FIELD: engines and pumps.
SUBSTANCE: invention can be used in automatic control systems of gas turbine engines (GTE). GTE control device includes fuel pump the outlet of which is connected to compressor mechanisation regulator and connected to fuel supply line to engine, in which there in series installed is metering device and distributing valve (DV); at that, metering device is connected to regulator of engine operating mode and to electronic alarm and control unit (ERD), and electromagnetic stop valve (SV) of engine is connected to fuel supply line to engine, sensor unit (SU) connected to regulators of engine operating mode, compressor mechanisation and ERD; in addition, there introduced is electromagnet (EM) and valve of minimum pressure (VMP), which are connected to regulator of engine operating modes; at that, inlet of electromagnet is connected to ERD.
EFFECT: higher operating reliability of GTE and aircraft flight safety.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF CONTROLLING FUEL FEED INTO GAS TURBINE ENGINE | 2010 |
|
RU2474712C2 |
| METHOD OF HELICOPTER POWER PLANT CONTROL | 2010 |
|
RU2482024C2 |
| DEVICE FOR GAS TURBINE ENGINE CONTROL | 2012 |
|
RU2497000C1 |
| METHOD OF MECHANIZATION CONTROL OF GAS TURBINE ENGINE COMPRESSOR | 2017 |
|
RU2639923C1 |
| GAS TURBINE ENGINE CONTROL DEVICE | 2009 |
|
RU2439349C2 |
| DEVICE FOR GAS-TURBINE ENGINE CONTROL | 2012 |
|
RU2516761C2 |
| GAS TURBINE ENGINE COMPRESSOR MECHANIZATION CONTROL DEVICE | 2016 |
|
RU2658709C2 |
| METHOD OF FUEL FLOW CONTROL AT START OF GAS TURBINE ENGINE | 2010 |
|
RU2435973C1 |
| METHOD OF CONTROLLING FUEL FEED TO GAS TURBINE ENGINE | 2011 |
|
RU2489592C1 |
| MONITORING METHOD OF GAS TURBINE ENGINE CONTROL SYSTEM | 2010 |
|
RU2468229C2 |
