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Aircraft ventral fairing partition wall and aircraft equipped with a ventral fairing

机译:飞机腹整流罩隔墙和装有腹整流罩的飞机

摘要

The invention concerns a wall (10) of vertical partitioning for a ventral cowling of an aircraft including a plurality of vertical panels (11, 12, 12′, 13, 13′), each panel being linked to an adjacent panel by a vertical post (14, 15, 16). At least one exterior panel (13, 13′) is mounted in a fixed manner on at least one associated vertical post (14, 16). The upper end of said vertical post is fitted with a means of fastening in transverse rotation intended to be fixed to the structure (8) of an aircraft, the means of fastening in transverse rotation being capable of allowing the displacement (Dy) of the structure of the aircraft with respect to the fixed partitioning wall. It is also possible for at least one intermediary panel (12, 12′) to be mounted floating on at least one associated vertical post (15, 16), in such a way as to have a deflection parallel and perpendicular to the adjacent panels.
机译:本发明涉及一种用于飞机的腹罩的垂直分隔壁( 10 ),其包括多个垂直面板( 11、12、12',13、13' ),每个面板都通过垂直柱( 14、15、16 )链接到相邻的面板。至少一个外部面板( 13、13')以固定方式安装在至少一个相关的垂直立柱( 14、16 )上。所述垂直支柱的上端装有横向旋转的紧固装置,该紧固装置旨在固定到飞机的结构( 8 ),横向旋转的紧固装置能够允许飞机结构相对于固定分隔壁的位移(Dy)。在这种情况下,至少一个中间面板( 12、12')也可以浮动地安装在至少一个相关的垂直立柱( 15、16 )上。方式是具有平行于和垂直于相邻面板的偏转。

著录项

  • 公开/公告号US8066221B2

    专利类型

  • 公开/公告日2011-11-29

    原文格式PDF

  • 申请/专利权人 FRANCOIS ROUYRE;

    申请/专利号US20060096459

  • 发明设计人 FRANCOIS ROUYRE;

    申请日2006-11-23

  • 分类号B64C1/10;B64C1/38;

  • 国家 US

  • 入库时间 2022-08-21 17:26:01

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