发明名称 FLAP ASSEMBLY AIRCRAFT WING
摘要 An airtoil (10), having a trailing edge flap assembly (18) comprising a flap member (20) which in its stowed position is located above a fixed mounting structure (22). There is a rear pivot link (26) connected at its lower end (42) to the mounting structure (22) and by its upper end (44) to an aft portion of the flap (20). There is a forward slideway (40) by which the forward part (32) of the flap (20) is mounted for longitudinal slide motion relative to the fixed mounting structure (22). The flap (20) has a stowed position in the rear portion (16) of the wing (10), and is movable rearwardly with substantial Fowler motion to an intermediate position for take-off, and movable further rearwardly to a fully extended position where the flap (20) extends rearwardly and downwardly for take-off.
申请公布号 DE3175717(D1) 申请公布日期 1987.01.29
申请号 DE19813175717 申请日期 1981.12.16
申请人 THE BOEING COMPANY 发明人 RUDOLPH, PETER K.C.
分类号 B64C9/16;B64C9/20;(IPC1-7):B64C9/16 主分类号 B64C9/16
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