The invention relates to an aircraft assembly, an aircraft wing and a method of operating an aircraft assembly. An aircraft assembly has a cover having an outer aerodynamic surface and an aperture having a stop adjacent an edge of the aperture; and a movable device for extending through an aperture in the cover. The movable device carries a panel attached to the movable device by a plurality of leaf springs. The assembly is configured such that when the movable device is moved toward the retracted position, the panel abuts the stop, thereby forming a surface substantially flush with an outer aerodynamic surface of the cover surrounding the aperture. The panel is displaced from the movable device by elastic deformation of at least some of the leaf springs.

    本发明涉及飞行器组件、飞行器机翼及操作飞行器组件的方法。飞行器组件具有:覆盖件,该覆盖件具有外部空气动力学表面和孔口,该孔口具有与孔口的边缘相邻的止挡部;以及可移动装置,该可移动装置用于伸出穿过覆盖件中的孔口。可移动装置承载通过多个板簧附接至可移动装置的面板。组件构造成使得当可移动装置朝向缩回位置移动时,面板抵靠止挡部,从而形成与覆盖件的围绕孔口的外部空气动力学表面基本上齐平的表面。面板通过板簧中的至少一些板簧的弹性变形而从可移动装置移位。


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    Title :

    Aircraft assembly, aircraft wing and method of operating aircraft assembly


    Additional title:

    飞行器组件、飞行器机翼及操作飞行器组件的方法


    Contributors:

    Publication date :

    2024-07-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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