Method of monitoring gas turbine engine operation
US8594903B2 · kind B2 · utility
5Cited by
52References
7Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 29, 2008 |
| Grant date | Nov 26, 2013 |
| Priority date | — |
| Expiry date | Jun 3, 2029 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2270/44
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
A system, method and apparatus for monitoring the performance of a gas turbine engine. A counter value indicative of the comparison between the engine condition and the threshold condition is adjusted. The aircraft operator is warned of an impending maintenance condition based on the counter value and determines an appropriate course of action.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.