HELICOPTER OF COMBINED SCHEME Russian patent published in 2018 - IPC B64D1/22 B64C27/08 B64C27/18 

Abstract RU 2641565 C1

FIELD: aviation.

SUBSTANCE: multiscrew helicopter with combined drive of propellers contains fuselage with powerplant hosted in it, upper placed air screw and air screw of reactive point compensation, located at the end of the tail boom. To the fuselage at four cruciform external consoles four propellers with reactive drive are attached. The reactive drive of propellers is carried out with the help of engines installed at the ends of their blades, with forced supply of fuel components in them.

EFFECT: increase of flight performance of an aircraft with a reactive drive of propellers.

3 cl, 2 dwg

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Authors

Lyalin Aleksandr Polikarpovich

Dates

2018-01-18Published

2016-09-27Filed