FIELD: engines and pumps.
SUBSTANCE: fuel maximum flow rate limiter is added, its input being connected to air pressure gage outlet at gas turbine inlet while its pout connected to fuel metering unit. Note here that fuel pump is arranged in separate case and maximum tolerable distance from gas turbine drive box. Note also that electro-hydro-converter is arranged at minimum possible distance from said drive box.
EFFECT: higher engine reliability and aircraft flight safety.
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR GAS-TURBINE ENGINE CONTROL | 2012 |
|
RU2516761C2 |
| METHOD OF GAS TURBINE ENGINE | 2011 |
|
RU2493392C2 |
| GAS TURBINE ENGINE CONTROL DEVICE | 2012 |
|
RU2487259C1 |
| METHOD OF CONTROLLING FUEL FEED TO GAS TURBINE ENGINE | 2012 |
|
RU2497001C1 |
| METHOD OF CONTROLLING FUEL FEED TO GAS TURBINE ENGINE | 2011 |
|
RU2489592C1 |
| GAS TURBINE ENGINE CONTROL DEVICE | 2009 |
|
RU2439349C2 |
| METHOD OF CONTROLLING FUEL FEED INTO GAS TURBINE ENGINE | 2010 |
|
RU2474712C2 |
| GAS TURBINE ENGINE FUEL FEED AND ADJUSTMENT SYSTEM | 2009 |
|
RU2435971C2 |
| CONTROL OVER GAS TURBINE ENGINE COMPRESSOR ACTUATORS | 2012 |
|
RU2514463C1 |
| GAS TURBINE ENGINE CONTROL DEVICE | 2006 |
|
RU2334890C2 |
