The invention discloses a high lift device for an aircraft and a high lift method. The high lift device (1) for an aircraft may comprise: a connecting bracket (10) for connecting the high lift device to a wing (2) of the aircraft; a front wing section (3) and a rear wing section (5) are fixed to the connecting bracket, the front wing section and the rear wing section are separated so that a gap can be formed between the front wing section and the rear wing section, the front wing section is provided with a first surface facing the gap, and the rear wing section is provided with a second surface facing the gap; a first cover plate (4) is positioned on the rear wing section; and an actuator (7) can control the first cover plate to extend into a gap between the front wing section and the rear wing section. The invention relates to the aircraft comprising the wing and a high lift method for the aircraft.

    公开了一种用于飞行器的增升装置和增升方法。用于飞行器的增升装置(1)可包括:连接支架(10),所述连接支架用于将所述增升装置连接至所述飞行器的机翼(2);固定在所述连接支架上的前翼段(3)和后翼段(5),所述前翼段与所述后翼段分离以在所述前翼段与所述后翼段之间形成缝道,所述前翼段具有朝向所述缝道的第一表面且所述后翼段具有朝向所述缝道的第二表面;位于所述后翼段上的第一盖板(4);以及作动器(7),所述作动器能控制所述第一盖板伸展至所述前翼段与所述后翼段之间的缝道中。还公开了包含机翼的飞行器和用于飞行器的增升方法。


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    Titel :

    High lift device for aircraft and high lift method


    Weitere Titelangaben:

    一种用于飞行器的增升装置和增升方法


    Beteiligte:
    NI ZAO (Autor:in) / YUAN JIANFENG (Autor:in) / QI YUDAN (Autor:in)

    Erscheinungsdatum :

    13.07.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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