首页> 外国专利> Drive-and guiding device for aircraft, has crank lever arranged, so that rotation direction of lever for driving of flap corresponds to direction of lever for flap, where rotation direction of lever for flap takes place anticlockwisely

Drive-and guiding device for aircraft, has crank lever arranged, so that rotation direction of lever for driving of flap corresponds to direction of lever for flap, where rotation direction of lever for flap takes place anticlockwisely

机译:飞机的驱动和引导装置,具有曲柄,使襟翼驱动杆的旋转方向与襟翼杆的方向一致,襟翼杆的旋转方向逆时针旋转。

摘要

The device has a coupler (26) automatically and rotatably connected with a rear flap (28) and another coupler (30), and supported by a crank lever (24) that is rotatably connected with an airfoil wing (22) of an aircraft. The coupler (30) is connected with the flap by a pendulum support (32). The lever is arranged in such a manner that a rotation direction of the lever for driving of the flap corresponds to a rotation direction of the lever for the flap. The rotation direction of the lever for the flap of a right wing takes place anticlockwisely by a fuselage.
机译:该装置具有联接器(26),该联接器(26)与后襟翼(28)和另一个联接器(30)自动且可旋转地连接,并由曲柄杆(24)支撑,该曲柄杆(24)可旋转地与飞机的机翼(22)连接。耦合器(30)通过钟摆支架(32)与挡板连接。杆被布置成使得用于驱动襟翼的杆的旋转方向对应于用于襟翼的杆的旋转方向。右翼襟翼的控制杆的旋转方向通过机身逆时针旋转。

著录项

  • 公开/公告号DE102005031840A1

    专利类型

  • 公开/公告日2007-03-29

    原文格式PDF

  • 申请/专利权人 AIRBUS DEUTSCHLAND GMBH;

    申请/专利号DE20051031840

  • 发明设计人 HOLERT BEN;

    申请日2005-07-06

  • 分类号B64C3/50;

  • 国家 DE

  • 入库时间 2022-08-21 20:29:55

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