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Mechanical device for the control of a flexible wing aircraft of the delta type by warping of the wing

机译:通过机翼弯曲来控制三角型柔性机翼飞机的机械装置

摘要

The steering wheel 12 acts on the torsion tube 13 and the pulley 14 which drives the cable 16 guided by the two pulleys 15 for driving the pulley 17 which is integral with the torsion tube 11. This tube bears, at each end, two pinions 20 which act simultaneously on the rack gears fixed onto the transverse shafts 6. It follows that the circular movements of the steering wheel 12 are translated into linear movements of the shafts 6, to left and to right, these movements are transmitted to the structure of the wing by means of ball joints articulated onto the clevises fixed to the tubes joined in a V at their meeting point with the leading edge tube. The tubes transmit the movement which they receive from the shaft 6 to the leading edges. IMAGE
机译:方向盘12作用在扭力管13和皮带轮14上,皮带轮14驱动由两个皮带轮15引导的缆线16,以驱动与扭力管11一体的皮带轮17。该管的两端分别承载两个小齿轮20。齿条同时作用在固定在横轴6上的齿条上。由此,方向盘12的圆周运动转化为轴6的线性运动,即左右运动,这些运动被传递到后轮的结构上。通过铰接在固定在管子上的U形夹上的球窝连接到管子上,该管子在与前缘管子的汇合点以V形连接。管将它们从轴6接收的运动传递到前缘。 <图像>

著录项

  • 公开/公告号FR2555128B1

    专利类型

  • 公开/公告日1986-02-21

    原文格式PDF

  • 申请/专利权人 BAFFERT HUGUES;

    申请/专利号FR19830018696

  • 发明设计人

    申请日1983-11-22

  • 分类号B64C39/00;B64C13/04;

  • 国家 FR

  • 入库时间 2022-08-22 07:31:21

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