AIRCRAFT Russian patent published in 2010 - IPC B64G1/26 B64D33/00 

FIELD: transport.

SUBSTANCE: invention relates to airspace engineering and can be used in atmospheric and cosmic flights using jet propulsion facilities. The aircraft contains frame with cylinder (combustion chamber) equipped with the first and the second exhaust nozzle. The second nozzle is located in front of cylinder and ends with bended down exhaust pipe coming out of the frame after bend below the cylinder. In the mentioned cylinder there are two shock-absorbers the entries of which are hydraulically connected with shock-absorber control unit. Between shock-absorbers a plate (movable) is installed which divides the cylinder into two chambers where fuel combustion takes place. This fuel is supplied to shock-absorbers from the mentioned control unit.

EFFECT: providing aircraft reliability while increasing its flight speed.

1 dwg