Sensor arrangement for measuring gas turbine combustor temperatures
US10935431B2 · kind B2 · utility
2Cited by
4References
18Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Sep 21, 2018 |
| Grant date | Mar 2, 2021 |
| Priority date | — |
| Expiry date | Jan 14, 2040 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R2900/00013
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
A sensor system for use in a gas turbine engine. The sensor system includes a reflective surface configured to reflect optical features corresponding to combustion in a combustion chamber that exit the combustion chamber via at least one opening therein. The sensor system further includes an optical sensor configured to receive the reflected optical features from the reflective surface.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.