A fixed-wing aircraft (1) comprising at least at least one vortex generator (6, 7, 8, 11) movable through an outer surface of the aircraft (1) between a retracted state and a fully extended state by at least one electric motor (12), the at least one electric motor (12) being specially adapted to actuate the at least one vortex generator (6, 7, 8, 11), and the aircraft comprises an electronic control unit (13) adapted to control the operation of the at least one electric motor (12) for the actuation of the at least one vortex generator (6, 7, 8, 11).

    一种固定翼飞行器(1),其至少包括至少一个涡流发生器(6、7、8、11),至少一个涡流发生器能够通过至少一个电动马达(12)在缩回状态与完全伸出状态之间移动穿过飞行器(1)的外表面,至少一个电动马达(12)专门适于致动至少一个涡流发生器(6、7、8、11),并且该飞行器包括电子控制单元(13),该电子控制单元适于控制至少一个电动马达(12)的操作以用于至少一个涡流发生器(6、7、8、11)的致动。


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    Titel :

    Aircraft with retractable vortex generator


    Weitere Titelangaben:

    具有可缩回式涡流发生器的飞行器


    Beteiligte:
    WINCEKOVIC DAVID (Autor:in) / PASQUIER FLORIAN (Autor:in) / SAVIN OLIVIER (Autor:in)

    Erscheinungsdatum :

    2023-09-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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