The invention relates to an aircraft cabin air distribution system, an aircraft and a method of feeding air into a cabin of a fuselage. An aircraft cabin air distribution system has a fuselage, a cabin in the fuselage, a supply duct, and a plurality of outlets configured to feed air into the cabin. The outlets include an upper outlet positioned at a higher level than the supply conduit and a lower outlet positioned at a lower level than the supply conduit. The aircraft cabin air distribution system also includes a plurality of branch ducts configured to feed air from the supply duct to the outlet, where each branch duct is in contact with the supply duct at a respective junction. The branch ducts include upper branch ducts each feeding air to one or more of the upper outlets and lower branch ducts each feeding air to one or more of the lower outlets.

    本发明涉及飞行器机舱空气分配系统、飞行器及将空气给送到机身的机舱中的方法。飞行器机舱空气分配系统具有机身、机身中的机舱、供应管道和构造成将空气给送到机舱中的多个出口。出口包括上出口和下出口,上出口定位在比供应管道更高的水平处,下出口定位在比供应管道更低的水平处。飞行器机舱空气分配系统还包括多个分支管道,多个分支管道构造成将空气从供应管道给送至出口,其中,每个分支管道在相应的接合部处与供应管道相接。分支管道包括上分支管道和下分支管道,上分支管道各自将空气给送至上出口中的一个或更多个上出口,下分支管道各自将空气给送至下出口中的一个或更多个下出口。


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    Titel :

    Aircraft cabin air distribution system, aircraft and method of feeding air into cabin of fuselage


    Weitere Titelangaben:

    飞行器机舱空气分配系统、飞行器及将空气给送到机身的机舱中的方法


    Beteiligte:

    Erscheinungsdatum :

    21.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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