FIELD: engines and pumps.
SUBSTANCE: additionally, in case signal "Fire in nacelle" is generated at takeoff by aircraft anti-fire system turbo compressor current rpm is fixed to be used as the blower preset rpm magnitude for preset time interval. Said interval elapsed, fuel feed is terminated to shut down the engine.
EFFECT: improved control over fuel feed, higher reliability of engine and aircraft.
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF CONTROLLING FUEL FEED TO GAS TURBINE ENGINE | 2011 |
|
RU2489592C1 |
| DEVICE FOR GAS-TURBINE ENGINE CONTROL | 2012 |
|
RU2516761C2 |
| METHOD OF CONTROLLING FUEL FEED INTO GAS TURBINE ENGINE | 2010 |
|
RU2474712C2 |
| METHOD OF GAS TURBINE ENGINE | 2011 |
|
RU2493392C2 |
| CONTROL OVER GAS TURBINE ENGINE COMPRESSOR ACTUATORS | 2012 |
|
RU2514463C1 |
| DEVICE FOR GAS TURBINE ENGINE CONTROL | 2012 |
|
RU2497000C1 |
| METHOD OF GAS TURBINE ENGINE PROTECTION | 2010 |
|
RU2474713C2 |
| METHOD OF GAS TURBINE ENGINE PROTECTION | 2011 |
|
RU2472974C2 |
| TURBOPROP POWER PLANT FUEL FLOW RATE CONTROL METHOD | 2006 |
|
RU2334889C2 |
| MONITORING METHOD OF GAS TURBINE ENGINE CONTROL SYSTEM | 2010 |
|
RU2468229C2 |
