An aircraft structural component including an aircraft skeleton component and a fluid conduit component is described. The aircraft skeleton component (12) divides a space along a longitudinal axis ofthe aircraft skeleton component (12) into two spatial portions arranged on opposite sides of the aircraft skeleton component (12). The fluid conduit component (14) runs on an outer side of the aircraft skeleton component (12) and fluidically connects the two spatial portions. Also described is an aircraft wing with an aircraft structural component, as well as an aircraft with an aircraft structural component or with an aircraft wing.

    本发明描述了一种具有飞行器骨架构件和流体线路构件的飞行器结构构件,该飞行器骨架构件(12)沿飞行器骨架构件(12)的纵向轴线将空间划分成布置在飞行器骨架构件(12)的相对置的侧上的两个区段,该流体线路构件(14)在飞行器骨架构件(12)的外侧上延伸并且将这两个空间区段流体连接起来。此外,本发明还描述了一种具有飞行器结构构件的飞行器机翼以及一种具有飞行器结构构件或飞行器机翼的飞行器。


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    Titel :

    Aircraft structural component including an aircraft skeleton component and a fluid conduit component


    Weitere Titelangaben:

    具有飞行器骨架构件和流体线路构件的飞行器结构构件


    Beteiligte:
    SEEGEL HAUKE (Autor:in) / KARRAS SVEN (Autor:in) / HAEBERLE ANJA (Autor:in)

    Erscheinungsdatum :

    25.08.2020


    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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