Sacrificial sensor for determining damage to a part

Patent metadata

Field	Value
Publication number	US-12287303-B2
Application number	US-202017596146-A
Country	US
Kind code	B2
Filing date	May 27, 2020
Priority date	Jun 6, 2019
Publication date	Apr 29, 2025
Grant date	Apr 29, 2025

Abstract

There is provided a sacrificial sensor configured to be coupled with a part and provide an indication of damage in the part, wherein an electrical property of the sacrificial sensor is configured to change as the sacrificial sensor is damaged to indicate damage to the part.

First claim

The invention claimed is:

1. A sensor system configured to be coupled with a part and provide an indication of damage in the part, the sensor system comprising a plurality of sacrificial sensors arranged across a surface of the part, such that the sacrificial sensors are spaced from one another on the surface, each of the plurality of sacrificial sensors comprising a separate and distinct plurality of electrically conductive, flexible fibers in a tissue structure, wherein an electrical property of a given sacrificial sensor of the plurality of sacrificial sensors changes as at least a portion of the given sacrificial sensor is physically broken to indicate damage to the part.

2. The sensor system according to claim 1 , wherein the electrical property comprises electrical resistance, wherein the electrical resistance increases as the given sacrificial sensor is damaged.

3. The sensor system according to claim 1 , wherein the electrical property comprises capacitance.

4. The sensor system according to claim 1 , wherein the plurality of sacrificial sensors is located within an adhesive coupled to the part.

5. The sensor system according to claim 1 , wherein the plurality of sacrificial sensors is configured to be integral within the part.

6. The sensor system according to claim 1 , wherein the given sacrificial sensor has an areal density of between approximately 5 gsm and approximately 30 gsm.

7. A system comprising:
a part to be inspected; and
the sensor system according to claim 1 , wherein one or more of the plurality of sacrificial sensors has a lower strain to failure value compared with a strain to failure value of the part.

8. The system according to claim 7 , wherein the one or more of the plurality of sacrificial sensors includes a plurality of sacrificial sensors arranged at various locations on the part to determine the location of any damage of the part.

9. The system according to claim 7 , wherein the part comprises a non-conductive composite laminated material.

10. The system according to claim 9 , wherein the one or more of the plurality of sacrificial sensors is located in a laminar layer of the composite laminated material.

11. The system according to claim 9 , wherein the one or more of the plurality of sacrificial sensors is located in a matrix of the composite laminated material.

12. The system according to claim 8 , wherein the one or more of the plurality of sacrificial sensors is located within an adhesive at a joint in the part.

13. A method of providing an indication of damage in a part, the method comprising:
providing a part with the sensor system according to claim 1 ;
providing a voltage potential to the given sacrificial sensor; and
determining a change in the electrical property of the given sacrificial sensor to indicate damage to the part.

14. A sensor system configured to be coupled with a part and provide an indication of damage in the part, the sensor system comprising a plurality of sacrificial sensors arranged across a surface of the part, such that the sacrificial sensors are spaced from one another on the surface, each of the plurality of sacrificial sensors comprising a separate and distinct plurality of electrically conductive, flexible fibers in a tissue structure, wherein an electrical property of a given sacrificial sensor of the plurality of sacrificial sensors changes as the given sacrificial sensor is physically broken to indicate damage to the part, wherein the sensor system is one of (1) located within an adhesive coupled to the part or (2) integral within the part.

15. The sensor system according to claim 14 , wherein the electrical property comprises electrical resistance, capacitance, or both.

16. A system comprising:
a part comprising a non-conductive composite laminated material; and
a sacrificial sensor arranged on a surface of the part, the sacrificial sensor comprising a plurality of electrically conductive, flexible fibers in a tissue structure and is configured to provide an indication of damage in the part, wherein an electrical property of the sacrificial sensor changes as the sacrificial sensor is physically broken to indicate damage to the part.

17. The system according to claim 16 , wherein the sacrificial sensor is located in one of (1) a laminar layer of the composite laminated material, (2) a matrix of the composite laminated material, or (3) an adhesive at a joint in the part.

18. The sensor system according to claim 1 , wherein the plurality of sacrificial sensors are rectangular strips spaced adjacent to one another across the surface of the part.

19. The sensor system according to claim 14 , wherein the plurality of sacrificial sensors are rectangular strips spaced adjacent to one another across the surface of the part.

20. The system according to claim 16 , wherein the sacrificial sensor is a rectangular strip on the surface of the part.

Assignees

• Bae Systems Plc

Inventors

• Barton Janice Marie
• Olafsson Geir

Classifications

• G01N27/24

  Investigating the presence of flaws · CPC title

• G01M5/0016

  of aircraft wings or blades · CPC title

• G01B7/18

  using change in resistance · CPC title

• G01B7/16

  for measuring the deformation in a solid, e.g. by resistance strain gauge · CPC title

• G01B7/001

  Constructional details of gauge heads (G01B7/012 takes precedence) · CPC title