首页> 外国专利> The structure ru00ecgida a stirrup of display of aircraft engine and the stirrup of display of aircraft engine,

The structure ru00ecgida a stirrup of display of aircraft engine and the stirrup of display of aircraft engine,

机译:r u00ecgida的结构是飞机发动机的展示架和飞机发动机的展示架,

摘要

The structure ru00ecgida a stirrup of display of aircraft engine and the stirrup of display of aircraft engine.The invention relates to a rigid structure (8) of a hanger for display of aircraft engine, which is presented in the form of a closed casket for a first and a second side panel of the coffin (34a, 34B), this rigid structure including spaces intemervuras (38 ~ 1 ~ 38 ~ 8 ~) each delimited by two transversal ribs (36) directly in succession of the coffin.According to the invention, for each space internervuras which belongs to a group that includes at least three spaces intemervuras any and that are directly consecutive, a single access opening (42 ~ 1 ~ 42 ~ 8 ~) is provided in the side panels, these openings being arranged In the alternation in the first and second side panels.
机译:一种用于飞机发动机的展示架的rup架和一种用于飞机发动机的展示架的。架。本发明涉及一种用于飞机发动机的展示架的悬挂架的刚性结构(8),其以封闭的棺材的形式呈现。对于棺材(34a,34B)的第一和第二侧板,这种刚性结构包括内部空隙(38〜1〜38〜8〜),每个空隙都直接由棺材连续地由两个横向肋(36)界定。根据本发明,对于属于至少包括三个间隔的任何间隔且直接连续的一组的每个间隔神经,在侧板中提供单个进入开口(42〜1〜42〜8〜)。在第一和第二侧面板中交替布置。

著录项

  • 公开/公告号BRPI0616484A2

    专利类型

  • 公开/公告日2011-06-21

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号BR2006PI16484

  • 发明设计人 LIONEL BERNARDI;THIERRY HUGUET;

    申请日2006-10-05

  • 分类号B64D27/26;

  • 国家 BR

  • 入库时间 2022-08-21 18:07:12

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