首页> 外国专利> AIRCRAFT CABIN WITH SECONDARY AIRCRAFT CABIN STRUCTURE MOUNTED WITH ROTARY JOINTS AND METHOD FOR MOUNTING A SECONDARY AIRCRAFT CABIN STRUCTURE IN AN AIRCRAFT CABIN

AIRCRAFT CABIN WITH SECONDARY AIRCRAFT CABIN STRUCTURE MOUNTED WITH ROTARY JOINTS AND METHOD FOR MOUNTING A SECONDARY AIRCRAFT CABIN STRUCTURE IN AN AIRCRAFT CABIN

机译:具有旋转接头的第二飞机客舱结构的飞机客舱以及用于安装在飞机客舱中的第二飞机客舱结构的方法

摘要

The present invention pertains to an aircraft cabin (100) comprising a primary structure (40), a secondary aircraft cabin structure (50), and a plurality of interconnecting struts (20) coupling the primary structure (40) to the secondary aircraft cabin structure (50), each of the plurality of interconnecting struts (20) comprising engaging members (21,22) at the respective end portions for insertion into strut holding fixtures (11) of corresponding rotary joints (10) attached at each opposing end. Each of the rotary joints (10) comprises an outer shell segment (1) having the outer shape of a segment of a solid of revolution, the outer shell segment (1) having an opening (4) arranged in the outer surface, an inner shell segment (2) having the outer shape of the segment of the solid of revolution of the outer shell segment (1), the inner shell segment (2) being aligned concentrically with the outer shell segment (1) and spaced apart from the outer shell segment (1) by a compensation gap, and a strut holding fixture (11) having a hollow interior and a flange portion (13) and being arranged in the opening (4) so that the flange portion (13) extends within the compensation gap between the inner shell segment (2) and the outer shell segment (1).
机译:本发明涉及一种飞机机舱(100),其包括主要结构(40),次要飞机机舱结构(50)以及将主要结构(40)耦合到次要飞机机舱结构的多个互连支柱(20)。 (50),多个互连支柱(20)中的每一个在相应的端部包括接合构件(21,22),用于插入附接在每个相对端的相应的旋转接头(10)的支柱固定夹具(11)中。每个旋转接头(10)包括外壳部分(1),外壳部分(1)具有旋转实体的一部分的外形,外壳部分(1)具有布置在外表面中的开口(4),内部外壳段(2)具有外壳段(1)的旋转实体段的外形,内壳段(2)与外壳段(1)同心对齐并与外壳段隔开壳体段(1)和补偿间隙,以及具有中空内部和凸缘部分(13)并布置在开口(4)中以使凸缘部分(13)在补偿范围内延伸的支柱固定装置(11)内壳段(2)和外壳段(1)之间的间隙。

著录项

  • 公开/公告号EP3281860A1

    专利类型

  • 公开/公告日2018-02-14

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号EP20160183322

  • 发明设计人 BENTHIEN HERMANN;SCHAEFER BASTIAN;

    申请日2016-08-09

  • 分类号B64C1/00;E04B1/19;

  • 国家 EP

  • 入库时间 2022-08-21 13:16:12

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