The invention discloses a wing auxiliary butt joint control system which comprises a supporting module, an adjusting module, a driving module and wings. According to the wing auxiliary butt joint control system, by arranging the supporting module, the wings can be rapidly moved to the vicinity of a fuselage, so that the butt joint efficiency between the fuselage and the wings is improved; by arranging the adjusting module, the height change of the wings can be rapidly adjusted, the rough butt joint time is shortened, and the butt joint speed is increased; and by arranging the driving module, the heights of the two sides of the wings can be adjusted by adopting a single driving motor, so that the manufacturing cost of the device is reduced.

    本发明公开了一种机翼辅助对接控制系统,包括支撑模块、调节模块、驱动模块和机翼。本发明通过设置支撑模块,可以将机翼快速的移动到机身附近,从而提高机身和机翼之间的对接效率,通过设置调节模块,可以快速的调节机翼的高度变化,从而缩短粗略对接时的时间,进而提高了对接速度,通过设置驱动模块,采用单个驱动电机就可以调节机翼两侧的高度,从而降低本装置的制造成本。


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    Title :

    Wing auxiliary butt joint control system


    Additional title:

    一种机翼辅助对接控制系统


    Contributors:
    WANG SHUO (author)

    Publication date :

    2021-01-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B66F HOISTING, LIFTING, HAULING, OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD , Hub-, Verhol- oder Schubvorrichtungen, soweit nicht anderweitig vorgesehen, z.B. Vorrichtungen mit unmittelbarer Krafteinwirkung auf die Last / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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