FIELD: aviation.
SUBSTANCE: invention relates to power plants of aircraft. Output device of aircraft jet engine installed on aircraft containing wing comprises engine output nozzle and noise silencer equipped with outlet nozzle. Output device is controlled so that on the takeoff, climb and landing modes in the aircraft noise level limitation zone, the engine output jet through the noise silencer enters the noise silencer outlet nozzle, and in the cruise flight mode enters the engine output nozzle bypassing the noise silencer. Outlet nozzle of noise silencer is made so that at passage through it of outlet jet of engine provides along with longitudinal tie-in vertical force in addition to lifting force of wing.
EFFECT: invention increases efficiency of noise damping during takeoff, set of altitude and landing and at least partially compensates losses of lifting force.
4 cl
Title |
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