Method of monitoring gas turbine engine operation
US7487029B2 · kind B2 · utility
14Cited by
29References
47Claims
0Family size
Inventors
Key dates
| Filing date | May 21, 2004 |
| Grant date | Feb 3, 2009 |
| Priority date | — |
| Expiry date | Feb 15, 2026 |
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.