A control assembly (100) and an aircraft (200) include a bearing board (11), a central board (12), a flight control board (13), a shock absorbing mechanism (14), and a communication connection cable (15). The flight control board (13) is mounted on the central board (12). The central board (12) is connected to the bearing board (11) via the shock absorbing mechanism (14). Therefore, the flight control board (13) and the central board (12) form a whole for shock absorption through the shock absorbing mechanism (14).


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    Title :

    CONTROL ASSEMBLY AND AIRCRAFT


    Additional title:

    STEUERUNGSANORDNUNG UND FLUGZEUG
    ENSEMBLE DE COMMANDE ET AÉRONEF


    Contributors:
    GAO SHIJING (author) / DING PENG (author) / WANG CHAORUI (author)

    Publication date :

    2021-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16F SPRINGS , Federn



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