VERTICAL TAKE-OFF AND LANDING AIRCRAFT Russian patent published in 2001 - IPC

Abstract RU 2165867 C2

FIELD: aviation. SUBSTANCE: aircraft has fuselage, wing and engines whose gas flow washes part of upper surface of wing. Engines are arranged in front portion of aircraft in such way that axis of escaping gases and air ejected at this is located tangentially relative to upper surface of wing. Wing is M-shaped in configuration and is secured to fuselage in lower rear part. EFFECT: increased lift force at take-off and landing; reduced sizes of runways. 2 dwg

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RU 2 165 867 C2

Authors

Bezrukov Ju.I.

Dates

2001-04-27Published

1996-07-23Filed