AIRBORNE VEHICLE Russian patent published in 2015 - IPC B64C29/04 

FIELD: aircraft engineering.

SUBSTANCE: aircraft consists of airframe rigidly coupled with engine that has rigid coupling with first exhaust nozzle behind the engine. Besides airframe is rigidly coupled with combustion chamber control unit hydraulically communicated therewith and arranged below and provided with rigid coupling with second exhaust nozzle directed upward. Driven horizontal plate is arranged under exhaust nozzle. Said drive has inlet connected with drive control unit outlet. Aircraft comprises second combustion chamber control unit, second combustion chamber, bent exhaust pipe, third exhaust nozzle, rotary sector spring shutter and vertical prop. Combustion chamber second control unit is arranged ahead of the first control unit and hydraulically connected with second combustion chamber under second control unit rigidly connected with bent exhaust pipe. Said pipe is located above said chamber and rigidly connected with third exhaust nozzle rigidly coupled with airframe. Rotary sector spring-loaded shutter is arranged inside said airframe.

EFFECT: accelerated braking at sufficient flight safety.

1 dwg