VERTICAL TAKE-OFF AND LANDING AIRCRAFT Russian patent published in 2014 - IPC B64C29/00

Abstract RU 2524318 C1

FIELD: aircraft engineering.

SUBSTANCE: VTOL aircraft consists of fuselage, wing, tail unit, compressor with air intake and engine. Diesel shaft is arranged aligned with aircraft lengthwise axis and engaged via step-up gearing with compressor shaft. Compressor receiver is communicated via air duct extending through fuselage and equipped with throttles with electromechanical drive with the wing leading and tailing edge air duct and tail unit leading edge air duct, said edges being equipped with slot-type nozzles. Nozzles of the wing and tail unit leading edges are directed tangentially to top skins while wing tailing edge air duct nozzle is directed in bisecant. Said throttles with electromechanical drive are connected with aircraft vertical stabilisation system built around digital processor. Compressor shaft output end can be equipped with propeller.

EFFECT: vertical takeoff and landing, lower noise.

2 cl, 5 dwg

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RU 2 524 318 C1

Authors

Pikulev Nikolaj Mikhajlovich

Dates

2014-07-27—Published

2013-06-25—Filed