The invention discloses a wall covering panel for a nose of an aircraft and the aircraft. The panel comprises a rigid carrying framework preferably having an alveolar structure obtained by 3-D printing, a decor carried by the carrying framework and an acoustically and thermally insulating padding fixed to the carrying framework, and also attachments for fixing the carrying framework to the primarystructure of the aircraft. Preferably, the panel also integrates systems, such as electrical route portions or ventilation route portions that traverse the panel from one side to the other or lead toan outlet equipment item also integrated in the panel. Only the carrying structure of the panel, which carries the decor, the insulating padding and any route portions and equipment items, is fixed to the primary structure of the aircraft. The number of attachments is low; the kitting-out and the finishing of the nose of the aircraft are greatly simplified.

    本发明涉及一种用于飞行器的壁覆盖面板和飞行器。面板包括:刚性承载框架(10),该刚性承载框架优选地具有通过3‑D打印获得的齿槽结构;由承载框架承载的装饰物以及固定至承载框架的声学和热学隔离衬垫(12);以及还有用于将承载框架固定至飞行器的主结构的附接件。优选地,面板还整合了系统,例如电气线路部分或通风回路部分,该电气线路部分或通风回路部分从一侧到另一侧横贯该面板、或通向同样整合在该面板中的出口设备。仅有面板的承载装饰物、隔离衬垫、任何线路部分、以及设备的承载结构固定至飞行器的主结构。附接件数量少;大大简化了飞行器的鼻部的装备和修整。


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    Titel :

    WALL COVERING PANEL FOR AIRCRAFT WITH BUILT-IN INSULATION


    Weitere Titelangaben:

    用于飞行器的壁覆盖面板和飞行器


    Beteiligte:
    GUERING BERNARD (Autor:in) / DELAHAYE ROMAIN (Autor:in)

    Erscheinungsdatum :

    30.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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