FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly to hybrid aircrafts. Aircraft comprises thrust generating unit, unit for energy generation and electric transfer unit for energy transmission from unit of generation of energy to thrust generating unit. Thrust generation unit consists of motor and connected with it by means of propeller shaft. Unit for energy generation consists of internal combustion engine and connected to it by means of electric generator shaft. In aircraft structure there is device, guiding sound of engines upwards from aircraft, having channel to direct sound upward and axis of rotation positioned across specified direction of aircraft flight.
EFFECT: possibility to provide large number of structural degrees of freedom when determining positions of aircraft units.
23 cl, 2 dwg
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