The invention relates to a static pressure hole device for an airplane, which comprises a first static pressure hole component, a second static pressure hole component and a third static pressure hole component, the second static pressure hole part comprises one end facing the outer part of the aircraft and the other end located in the skin and facing the first static pressure hole part, and one end of the second static pressure hole part is provided with an air guide hole used for sensing external static pressure and is releasably attached to the skin; the first static pressure hole part is connected to the other end of the second static pressure hole part. By the adoption of the two-piece type static pressure hole component, quick disassembly and assembly outside the static pressure hole device can be achieved (disassembly and assembly can be conducted from the outside), and therefore the maintenance or replacement cost is reduced, and time is saved. The invention also relates to a static orifice system.

    本发明涉及一种用于飞机的静压孔装置,包括:第一静压孔部件,第一静压孔部件相对于飞机的蒙皮固定设置;第二静压孔部件,第二静压孔部件包括面向飞机外部的一端和处于蒙皮之内并朝向第一静压孔部件的另一端,第二静压孔部件在其一端处设有用于感测外部静压的导气孔并且可释放地附连于蒙皮,并且在其另一端处连接于第一静压孔部件。通过采用两件式的静压孔部件,可以实现在静压孔装置的外部快速拆装(可以从外部进行拆装),从而降低维护或更换成本,节约时间。本发明还涉及一种静压孔系统。


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    Titel :

    Static pressure hole device and static pressure hole system for airplane


    Weitere Titelangaben:

    用于飞机的静压孔装置及静压孔系统


    Beteiligte:
    YUAN WENDUO (Autor:in) / ZHAO JIAN (Autor:in)

    Erscheinungsdatum :

    2023-12-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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