发明名称 Stol aircraft with wing tip gas outlet - has orifices all along wing tips, ailerons and flaps and has single lever flap setting and nozzle tilting
摘要 <p>The STOL aircraft has wing tip and edge outlets for pressurised and exhaust gas from the engine. The outlets are in wing tip-shaped, hollow caps which can be rotated between a position with the openings closed, pointing outwards, and one with them open, pointing downwards. Ailerons and flaps are hollow and have outlets in the trailing edges the flaps being supplied through flexible hoses. A toggle lever controls flap position by a linkage from one fulcrum, and sets the outlet by a Bowden-cable from the other one. The tip outlets are angled inwards progressively from the leading edge.</p>
申请公布号 DE2159184(C2) 申请公布日期 1983.12.08
申请号 DE19712159184 申请日期 1971.11.29
申请人 WEINERT, EDUARD, 8011 BRUNNTHAL, DE 发明人 WEINERT, EDUARD, 8011 BRUNNTHAL, DE
分类号 B64C23/00;(IPC1-7):64C9/38 主分类号 B64C23/00
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