发明名称 Wing for aircraft has a rear auxiliary lift flap coupled to main wing and able to lie against main wing in retracted position and form air gap with it when extended
摘要 <p>The aircraft wing includes a main wing (301) with a pivoted rear edge (304) and an auxiliary lift flap (302) at the rear of the wing. The auxiliary lift flap is coupled to the main wing, and is arranged so that in its retracted position (300) it is against the wing, and in its extended position (310), forms an air gap with the main wing. The shaped and width of the air gap is adjustable.</p>
申请公布号 DE102004049504(A1) 申请公布日期 2006.04.13
申请号 DE20041049504 申请日期 2004.10.11
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 RECKZEH, DANIEL;DYKE, ADRIAN R.
分类号 B64C3/50;B64C9/16 主分类号 B64C3/50
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