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Structural assembly of part of an aircraft and aircraft, particularly rotary-wing aircraft, comprising such a structural assembly

机译:飞机和飞机,尤其是旋翼飞机的一部分的结构组装,包括这种结构组装

摘要

Structural assembly of part of an aircraft and aircraft, particularly a rotary-wing aircraft, comprising such a structural assembly.;The structural assembly comprises an outer structure (3) equipped with a floor (4), a cladding assembly (5) comprising cladding panels (6) forming a self-supporting envelope (7) which is arranged inside (9) the outer structure (3) and mounted on the floor (4), and a connecting system (10) for connecting the self-supporting envelope (7) to the outer structure (3). The connecting system (10) comprises a number of connecting means (11) which, by rigid and permanent connections, fix the self-supporting envelope (7) to the outer structure (3) and perform this rigid and permanent fixing only between the floor (4) of the outer structure (3) and ends (12) of cladding panels (6) of the self-supporting envelope (7).
机译:飞机和飞机,尤其是旋翼飞机的一部分的结构组装件,包括这种结构组装件;该结构组装件包括配备有地板( 4)的外部结构( 3 ),包层组件( 5 ),包括形成自支撑外壳( 7 )的包层面板( 6 ),布置在( 9 )的内部结构( 3 )的内部并安装在地板( 4 )上,并连接系统( 10 ),用于将自支撑信封( 7 )连接到外部结构( 3 )。连接系统( 10 )包括多个连接装置( 11 ),这些装置通过刚性和永久连接固定自支撑包膜( 7 )到外部结构( 3 )上,并仅在外部结构( 3 >)和自支撑信封( 7 )的覆层面板( 6 )的端部( 12 )。

著录项

  • 公开/公告号US6766985B2

    专利类型

  • 公开/公告日2004-07-27

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号US20020212813

  • 发明设计人 MARC DUSSAC;HENRI-CHARLES VINCENT;

    申请日2002-08-07

  • 分类号B64C10/00;

  • 国家 US

  • 入库时间 2022-08-21 23:18:18

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