发明名称 AIR FLOW CONTROL MEANS FOR CHANNEL WINGED AIRCRAFT
摘要 An apparatus for use with channel winged aircraft to seal the airfoil surface of the channel between the trailing edge thereof and the propeller tip, by discharging jets of water rearwardly from the leading edge of the airfoil surface of the channel to form a film of water on said surface. The film of water seals the space between the propeller tip traveling at or near the speed of sound and the channel surface where very low pressure is created just ahead of the propeller tip, so as to prevent spillback of air through this space.
申请公布号 US3705700(A) 申请公布日期 1972.12.12
申请号 USD3705700 申请日期 1970.10.23
申请人 WILLARD R. CUSTER 发明人 WILLARD R. CUSTER
分类号 B64C23/00;(IPC1-7):B64C3/32 主分类号 B64C23/00
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