首页> 外国专利> Device for supporting reinforcement of leading edge of blade of turboshaft engine, has controlling unit controlling displacement of movable elements to draw aside from wing, which is interdependent by depression

Device for supporting reinforcement of leading edge of blade of turboshaft engine, has controlling unit controlling displacement of movable elements to draw aside from wing, which is interdependent by depression

机译:用于支撑涡轮轴发动机的叶片的前缘的加强的装置,具有控制单元,该控制单元控制可动元件的位移以从机翼拉开,该机翼通过凹陷相互依赖。

摘要

The device (10) has immobilization units (18, 20) for immobilizing a reinforcement (12) in a predetermined bonding position by tightening a junction part. A spacing unit forms a space between wings, and comprises movable elements (34, 36), which are connected to a pumping unit for pumping of air so as create depression between the movable elements and the wings to attach the one of the wings and an aspiration element. A controlling unit controls displacement of the movable elements to draw aside from the other wing, which is interdependent by depression. An independent claim is also included for a method for fixing a reinforcement of leading edge of a blade of a turboshaft engine.
机译:装置(10)具有固定单元(18、20),该固定单元(18、20)用于通过拧紧接合部将加强件(12)固定在预定的接合位置。间隔单元在机翼之间形成空间,并且包括可移动元件(34、36),可移动元件(34、36)连接到用于抽吸空气的泵送单元,从而在可移动元件和机翼之间产生凹陷,以将其中一个机翼和一个机翼连接在一起。愿望元素。控制单元控制可移动元件的位移以从另一侧翼拉开,另一侧翼由下压相互依存。还包括一种用于固定涡轮轴发动机的叶片的前缘的加强件的方法的独立权利要求。

著录项

  • 公开/公告号FR2994884A1

    专利类型

  • 公开/公告日2014-03-07

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号FR20120058278

  • 申请日2012-09-05

  • 分类号B29C65/78;B29C65/48;F04D29/38;

  • 国家 FR

  • 入库时间 2022-08-21 15:36:34

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