发明名称 Dipped wing sea-glider stabilised by pendulum cockpit - has main wings and tail with aerial controls and sails with leeward wing tip keel in sea
摘要 The ultra-lightweight sea glider sails with a single wing dipped and is stabilised by a pendulum (6,7). It comprises main wings (1) and a tail unit (8), including wing-tip keel boards (3,4) together with an ariel keel (9) at the tail and a pilots cock-pit (6). When sailing, one wing-tip keel-board (3) is immersed to the leeward whilst the opposite wing tip (4) lifts to the windward. The cockpit takes the form of a freely suspended harness, the wings may be of the bi-plane or the multi-plane type and the harness may be a rigid or semi-rigid seat or fairing. The wings may incorporate slots or jet-pipes. Wing warp may be used to control rolling, and steering may be effected by using the tail keel together with the submerged keel.
申请公布号 FR2498553(A1) 申请公布日期 1982.07.30
申请号 FR19810001674 申请日期 1981.01.29
申请人 ORTAIS PAUL 发明人
分类号 B63B39/06;B63B41/00;B64C39/00 主分类号 B63B39/06
代理机构 代理人
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