发明名称 Combined lift flap and aileron for glider - has flap divided with after part hinged to forward part and moving with aileron when extended
摘要 <p>The combined lift flap and aileron for a glider has the flaps conventionally retractably mounted along the wing trailing edge with the ailerons on transverse hinges along the flap trailing edge. Over at least part of their length the flaps are divided transversely, the after portion being hinged to the normally supported forward portion. A setting mechanism for the former coupled to that for the associated aileron has a cam-and-follower coupling actuated by a linkage from the forward portion. This varies a crank length to render the mechanism ineffective with flap retracted.</p>
申请公布号 DE2833524(A1) 申请公布日期 1980.02.14
申请号 DE19782833524 申请日期 1978.07.31
申请人 AKAFLIEG MUENCHEN E.V. FLUGTECHNISCHE FORSCHUNGSGRUPPE AN DER TECHNISCHEN UNIVERSITAET MUENCHEN 发明人 FISCHER,THOMAS,DIPL.-ING.;NESEMANN,ANDREAS;MOERTL,FRITZ;PATTERMANN,WERNER
分类号 B64C9/04;(IPC1-7):B64C9/04 主分类号 B64C9/04
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