CONVERTIPLANE Russian patent published in 2006 - IPC B64C39/00 B64C39/12 

FIELD: aviation.

SUBSTANCE: proposed convertiplane has fuselage 1 with cabin, wings 2 and two screws 3. Screws may change their position from vertical to horizontal. Convertiplane engines are mounted in fixed parts of elongated nacelles 4 which are mounted in center section of each wing 2. Mounted on movable part of each engine nacelles 4 are screws 3; nose horizontal fin 5 is located after screws 3. Fixed section of each engine nacelles 4 is provided with vertical tail unit 6 which is inclined inside relative to vertical longitudinal plane of fixed section of engine nacelle 4.

EFFECT: enhanced stability and reliability of flying vehicle.

3 cl, 5 dwg