The invention relates to a connection assembly (100) for connecting two structural bodies (130, 150) of an aircraft, comprising a central element having a through hole, preferably a bore hole, the central element is arranged to be connected to one of the two structures (150) by means of a fastener element (160, 161) comprising a shank (160 ') inserted into the through-hole, the connection assembly (100) further comprising a plurality of damping elements made of a deformable material, each damping element is fixed on the one hand to the central element and on the other hand is configured to bear against a surface of the other structure (130) of the two structures (130, 150). The invention also relates to an aircraft component (400) comprising such a connection assembly (100).

    本发明涉及一种用于连接飞行器的两个结构体(130、150)的连接组件(100),连接组件(100)包括中央元件,中央元件具有通孔,优选地具有镗孔,中央元件被布置成通过包括插入通孔中的柄部(160’)的紧固件元件(160、161)与两个结构体(150)之一连接,连接组件(100)进一步包括由可变形材料制成的多个减震元件,每个减震元件一方面固定到所述中央元件并且另一方面被构造为抵靠在两个结构体(130、150)中的另一个结构体(130)的表面上。本发明还涉及一种包括这种连接组件(100)的飞行器部件(400)。


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    Title :

    Connecting assembly for connecting two aircraft structures, aircraft component comprising such assembly, and aircraft


    Additional title:

    用于连接两个飞行器结构体的连接组件、包括这种组件的飞行器部件以及飞行器


    Contributors:

    Publication date :

    2022-10-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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