The invention provides a rear pressure bulkhead for an aircraft, a rear fuselage of the aircraft, and the aircraft. The rear pressure bulkhead comprising a dome-shaped structure, and a set of built-inextension components ("petals") homogeneously distributed along the periphery of said dome-shaped structure, so that the dome-shaped structure is secured to a frame of the aircraft, whilst the extension components are secured to longitudinal structures of the aircraft. The invention further provides an aircraft rear fuselage comprising such rear pressure bulkhead so that the available cabin space, i.e. pressurized space, can be extended without enlarging the fuselage.

    本发明提供了一种用于飞行器的后部压力隔板、飞行器的后部机身和飞行器,所述后部压力隔板包括圆顶形结构和一组内置延伸部件(“花瓣状物”),所述组内置延伸部件沿着所述圆顶形结构的周边均匀分布,从而所述圆顶形结构固定到所述飞行器的框架,而所述延伸部件固定到所述飞行器的纵向结构。此外,本发明提供了一种包括这种后部压力隔板的飞行器后部机身,从而可以在不扩大所述机身的情况下扩展可用的机舱空间,即加压空间。


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    Titel :

    Rear pressure bulkhead for aircraft, rear fuselage of aircraft, and aircraft


    Weitere Titelangaben:

    用于飞行器的后部压力隔板、飞行器的后部机身和飞行器


    Beteiligte:

    Erscheinungsdatum :

    2021-02-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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