An alternating-current servo electric cylinder driving device of a military aircraft missile loading truck comprises a frame. A hoisting device is fixed on the frame and comprises an alternating-current servo electric cylinder, the tail of the alternating-current servo electric cylinder is hinged to the frame by a pin shaft, the alternating-current servo electric cylinder is hinged to the parallelogram hoisting device hinted to the frame, the parallelogram hoisting device is connected with a direction adjusting and jacking device, the alternating-current servo electric cylinder coordinates with a planetary reducer driving ball screw pair to output linear motion by four alternating-current servo motors, the parallelogram hoisting device adopts a parallelogram mechanism, the direction adjusting and jacking device controls four motion degrees of freedom including jacking, rotating, front-back adjustment and left-right adjustment by the four alternating-current servo motors, and the four degrees of freedom are not interfered and can synchronously act. Servo control is accurate and stable and high in reliability. The alternating-current servo electric cylinder driving device is high in energy resource utilization rate and pollution free.


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    Titel :

    Alternating-current servo electric cylinder driving device of military aircraft missile loading truck


    Beteiligte:
    ZHAO SHENGDUN (Autor:in) / LI XUE (Autor:in) / FAN SHUQIN (Autor:in) / LI JINGXIANG (Autor:in) / CAI HOUYONG (Autor:in) / JING FEI (Autor:in)

    Erscheinungsdatum :

    2015-07-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / 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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