The present invention relates to an aerodynamic system for an aircraft and an aircraft, the aerodynamic system comprising a support structure and an aerodynamic component movably coupled to the support structure via a first coupling unit and a second coupling unit, the aerodynamic component is movable relative to the support structure. The first coupling unit and the second coupling unit may transfer a load from the aerodynamic component to a support structure. The system further includes an auxiliary coupling unit coupled between the aerodynamic component and the support structure and configured to switch from a decoupled state in which a load transfer via the at least one auxiliary coupling unit is blocked to a coupled state, and in which the at least one auxiliary coupling unit is coupled to the support structure. In the coupled state, a load transfer via the at least one auxiliary coupling unit is enabled.

    本发明涉及一种用于飞行器的空气动力学系统及飞行器,该空气动力学系统包括支撑结构和空气动力学部件,该空气动力学部件经由第一联接单元和第二联接单元可移动地联接至该支撑结构,使得该空气动力学部件可以相对于该支撑结构移动。该第一联接单元和第二联接单元可以将来自该空气动力学部件的载荷传递至支撑结构。该系统进一步包括辅助联接单元,该辅助联接单元联接在该空气动力学部件与该支撑结构之间、并且被配置为从脱联接状态切换成联接状态,其中,在该脱联接状态下,经由该至少一个辅助联接单元进行的载荷传递被阻止,并且其中,在该联接状态下,经由该至少一个辅助联接单元进行的载荷传递被启用。


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    Title :

    Aerodynamic system for aircraft and aircraft


    Additional title:

    用于飞行器的空气动力学系统及飞行器


    Contributors:
    HENKE MARC (author)

    Publication date :

    2024-12-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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