The invention relates to a fluid pipe connector, an aircraft fuel system, an aircraft and a disassembly and assembly method, the fluid pipe connector comprises an inner pipe assembly, the inner pipe assembly comprises a first inner pipe section and a second inner pipe section, and an inner connecting part located between the first inner pipe section and the second inner pipe section; an outer tube assembly including a first outer tube section, a second outer tube section, a housing covering the inner link and mechanically connecting the first outer tube section to the second outer tube section via a mechanical connection, and a door secured to the housing by one or more fasteners and covering a hole in the housing, the hatch door is movable between a closed position and an open position to provide access to the inner link through the aperture.

    本发明涉及一种流体管连接件、一种飞行器燃料系统、一种飞行器及拆装方法,该流体管连接件包括:内管组件,该内管组件包括第一内管部段和第二内管部段以及位于第一内管部段与第二内管部段之间的内连结部;外管组件,该外管组件包括第一外管部段、第二外管部段、罩壳以及舱门,该罩壳覆盖内连结部并且经由机械连接将第一外管部段机械地连接至第二外管部段,该舱门通过一个或更多个紧固件紧固至罩壳并且覆盖罩壳中的孔,其中,该舱门能够在闭合位置与打开位置之间移动以提供通过孔接近内连结部的途径。


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    Title :

    Fluid pipe connecting piece, aircraft fuel system, aircraft and disassembling and assembling method


    Additional title:

    流体管连接件、飞行器燃料系统、飞行器及拆装方法


    Contributors:

    Publication date :

    2023-04-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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