FIELD: machine building.
SUBSTANCE: invention relates to the field of a gas turbine engine (GTE) automatic control, namely, to the afterburner combustion chamber with adaptive fuel supply system operation control methods. Invention differs from the known ones in that the temperature of the gas flow at the output of the afterburner combustion chamber is additionally measured and the position of the fuel manifold in the afterburner combustion chamber is controlled.
EFFECT: technical result of the invention is increase of efficiency of control of working process of the combustion chamber due to measurement of value of temperature of a gas flow at output of an afterburner combustion chamber and control of position of a fuel collector before the flame stabilizer.
1 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AFTERBURNER COMBUSTION CHAMBER CONTROL SYSTEM | 2017 |
|
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|
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|
RU2464437C1 |
