent and about seventy percent of the area of the front surface.

15. The system of claim 14, wherein the peripheral attachment region occupies between about thirty percent of the area of the front surface and about sixty percent of the area of the front surface.

16. The system of claim 10, wherein the shim defines a length and a width, the length of the shim is between about two tenths of an inch and about one and a half inches and the width of the shim is between about one tenth of an inch and about three quarters of an inch.

17. A method of making a passive strain indicator on a component, the method comprising:

forming a shim into the passive strain indicator, the passive strain indicator comprising the shim and a plurality of fiducial markers on the shim, the plurality of fiducial markers formed on the shim by deforming selected locations on the shim; and

attaching at least a portion of the shim to an outer surface of the component;

wherein forming the passive strain indicator is performed separately prior to attaching at least a portion of the shim to the outer surface of the component, and wherein the plurality of fiducial markers are arranged in a predetermined pattern, wherein the predetermined pattern comprises an analysis region, a locator region, and a serial region, and wherein at least one of the plurality of fiducial markers is positioned in each of the analysis region, the locator region, and the serial region.

18. The method of claim 17, wherein the predetermined pattern includes binary-encoded data.

19. The method of claim 17, wherein deforming selected locations on the shim comprises dot peening.

20. The method of claim 17, wherein deforming selected locations on the shim comprises forming indentations in selected locations on a front surface of the shim.

21. The method of claim 20, wherein the front surface of the shim comprises a reference portion and a peripheral welding region, and wherein deforming selected locations on the shim comprises deforming selected locations within the reference portion.

22. The method of claim 21, wherein the peripheral welding region is distinct from the reference portion, no fiducial markers are formed on the peripheral welding region, and attaching at least a portion of the shim to the outer surface of the component comprises spot welding only the peripheral welding region of the shim to the outer surface of the component.

23. The method of claim 22, wherein the shim defines a length and a width, the product of the length and the width defines an area of the front surface, and the reference portion occupies between about forty percent of the area of the front surface and about seventy percent of the area of the front surface.

24. The method of claim 23, wherein the peripheral welding region occupies between about thirty percent of the area of the front surface and about sixty percent of the area of the front surface.

25. The method of claim 17, wherein the shim defines a length and a width, the length of the shim is between about two tenths of an inch and about one and a half inches and the width of the shim is between about one tenth of an inch and about three quarters of an inch.