FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to convertible aircraft. Proposed aircraft has folding high wing with all-moving outer wings, bypass turbojet engines and motors. Motors are provided with propellers and arranged in more than two shaped annular channels integrated with each other and with high wing. Wing has flaps and outer flaperons. Propellers generate lifting and sustaining distributed or jet thrust by propellers in helicopter and aircraft flight configuration with low or high heat and sound signature in flight mode with spinning or dead propellers with running engines.
EFFECT: simplified design, better controllability at VTOL, increased speed, range and transportation efficiency.
2 cl, 3 dwg
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