发明名称 Variable camber leading edge assembly for an airfoil
摘要 A variable camber leading edge device having a movable nose section and an upper flexible panel extending rearwardly from the nose section. To move the nose section between its upper cruise position and a high lift downwardly deflected position, there is attached to the nose section a generally arcuate cam track, having its forward and rear portions curving upwardly. The cam track is constrained to move in a generally arcuate path, but with a movable center of rotation, and is driven by a gear engaging a radially outward rear portion of the track.
申请公布号 US4706913(A) 申请公布日期 1987.11.17
申请号 US19840658674 申请日期 1984.10.09
申请人 THE BOEING COMPANY 发明人 COLE, JAMES B.
分类号 B64C3/48;(IPC1-7):B64C3/50 主分类号 B64C3/48
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