发明名称 Wing trailing edge tongue in an aircraft suspension wing
摘要 Wing trailing edge tongues (10) enable adjustment in the trailing edge angle on the rear surface of an aircraft suspension wing. The rear surface of an aircraft suspension wing can be adjusted for required conditions by setting the draw-out position of the suspension wing trailing edge tongues. Flow increase (23) is achieved with a displacement line (24) on the top side of these tongues
申请公布号 DE19819308(A1) 申请公布日期 1999.10.07
申请号 DE19981019308 申请日期 1998.03.10
申请人 BENKER, GERHARD 发明人 BENKER, GERHARD
分类号 B64C9/18;B64C13/24;(IPC1-7):B64C13/24 主分类号 B64C9/18
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