FIELD: aviation.
SUBSTANCE: invention relates to hybrid propulsion construction for an aircraft. Aircraft engine structure comprises two reversible electric machines, which rotors are connected with both the low-pressure shaft and the high-pressure shaft by means of transmissions which are alternately disconnected depending on the rotor rotation direction. Transmissions comprise passive one-way clutches with opposite directions of engagement.
EFFECT: independent operating modes of machines are provided as a starter or as an electric generator of each of shafts.
6 cl, 7 dwg
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