发明名称 Vortex reducing wing tip
摘要 An airfoil tip is constructed to droop downward and extend aft of the trailing edge of the air foil structure and to include air foil configuration both chordwise and spanwise with camber in both the chordwise and spanwise directions and further including a vortex opposing twist in the chordwise direction.
申请公布号 US4108403(A) 申请公布日期 1978.08.22
申请号 US19770822134 申请日期 1977.08.05
申请人 FINCH, REGINALD VERNON 发明人 FINCH, REGINALD VERNON
分类号 B64C23/06;(IPC1-7):B64C21/00 主分类号 B64C23/06
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