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The stirrup of display for aircraft engine assembly engine for aircraft and the assembly process of an aircraft engine on the structure of a display hanger ru00ecgida

机译:飞机发动机组装发动机的显示器的箍筋和在显示器吊架的结构上飞机发动机的组装过程

摘要

The stirrup of display for aircraft engine assembly engine for aircraft and the assembly process of an aircraft engine on the structure ru00ecgida a stirrup for display.The invention relates to a hanger for display (4) for aircraft engine, the stirrup including a rigid structure (10) which form a closed coffin in front by a front locking rib (36), and a mounting system which comprises mainly a motor fixing D And the engine front (6) which includes a body for fixing (46) mounted at the rigid structure (10).According to the invention, the body fitting (46) is applied against a front surface (38), and the stirrup (4) comprises at least a top shear (68) which crosses at least partially the body fitting (46) as well as the front locking rib (36).
机译:用于飞机的飞机发动机组装发动机的显示器的箍筋,以及在显示器的箍筋结构上的飞机发动机的组装方法。用于飞机发动机的显示器的悬挂件(4),其包括刚性的箍筋该结构(10)通过前部锁定肋(36)在前面形成封闭的棺材,以及一种安装系统,其主要包括电动机固定装置D和发动机前部(6),该发动机前部(6)包括安装在壳体上的用于固定的主体(46)根据本发明,主体配件(46)抵靠前表面(38)施加,并且箍筋(4)包括至少一个顶部剪力器(68),该顶部剪力器至少部分地穿过主体配件。 (46)以及前锁定肋(36)。

著录项

  • 公开/公告号BRPI0616140A2

    专利类型

  • 公开/公告日2012-04-10

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号BR2006PI16140

  • 申请日2006-09-22

  • 分类号B64D27/26;

  • 国家 BR

  • 入库时间 2022-08-21 17:25:31

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