发明名称 High effect lift control for hovercraft - has airstream from central thruster deflected over inclined profiled wings set about craft skirt
摘要 <p>The high effect hovercraft has profiled wings (11) set about the skirt of the craft and has the airstream from the central thruster (18) deflected over the angled wings to achieve lift. The craft lies higher than a conventional air cushion in a controlled way. The lift is achieved without having a high airspeed, and can be generated by different types of impeller, including radial types, or jets. The control of the wing angles provides different lift, while differential control generates horizontal, thrust.</p>
申请公布号 FR2354241(A1) 申请公布日期 1978.01.06
申请号 FR19770017332 申请日期 1977.06.07
申请人 CLUCAS REGINALD 发明人
分类号 B64C39/06;(IPC1-7):64C29/00 主分类号 B64C39/06
代理机构 代理人
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