FIELD: engines. SUBSTANCE: first and second flow rate regulators 6 and 7 are connected to setter 8 and engine speed of rotation transducer 9 respectively. When setter 8 forms command "stop" "stop" mode actuator 11 is brought into action. The fuel from cavity 5 is drained to manifold 2 through actuator 11. The speed of displacement of servomotor 4 increases. The fuel feed to the engine abruptly decreases. EFFECT: improved accuracy. 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CONTROLLER OF ROTATION SPEED FOR GAS-TURBINE ENGINE | 1990 |
|
RU2009351C1 |
| GAS-TURBINE ENGINE SPEED CONTROLLER | 0 |
|
SU1825879A1 |
| GAS-TURBINE ENGINE SPEED CONTROLLER | 0 |
|
SU1825881A1 |
| SPEED GOVERNOR OF GAS TURBINE ENGINE | 0 |
|
SU1795137A1 |
| GAS-TURBINE ENGINE OPERATION CONTROLLER | 0 |
|
SU1825880A1 |
| GAS TURBINE ENGINE (GTE) FUEL SUPPLY AND CONTROL TWO-CHANNEL SYSTEM | 2018 |
|
RU2680475C1 |
| GAS TURBINE ENGINE FUEL FEED AND ADJUSTMENT TWO-CHANNEL SYSTEM | 2014 |
|
RU2553915C1 |
| TWO-CHANNEL GAS TURBINE ENGINE FUEL SUPPLY AND REGULATION SYSTEM | 2019 |
|
RU2700989C1 |
| GAS-TURBINE ENGINE GOVERNOR | 0 |
|
SU1825878A1 |
| TWO-CHANNEL GAS TURBINE FUEL FEED AND ADJUSTMENT SYSTEM | 2012 |
|
RU2504677C1 |
