首页> 外国专利> FOLDING TRUSS MECHANISM FOR TRAILING EDGE FLAPS.

FOLDING TRUSS MECHANISM FOR TRAILING EDGE FLAPS.

机译:折叠翼架用于牵引边缘襟翼。

摘要

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 (Fig. 7-9), similar linkage is provided between a forward main flap (66) and an aft flap (64).
机译:摆动的驱动连杆(10)在其下端(18)可枢转地连接到襟翼(20)的前部支撑件(16)。襟翼后部支撑通过后部支撑点和摆动连杆(22)下端之间的枢轴连接(24)提供。摆动连杆(22)的上端枢转地连接(31)到支撑连杆(26)的上端和从动连杆(30)的后端。支撑连杆(26)的下端连接(27)到从主翼部分(13、29)向后突出的梁结构(28)。从动连杆(30)的前端枢转地附接(40)到驱动连杆(10)的中间部分。驱动连杆(10)向后旋转使挡板(20)向后平移,并有少量向下旋转,直到挡板(20)基本完全伸出。然后,该机构的进一步伸展使挡板(20)向下大量旋转。在双槽实施例中(图7-9),在前主襟翼(66)和后襟翼(64)之间提供了类似的连接。

著录项

  • 公开/公告号EP0120013A4

    专利类型

  • 公开/公告日1986-01-28

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP19830900524

  • 发明设计人 HERNDON GERALD FRANKLIN;

    申请日1982-09-29

  • 分类号B64C9/18;B64C9/20;

  • 国家 EP

  • 入库时间 2022-08-22 07:35:55

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