FIELD: physics.
SUBSTANCE: invention relates to the field of gas turbine engine (GTE) automatic control, and namely to the afterburner combustion mode operation modes control methods. Technical result of the invention is increase of efficiency of control of working process in afterburner combustion chamber due to measurement of value of full pressure of gas flow at output from afterburner combustion chamber and control of position of distributing valve of fuel collectors.
EFFECT: invention differs from known ones in that it is additionally measured value of full pressure of gas flow at output of afterburner combustion chamber and control over position of distributing valve of fuel manifolds.
1 cl, 3 dwg
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Authors
Dates
2019-09-16—Published
2017-12-18—Filed