The invention relates to a leading edge slat and a wing of an aircraft, the leading edge slat comprises an outer molded surface facing the outside of the wing and an inner molded surface opposite to the outer molded surface, the outer molded surface and the inner molded surface surround to form a cavity, the leading edge slat further comprises at least one movable plate, the movable plates are arranged on a fixed plate of the inner molded surface through pivots, and the movable plates are arranged on the fixed plate. The movable plate is arranged on the inner profile and has a closed position in which the movable plate is flush with the fixed plate of the inner profile and an open position in which the movable plate obliquely protrudes from the fixed plate of the inner profile around a pivot arranged on a first edge of the movable plate located on the front side; and the driving piece enables the movable plate to enter and keep the movable plate at the opening position. The wing comprises such a leading edge slat. The leading edge slat is such that when the movable plate is in the open position, the portion of the airflow flowing through the movable plate is directed to change the direction of flow, thereby delaying airflow separation.

    一种飞机的前缘缝翼及机翼,前缘缝翼包括朝向机翼外的外型面和与外型面相反的内型面,外型面和内型面围绕形成腔体,其中,前缘缝翼还包括:至少一个活动板,这些活动板通过枢轴设置在所述内型面的固定板上,并且相对内型面的固定板具有关闭位置与打开位置,在关闭位置中,活动板与内型面的固定板平齐,在打开位置中,活动板围绕枢轴从内型面的固定板倾斜地突起,枢轴设置在活动板的位于前侧的第一边缘;以及驱动件,驱动件使活动板进入并保持在所述打开位置。机翼包括这种前缘缝翼。这种前缘缝翼使得当活动板处于打开位置时,气流的流过活动板的部分被引导改变流动方向,从而延迟气流分离。


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    Titel :

    Leading edge slat and wing of aircraft


    Weitere Titelangaben:

    飞机的前缘缝翼及机翼


    Beteiligte:
    LI YAN (Autor:in) / CHEN MENGYING (Autor:in) / WANG BO (Autor:in)

    Erscheinungsdatum :

    29.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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