Method and device for aiding the monitoring of a turbine engine of an aircraft
US9193476B2 · kind B2 · utility
2Cited by
4References
16Claims
0Family size
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Key dates
| Filing date | Nov 26, 2013 |
| Grant date | Nov 24, 2015 |
| Priority date | — |
| Expiry date | Jan 3, 2034 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG01D2207/10
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A method and device for aiding the monitoring of a turbine engine of an aircraft, which displays on one and the same indicator of a of a display indication elements illustrating as a percentage the engine start progression or the current sub-idle state of the turbine engine, a margin to a limit temperature of the turbine engine, a margin to a maximum temperature of the turbine engine and a margin to a possible failure of the start that is generated by a too low speed increase of the turbine engine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.