FIELD: aviation.
SUBSTANCE: invention relates to aviation and concerns a power plant for an aircraft. The power plant (hereinafter – PP) contains the first and the second rotating moving bodies designed for being installed from both sides of the main hull of the aircraft, a gearbox connected to the first and the second moving bodies via the first and the second mechanical shafts, respectively. PP also contains a single gas generator connected to the gearbox and made with the possibility of rotation of the first and the second rotating moving bodies, and a single auxiliary turbomachine made with the possibility of rotation of the first and the second rotating moving bodies regardless the gas generator.
EFFECT: simple and efficient PP is achieved, which can be used on small-sized aircrafts, while providing optimal thrust, switching between an auxiliary turbomachine and a gas generator in case of failure of the gas generator is provided.
13 cl, 9 dwg
