The invention provides an actuator device (20) for a wing assembly of an aircraft, the wing assembly and the aircraft to improve aerodynamic performance of the aircraft (10) and reduce resistance and weight. In such a device, a high lift device support (22) that supports a high lift device (24), such as a flap, and guides the movement of the high lift device is axially aligned with a controlled actuator assembly (46) that controls one or more control surfaces (40). In this way, a single support cowl (30) is sufficient to cover both the track member (26) and the controlled actuator assembly (46), thereby allowing resistance and weight reduction.

    本发明提出了一种用于飞行器的机翼组件的致动器装置(20)、机翼组件及飞行器,以改善飞行器(10)的空气动力学性能并且减小阻力和重量。在这种装置中,对高升力装置(24)比如襟翼进行支承并且对该高升力装置的运动进行引导的高升力装置支承件(22)与控制一个或更多个控制表面(40)的控制式致动器组件(46)轴向对准。这样,单个支承件整流罩(30)足以覆盖轨道构件(26)和控制式致动器组件(46)两者,由此允许阻力和重量减小。


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    Titel :

    Actuator device for wing assembly of aircraft, wing assembly and aircraft


    Weitere Titelangaben:

    用于飞行器的机翼组件的致动器装置、机翼组件及飞行器


    Beteiligte:
    ANDREANI LUCI (Autor:in) / LORENZ FLORIAN (Autor:in)

    Erscheinungsdatum :

    01.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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