FIELD: aviation.
SUBSTANCE: mechanically distributed power plant includes engine for creation of power of mechanical drive, drive shaft, reversing direction of transmission and propulsive fan. Drive shaft is functionally connected to motor to receive power of mechanical drive. Reversing direction transmission has the first rotating shaft and the second rotating shaft, from which the first rotating shaft is functionally connected to the drive shaft for receiving power of the mechanical drive. Direction-reversing transmission is configured to redirect mechanical drive power received at first rotary shaft, from first direction to second direction on second rotating shaft. Propulsion fan is connected to the second rotating shaft for conversion of power of the mechanical drive to the tie-rod. Method of controlling operation of aircraft is characterized by using mechanically distributed power plant with integrated propulsion fan, having mechanically distributed power plant.
EFFECT: group of inventions is aimed at increasing traction, aerodynamic and structural efficiency.
15 cl, 12 dwg
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