首页> 外国专利> Tool for handling high pressure module of turbojet of aircraft, has fixing arms connected to vertical branches of support body by pivot joint, so as to allow rotation of high pressure module about horizontal rotation axis between branches

Tool for handling high pressure module of turbojet of aircraft, has fixing arms connected to vertical branches of support body by pivot joint, so as to allow rotation of high pressure module about horizontal rotation axis between branches

机译:用于操纵飞机涡轮喷气发动机高压模块的工具,其固定臂通过枢轴连接到支撑体的垂直分支,从而允许高压模块绕分支之间的水平旋转轴旋转

摘要

The tool has a support body (7) having an inverted U-shape and defining a horizontal beam (70) and two vertical branches (71, 72). Two fixing arms (81, 82) are attached to a high pressure module of a turbojet of an aircraft, where the fixing arms are connected to the vertical branches of the support body by a pivot joint (9), so as to allow rotation of the high pressure module about a horizontal rotation axis (V) between the branches of the support body. The socket body includes a fixing ring (73) for connection to a traction chain.
机译:该工具具有支撑主体(7),该支撑主体(7)具有倒U形形状并限定了水平梁(70)和两个垂直分支(71、72)。两个固定臂(81、82)附接至飞机的涡轮喷气发动机的高压模块,其中,固定臂通过枢转接头(9)连接至支撑体的竖直分支,从而允许旋转高压模块围绕支撑体的分支之间的水平旋转轴(V)。插座主体包括用于连接至牵引链的固定环(73)。

著录项

  • 公开/公告号FR2990190A1

    专利类型

  • 公开/公告日2013-11-08

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号FR20120054030

  • 发明设计人 TAILPIED FABRICE;CLAYE ANTHONY;

    申请日2012-05-02

  • 分类号B64F5;B66F11;

  • 国家 FR

  • 入库时间 2022-08-21 16:20:53

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