Sensor assembly for gas turbine engines
US11050011B2 · kind B2 · utility
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2References
20Claims
0Family size
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Key dates
| Filing date | Dec 18, 2017 |
| Grant date | Jun 29, 2021 |
| Priority date | — |
| Expiry date | Mar 1, 2040 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
A sensor assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a substrate layer formed on a localized surface of a rotatable gas turbine engine component, and at least one pair of transducers deposited on the substrate layer.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.