首页> 外国专利> Box-type aircraft engine e.g. jet engine, mounting structure, has monolithic framework covered with mechanically assembled covering panels, and fixed with reinforcement fittings mechanically secured to engine and/or wings fastening points

Box-type aircraft engine e.g. jet engine, mounting structure, has monolithic framework covered with mechanically assembled covering panels, and fixed with reinforcement fittings mechanically secured to engine and/or wings fastening points

机译:箱式飞机发动机喷气发动机,安装结构,具有被机械组装的盖板覆盖的整体式框架,并通过机械固定到发动机和/或机翼固定点的加强配件固定

摘要

The structure has a monolithic framework (20), constructed by smelting or welding, covered with mechanically assembled covering panels (40) made of composite material. Reinforcement fittings (30) are mechanically secured to the jet engine and/or wings fastening points (26). The fittings are added to the framework in order to double the points. The framework defines ribs (22) and corner supports (24). An independent claim is also included for a method of manufacturing a box type aircraft engine mounting structure.
机译:该结构具有通过熔炼或焊接构造的整体框架(20),该整体框架覆盖有由复合材料制成的机械组装的覆盖面板(40)。加强配件(30)机械固定在喷气发动机和/或机翼固定点(26)上。配件已添加到框架中,以使点数加倍。框架限定肋(22)和角支撑(24)。还包括一种用于制造箱式飞机发动机安装结构的方法的独立权利要求。

著录项

  • 公开/公告号FR2891252A1

    专利类型

  • 公开/公告日2007-03-30

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE;

    申请/专利号FR20050052934

  • 发明设计人 LAFONT LAURENT;

    申请日2005-09-28

  • 分类号B64D27/26;

  • 国家 FR

  • 入库时间 2022-08-21 20:26:55

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