发明名称 VERTICAL TAKE-OFF AND LANDING AIRCRAFT
摘要 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
申请公布号 RU2165867(C2) 申请公布日期 2001.04.27
申请号 RU19960114924 申请日期 1996.07.23
申请人 BEZRUKOV JURIJ IVANOVICH 发明人 BEZRUKOV JU.I.
分类号 B64C29/00;B64C3/10;B64D27/02;(IPC1-7):B64C29/00 主分类号 B64C29/00
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