The invention relates to a wing component for an aircraft and the aircraft. The wing component includes: a leading edge portion and a trailing edge portion, the trailing edge portion being pivotally mounted to the leading edge portion about a pivot axis; an actuator unit configured to move the trailing edge portion relative to the leading edge portion; and a damper arrangement configured for damping uncontrolled movement between the leading edge portion and the trailing edge portion. The object of providing a wing component comprising a trailing edge high lift assembly with a more efficient, fault tolerant and space-saving damper device is achieved in that the trailing edge portion comprises a first component portion and a second component portion arranged to abut one another in the span-wise direction and configured to pivot individually about a pivot axis, the damper device includes a damping element coupled between the first component portion and the second component portion for damping relative movement of the first component portion and the second component portion.

    本发明涉及一种用于飞行器的机翼部件和飞行器。该机翼部件包括:前缘部分和后缘部分,该后缘部分以能够绕枢转轴线枢转的方式安装至前缘部分;致动器单元,该致动器单元构造成用于使后缘部分相对于前缘部分移动;以及阻尼器装置,该阻尼器装置构造成用于对前缘部分与后缘部分之间的不受控的运动进行阻尼。对于提供包括具有更有效、容错和节省空间的阻尼器装置的后缘高升力组件的机翼部件的目的的实现方式在于,后缘部分包括布置成在翼展方向上彼此紧靠并且构造成单独地绕枢转轴线枢转的第一部件部分和第二部件部分,阻尼器装置包括联接在第一部件部分与第二部件部分之间的用以对第一部件部分和第二部件部分的相对运动进行阻尼的阻尼元件。


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    Titel :

    Wing component for aircraft and aircraft


    Weitere Titelangaben:

    用于飞行器的机翼部件和飞行器


    Beteiligte:
    SCHLIPF BERNHARD (Autor:in) / KRAY DENNIS (Autor:in)

    Erscheinungsdatum :

    2024-03-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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