FIELD: engines and pumps.
SUBSTANCE: additionally for power output control air pressure and temperature upstream of engine inlet are measured and air pressure is controlled so that engine rotor rpm in interval from the starting fuel feed in combustion chamber to the moment of fuel ignition is kept constant proceeding from jump increase in temperature of gases downstream of the turbine.
EFFECT: higher reliability of starting, higher ACS operation quality.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS TURBINE ENGINE START-UP CONTROL METHOD | 2011 |
|
RU2480601C2 |
| GAS-TURBINE ENGINE FUEL SYSTEM | 2006 |
|
RU2317431C1 |
| METHOD TO CONTROL GAS TURBINE ENGINE FUEL SYSTEM | 2008 |
|
RU2379535C2 |
| METHOD TO CONTROL FUEL FLOW RATE IN STARTING GAS TURBINE ENGINE | 2008 |
|
RU2386836C2 |
| GAS TURBINE ENGINE CONTROL SYSTEM | 2006 |
|
RU2329386C2 |
| CONTROL METHOD OF GAS TURBINE ENGINE WITH AFTERBURNER COMBUSTION CHAMBER | 2018 |
|
RU2706518C1 |
| METHOD FOR STARTING THE COMBUSTION CHAMBER OF A GAS TURBINE ENGINE | 2022 |
|
RU2786964C1 |
| METHOD OF FUEL FLOW CONTROL AT START OF GAS TURBINE ENGINE | 2010 |
|
RU2435973C1 |
| METHOD CONTROLLING FUEL FEED IN GAS TURBINE ENGINE COMBUSTION CHAMBER | 2008 |
|
RU2439350C2 |
| METHOD OF CONTROLLING GAS TURBINE ENGINE | 2010 |
|
RU2472957C2 |
