首页> 外国专利> Thrust reverser e.g. grid, for e.g. two-flow turbojet, has slider connected to downstream end of flap through rod, and telescopic activating actuator driving slider, in translation, in skid when cowl is in downstream translation phase

Thrust reverser e.g. grid, for e.g. two-flow turbojet, has slider connected to downstream end of flap through rod, and telescopic activating actuator driving slider, in translation, in skid when cowl is in downstream translation phase

机译:推力反向器网格,例如双流涡轮喷气发动机,其滑阀通过杆连接至襟翼的下游端,而伸缩式执行机构驱动滑阀在整流罩处于下游平移阶段时处于平移,打滑状态

摘要

The reverser has a driving slider (24) for driving an inversion flap (20) and movably mounted in a lateral launching skid (33) arranged in a longitudinal sliding cowl (2), where the slider is in a form of movable intermediate stub. The slider is connected to a downstream end of the flap through a driving rod (30), such that the traversing movement of the slider in the launching skid is accompanied by pivoting the rod and by the flap. A telescopic activating actuator drives the slider, in translation, in the skid when the sliding cowl is in a downstream translation phase.
机译:反向器具有驱动滑块(24),用于驱动翻转挡板(20),并且可移动地安装在布置在纵向滑动罩(2)中的侧向发射滑道(33)中,其中滑块为可移动中间短管的形式。滑块通过驱动杆(30)连接到襟翼的下游端,使得滑块在发射橇中的横向运动伴随着枢转杆和襟翼。当滑动罩处于下游平移阶段时,伸缩式致动器驱动滑块平移滑动。

著录项

  • 公开/公告号FR2907512A1

    专利类型

  • 公开/公告日2008-04-25

    原文格式PDF

  • 申请/专利权人 AIRCELLE SOCIETE ANONYME;

    申请/专利号FR20060009265

  • 发明设计人 VAUCHEL GUY;BAUDU PIERRE;

    申请日2006-10-23

  • 分类号F02K1/72;B64D33/04;

  • 国家 FR

  • 入库时间 2022-08-21 19:47:09

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