IP Library › Granted Patent US 12,287,303
Granted Patent B2
US 12,287,303 · App. 17/596,146 · Granted Apr 29, 2025

Sacrificial sensor for determining damage to a part

Inventors: Janice Marie Barton (Southhampton, GB); Geir Olafsson (Southampton, GB)
Assignee: BAE SYSTEMS PLC
G01N27/20G01N27/24
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,287,303
App. No.
17/596,146
Granted
Apr 29, 2025
Kind
B2
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.

Claims (27)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 3, 2021
From: BARTON, JANICE MARIE; OLAFSSON, GEIR
To: BAE SYSTEMS PLC
Reel/Frame 058283/0805 →
Priority Claims (1)
GB 1908053 · Jun 6, 2019 · national
Continuity (1)
Related Publication 20220229007A1 · Jul 21, 2022
References Cited (22)
US 5245293A · Runner · 1993 [cited by applicant]
US 9329021B1 · DeLuca et al. · 2016 [cited by applicant]
US 20070166831A1 · Watkins, Jr. et al. · 2007 [cited by applicant]
US 20090249885A1 · Shkel et al. · 2009 [cited by applicant]
US 20110089958A1 · Malecki · 2011 [cited by examiner]
US 20120188078A1 · Soles et al. · 2012 [cited by applicant]
US 20180306568A1 · Holman · 2018 [cited by examiner]
US 20200191549A1 · Aitchison · 2020 [cited by examiner]
CN 106643461A · 2017 [cited by applicant]
CN 107328827A · 2017 [cited by applicant]
CN 110230142A · 2019 [cited by applicant]
EP 2950085A1 · 2015 [cited by applicant]
JP 2001153603A · 2001 [cited by applicant]
KR 20140038149A · 2014 [cited by examiner]
KR 20180102898A · 2018 [cited by examiner]
WO WO2016175321A1 · 2016 [cited by examiner]
WO 2017157605A1 · 2017 [cited by applicant]
WO 2020245564A1 · 2020 [cited by applicant]
International Search Report and Written Opinion received for PCT Application No. PCT/GB2020/051272. Mail date: Aug. 11, 2020. 17 pages. [cited by applicant]
GB Search Report under Section 17(5) received for GB Application No. 1908053.0, dated Nov. 29, 2019. 4 pages. [cited by applicant]
Atalay, Ozgur and Kennon, William Richard, “Knitted Strain Sensors: Impact of Design Parameters on Sensing Properties,” Sensors, vol. 14, No. 3, Mar. 7, 2014. pp. 4712-4730. [cited by applicant]
International Preliminary Report on Patentbility received for PCT Application No. PCT/GB2020/051272. Mail date: Dec. 16, 2021. 10 pages. [cited by applicant]