The invention relates to a fastening unit (100) for movably fastening an aircraft component (300) to a support structure (400) of an aircraft (500). The fastening unit (100) has a connection element (5) having a hole (5a). The fastening unit (100) also has a first support arm (1) having a first end (1a) for connecting to the support structure (400) of the aircraft (500) and having a second end (1b) for connecting to the connection element (5). The fastening unit (100) also has a second support arm (2) having a first end (2a) for connecting to the support structure (400) of the aircraft (500) and having a second end (2b) for connecting to the connection element (5). The first support arm (1) and the second support arm (2) are arranged in such a way 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 than 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 produced at least partly by means of a deformation method. The invention further relates to the use of a fastening unit (100) for fastening arudder (300) to a support structure (400) of an aircraft (500) and to a method for providing movable fastening of an aircraft component (300) to a support structure (400) of an aircraft.

    本发明涉及一种用于将飞行器部件(300)可移动地紧固在飞行器(500)的支撑结构(400)上的紧固单元(100)。所述紧固单元(100)具有带有凹陷(5a)的连接元件(5)。所述紧固单元(100)还具有第一支臂(1),所述第一支臂具有用于与所述飞行器(500)的支撑结构(400)连接的第一端部(1a)和用于与所述连接元件(5)连接的第二端部(1b)。所述紧固单元(100)还具有第二支臂(2),所述第二支臂具有用于与所述飞行器(500)的支撑结构(400)连接的第一端部(2a)和用于与所述连接元件(5)连接的第二端部(2b)。所述第一支臂(1)和所述第二支臂(2)被布置成使得所述第一支臂(1)的第一端部(1a)与所述第二支臂(2)的第一端部(2a)之间的间隔(d)大于所述第一支臂(1)的第二端部(1b)与所述第二支臂(2)的第二端部(2b)之间的间隔(e)。所述第一支臂(1)至少部分地借助于成型工艺制造。本发明还涉及用于将方向舵(300)紧固在飞行器(500)的支撑结构(400)上的紧固单元(100)的用途以及一种用于提供将飞行器部件(300)可移动地紧固在飞行器的支撑结构(400)上的方法。


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    Titel :

    FASTENING UNIT FOR MOVABLY FASTENING AN AIRCRAFT COMPONENT TO A SUPPORT STRUCTURE OF AN AIRCRAFT


    Weitere Titelangaben:

    用于将飞行器部件可移动地紧固在飞行器的支撑结构上的紧固单元


    Beteiligte:
    SEITZ PHILIPP (Autor:in) / BAJORAT FALK (Autor:in) / BOCEK MARTIN (Autor:in)

    Erscheinungsdatum :

    10.04.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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