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Door for a subspace of thrust type door, subspace thrust type door and the nacelle to the engine turbojato

机译:推力型门子空间门,子空间推力型门和发动机涡轮喷气发动机的机舱

摘要

A door for a door-type thrust reverser is pivotally mounted on a stationary structure of a thrust reverser. The door includes an inner surface integrated to a flow path of an air flow generated by a turbojet engine, an outer surface providing an outer aerodynamic continuity of a nacelle equipped with the thrust reverser, a spoiler to deflect the air flow disposed at an upstream end of the door, and an actuator actuating the spoiler. The spoiler is movably mounted, in rotation around a rotation axis substantially perpendicular to a front frame of the door, between a retracted and a deployed position. In particular, the actuator includes a first rod connected to the spoiler, a second rod connected to the first rod and the front frame, and a third rod connected to the first and second rods as well as to the spoiler.
机译:用于门型推力反向器的门可枢转地安装在推力反向器的固定结构上。该门包括与涡轮喷气发动机产生的气流的流路集成的内表面,提供配备有反推力的机舱的外部空气动力学连续性的外表面,使位于上游端的气流偏转的扰流板。门的顶部,还有一个致动扰流板的致动器。扰流板可移动地安装在缩回位置和展开位置之间,该旋转轴绕基本垂直于门的前框架的旋转轴线旋转。特别地,致动器包括连接到扰流器的第一杆,连接到第一杆和前框架的第二杆,以及连接到第一和第二杆以及扰流器的第三杆。

著录项

  • 公开/公告号BR112014015279A8

    专利类型

  • 公开/公告日2017-06-13

    原文格式PDF

  • 申请/专利权人 AIRCELLE;

    申请/专利号BR20141115279

  • 发明设计人 XAVIER HERT;LUC QUERNET;NICOLAS DEZEUSTRE;

    申请日2012-12-07

  • 分类号F02K1/62;F02K1/70;

  • 国家 BR

  • 入库时间 2022-08-21 13:40:28

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