首页> 外国专利> An attachment unit for movably securing an aircraft component to a support structure of an aircraft

An attachment unit for movably securing an aircraft component to a support structure of an aircraft

机译:用于将飞机部件可移动地固定到飞机的支撑结构的附接单元

摘要

The invention relates to a fastening unit (100) for movably fastening an aircraft component (300) to a supporting structure (400) of an aircraft (500). The fastening unit (100) has a connection element (5) with a recess (5a). The fastening unit (100) further comprises a first support arm (1) having a first end (1a) for connection to the support structure (400) of the aircraft (500) and a second end (1b) for connection to the connection element (5). The fastening unit (100) further comprises a second support arm (2) having a first end (2a) for connection to the support structure (400) of the aircraft (500) and a second end (2b) for connection to the connection element (5). The first support arm (1) and the second support arm (2) are arranged such that a distance (d) between the first end (1a) of the first support arm (1) and the first end (2a) of the second support arm (2) is greater is as a distance (e) between the second end (1b) of the first support arm (1) and the second end (2b) of the second support arm (2). The first support arm (1) is at least partially manufactured by means of a forming process. The invention further relates to the use of a fastening unit (100) for attaching a rudder (300) to a support structure (400) of an aircraft (500), and to a method of movably attaching an aircraft component (300) to a support structure (400) of an aircraft ,
机译:本发明涉及一种用于将飞机部件(300)可移动地紧固至飞机(500)的支撑结构(400)的紧固单元(100)。固定单元(100)具有带有凹部(5a)的连接元件(5)。紧固单元(100)还包括第一支撑臂(1),该第一支撑臂(1)具有用于连接至飞机(500)的支撑结构(400)的第一端(1a)和用于连接至连接元件的第二端(1b)。 (5)。紧固单元(100)还包括第二支撑臂(2),该第二支撑臂(2)具有用于连接至飞机(500)的支撑结构(400)的第一端(2a)和用于连接至连接元件的第二端(2b)。 (5)。第一支撑臂(1)和第二支撑臂(2)布置成使得第一支撑臂(1)的第一端(1a)与第二支撑物的第一端(2a)之间的距离(d)臂(2)越大,第一支撑臂(1)的第二端(1b)与第二支撑臂(2)的第二端(2b)之间的距离(e)越大。第一支撑臂(1)至少部分地通过成型工艺制造。本发明还涉及用于将舵(300)附接到飞机(500)的支撑结构(400)的紧固单元(100)的用途,以及将飞机部件(300)可移动地附接到飞机的方法。飞机的支撑结构(400)

著录项

  • 公开/公告号DE102017117314A1

    专利类型

  • 公开/公告日2019-01-31

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号DE201710117314

  • 发明设计人 MARC ANTONIO BENTIVOGLIO;MARCO BIONDINI;

    申请日2017-07-31

  • 分类号B64C1/26;B64C1;

  • 国家 DE

  • 入库时间 2022-08-21 11:45:25

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