发明名称 Supersonic delta wing aircraft - contains trapezoidal opening in each wing to increase lift at subsonic speeds
摘要 <p>The delta-wing aeroplane contains an opening in each wing which takes the shape of a triangle, trapezium or parallelogram. The section of wing situated in front of the opening itself forms a front wing, the trailing edge of which is formed by the front edge of the opening. The section of wing situated behind the opening forms a rear wing, the leading edge of which is formed by the rear edge of the opening. The arrangement allows supersonic aircraft to generate extra lift at subsonic speeds.</p>
申请公布号 FR2526755(A1) 申请公布日期 1983.11.18
申请号 FR19820008607 申请日期 1982.05.17
申请人 NGUYEN MANH KHANH 发明人
分类号 B64C3/54;B64C39/06;(IPC1-7):64C3/54 主分类号 B64C3/54
代理机构 代理人
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