FIELD: engines and pumps.
SUBSTANCE: system of automatic control (ACS) of gas-turbine engines (GTE) comprises serially connected unit and the first levelling device, which is connected to electronic controller, and also with logical unit, in its turn electronic controller is connected to actuating mechanism, and also with model of actuating mechanism, realised as device in board digital computer of aircraft, actuating mechanism is connected to gas-turbine engine and the first sensor, which, as the model of actuating mechanism, which is connected serially to GTE model, is connected to the second levelling device, gas-turbine engine is connected to the second sensor, in its turn the second sensor and GTE model are connected to the third levelling device, which together with the second levelling device is connected to logical unit, which is also connected to electric controller.
EFFECT: improved quality of functioning of system of automatic control of short-resource gas-turbine engine at all modes and in all conditions of its application in composition of unmanned aircraft.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS TURBINE ENGINE AUTOMATIC CONTROL SYSTEM | 2007 |
|
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| METHOD OF CONTROLLING GAS TURBINE ENGINE | 2009 |
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RU2409751C2 |
| GAS TURBINE ENGINE ACS | 2010 |
|
RU2446298C1 |
