A separating mechanism comprises a motor and control element seat, a motor, a driving wheel, a supporting seat, a sliding pin, a connecting rod, a buffering spring, a parachute cord fixing ring, an end cover, a rotating shaft pin, a sliding pin bolt and a fixing screw. The sliding pin is mounted in a circular through hole slot of the supporting seat and can slide in the slot. The end part of the sliding pin is hinged with the connecting rod through the sliding pin bolt. The other end of the connecting rod is hinged with the driving wheel through the rotating shaft pin. The driving wheel is fixed on a motor shaft through a fastener. The supporting seat and the motor are fixed on the motor and control element seat. The end cover and the parachute cord fixing ring are connected with each other through a thread and fixed together with the motor and control element seat. The buffering spring is fixed on the bottom surface of the supporting seat.


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    Title :

    Parachute separating mechanism for small-sized throwing robot


    Contributors:
    GAO JUNYAO (author) / ZHAO JINGCHAO (author) / ZHANG WEIMIN (author) / HUANG QIANG (author) / LIU YI (author) / ZHAO FANGZHOU (author) / SHI XUANYANG (author) / LI YUE (author) / ZHANG LIANCUN (author) / LI XIN (author)

    Publication date :

    2015-10-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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