The invention relates to an aircraft fuselage part, an aircraft and a method of installation in which a duct assembly in the aircraft fuselage part comprises at least two ducts (9, 11, 13, 14) extending in an overall linear direction of extension, each duct (9, 11, 13, 14) being an electrical, hydraulic or ventilation duct connected to a duct support (15). The pipe support (15) comprises a first slideway element (19) designed to cooperate with a second slideway element in order to form a slideway in the overall direction of extension of the pipe. Thus, the duct assembly can be inserted into an aircraft fuselage portion after installation by translating in the direction of the slide. The installation of the pipe assembly and the installation of the pipe assembly in the fuselage are simplified, and the pipe assembly is more reliable.

    本发明涉及一种飞行器机身部分、飞行器和安装方法,其中,飞行器机身部分中的管道组件包括沿总体直线延伸方向延伸的至少两个管道(9,11,13,14),每个管道(9,11,13,14)是连接至管道支撑件(15)的电气管道、液压管道或通风管道。所述管道支撑件(15)包括第一滑道元件(19),所述第一滑道元件被设计成与第二滑道元件协作,以便在所述管道的总体延伸方向上形成滑道。因此,所述管道组件可以在安装之后通过沿所述滑道的方向平移而插入飞行器机身部分中。简化了所述管道组件的安装及其在机身中的安装,并且所述管道组件更可靠。


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    Titel :

    Aircraft fuselage part, aircraft and installation method


    Weitere Titelangaben:

    飞行器机身部分、飞行器和安装方法


    Beteiligte:

    Erscheinungsdatum :

    2021-06-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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