Method and system for detecting exposure of composites to high-temperature
US-9372177-B2 · Jun 21, 2016 · US
US9671386B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9671386-B2 |
| Application number | US-201414267718-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 1, 2014 |
| Priority date | May 1, 2013 |
| Publication date | Jun 6, 2017 |
| Grant date | Jun 6, 2017 |
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Improved methods of detecting thermal exposure are provided herein. The provided methods utilize initially dormant luminescent probes incorporated into a matrix to form a composite. When exposed to heat over a period of time, the luminescent probes are “activated” through a molecular transformation initiated by thermal energy. The activated probes exhibit a luminescent profile based on the extent of thermal exposure, thereby providing an indicator of the thermal exposure experienced by the matrix. When the composite is used to produce a structural component of a vehicle (e.g., an aircraft), the methods provide a convenient, large-area indicator of thermal damage experienced by the structural component.
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The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows: 1. A method of monitoring thermal exposure of a composite, comprising: (a) providing a composite, comprising: (i) a matrix; (ii) a first probe, wherein the first probe is not luminescent until activated by heat to a temperature above 200° C., after which it becomes luminescent and has a first luminescence profile; and (iii) a second probe, wherein the second probe is not luminescent until activated by heat, after which it becomes luminescent and has a second luminescence profile that is different from the first luminescence profile; (b) exposing the composite to a time-temperature profile that includes a portion of time at a temperature above 200° C.; and (c) measuring an optical property of the composite. 2. The method of claim 1 , wherein the matrix is selected from the group consisting of a thermoset polymer, a thermoplastic polymer, and a sol-gel. 3. The method of claim 1 , wherein the optical property is stimulated emission of the first probe. 4. The method of claim 1 , wherein the first probe is fluorescent or phosphorescent. 5. The method of claim 1 , wherein the matrix is transparent at wavelengths within the first luminescence profile. 6. The method of claim 1 , wherein the first probe is incorporated within the matrix. 7. The method of claim 1 , wherein a coating on the matrix comprises the first probe. 8. The method of claim 1 , wherein the time-temperature profile comprises a rise in temperature from a first temperature to a second temperature between a first time and a second time. 9. The method of claim 8 , wherein the time-temperature profile comprises temperature variations. 10. The method of claim 8 , wherein the time-temperature profile comprises repeated temperature cycles. 11. The method of claim 1 , wherein the first probe and the second probe combine to be a time-temperature indicator of thermal damage. 12. The method of claim 1 , wherein the optical property is the combined stimulated emission of the first probe and the second probe. 13. The method of claim 1 , further comprising a step of analyzing the optical property to determine thermal exposure of the composite. 14. The method of claim 13 , wherein the step of analyzing the optical property comprises comparing the optical property to a calibration data set. 15. The method of claim 1 , wherein the matrix further comprises carbon fibers. 16. The method of claim 15 , wherein the matrix is a carbon-fiber reinforced plastic composite. 17. The method of claim 1 , wherein the composite is a structural component of a vehicle. 18. The method of claim 17 , wherein the composite is a structural component of an aircraft.
thermally excited · CPC title
non-biological material · CPC title
Resins; Plastics · CPC title
using thermoluminescent materials (G01K11/32 takes precedence) · CPC title
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