发明名称 Folding truss mechanism for trailing edge flaps
摘要 PCT No. PCT/US82/01356 Sec. 371 Date Sep. 29, 1982 Sec. 102(e) Date Sep. 29, 1982 PCT Filed Sep. 29, 1982 PCT Pub. No. WO84/01343 PCT Pub. Date Mar. 29, 1984.A swinging drive link (10) is pivotally connected at its lower end (18) to a forward support (16) for a flap (20). The flap rear support is provided by a pivotal connection (24) between a rear support point and the lower end of a swing link (22). The upper end of the swing link (22) is pivotally connected (31) to the upper end of a support link (26) and the rear end of a slave link (30). The lower end of the support link (26) is attached (27) to a beam structure (28) projecting rearwardly from the main wing section (13, 29). The forward end of the slave link (30) is pivotally attached (40) to an intermediate portion of the drive link (10). Rearward rotation of drive link (10) causes the flap (20) to translate rearwardly with a small amount of downward rotation until the flap (20) is essentially completely extended. Then, further extension of the mechanism rotates the flap (20) a substantial amount downwardly. In a double slot embodiment (FIGS. 7-9), similar linkage is provided between a forward main flap (66) and an aft flap (64).
申请公布号 US4448375(A) 申请公布日期 1984.05.15
申请号 US19820463455 申请日期 1982.09.29
申请人 THE BOEING COMPANY 发明人 HERNDON, GERALD F.
分类号 B64C9/16;(IPC1-7):B64C9/16 主分类号 B64C9/16
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