首页> 外国专利> Grid for thrust reverser system of ducted-fan turbine engine i.e. jet engine, of aircraft, has two modules for respectively holding two opposite vanes at two ends of two supports, where grid is telescopic and extensible

Grid for thrust reverser system of ducted-fan turbine engine i.e. jet engine, of aircraft, has two modules for respectively holding two opposite vanes at two ends of two supports, where grid is telescopic and extensible

机译:用于管式风扇涡轮发动机(即飞机的喷气发动机)的推力反向器系统的格栅具有两个模块,用于分别在两个支架的两端固定两个相对的叶片,其中格栅是可伸缩的

摘要

The grid (108) has two modules (30) respectively holding two opposite vanes at two ends of two supports, where the grid is telescopic and extensible. The modules are moved and slidingly assembled with respect to each other. A rail is cooperated with the support. An independent claim is also included for a thrust reverser system for a turbomachine of an aircraft, including a grid.
机译:格栅(108)具有两个模块(30),两个模块(30)分别在两个支撑件的两端保持两个相对的叶片,其中格栅是可伸缩的和可伸长的。模块彼此相对移动和滑动组装。导轨与支架配合。还包括用于飞机的涡轮机的反推力系统的独立权利要求,所述涡轮机包括网格。

著录项

  • 公开/公告号FR2947869A1

    专利类型

  • 公开/公告日2011-01-14

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号FR20090003423

  • 发明设计人 CHANEZ PHILIPPE GERARD;

    申请日2009-07-10

  • 分类号F02K1/72;

  • 国家 FR

  • 入库时间 2022-08-21 17:45:50

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