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ENGINE MOUNT FOR AN AIRCRAFT, TO BE PLACED BETWEEN AN ENGINE AND AN ENGINE MOUNTING STRUCTURE

机译:用于飞机的发动机座,应放置在发动机和发动机座架结构之间

摘要

An aircraft engine attachment configured to be inserted between an engine and an EMS, the attachment including a plate assembly connected to a first fixing device including an end fitting with two arms and a pin passing through the plate assembly and the two arms, in each of which an orifice is formed including a first ring and a second ring respectively holding the pin. The first ring includes a bottom acting as a stop for a first end of the pin, and the first attachment device includes a mechanism to stop the pin in translation cooperating with a second end of the pin.
机译:被配置为插入发动机和EMS之间的飞机发动机附件,该附件包括板组件,该板组件连接到第一固定装置,该第一固定装置包括具有两个臂的端部配件和穿过该板组件和两个臂的销,孔形成为包括分别保持销的第一环和第二环。第一环包括用作销的第一端的止动件的底部,并且第一附接装置包括用于使销与销的第二端协作地停止平移的机构。

著录项

  • 公开/公告号EP1896326B1

    专利类型

  • 公开/公告日2009-10-28

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号EP20060763903

  • 发明设计人 GARDES PASCAL;AUDART-NOEL VIRGINIE;

    申请日2006-06-27

  • 分类号B64D27/26;

  • 国家 EP

  • 入库时间 2022-08-21 19:17:22

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