The invention discloses a double-layer folded aircraft traction rod, which comprises a traction rod body a, wherein one end of the traction rod body a is connected with a traction device, a universal wheel is arranged at the lower side of one end of the traction rod body a, the traction rod body a is provided with a plurality of punched holes, a fixed wheel disk is arranged on the traction rod body a and fixed on an arc-shaped connection piece, the arc-shaped connection piece is fixed to the adjacent punched holes through bolts, a support bracket is arranged on the two ends of the upper end surface of the traction rod body a, a traction rod body b is fixed on the support bracket, a vortex screw lifting mechanism is arranged at the other end of the traction rod body a, a steering wheel is arranged on a manual crank of the vortex screw lifting mechanism, and a fast joint is arranged at the opening of the other end of the traction rod body a. The double-layer folded aircraft traction rod has a novel and unique structure, can be quickly and conveniently operated and can easily realize the purpose of height finely tuning, therefore, not only is labor saved, but also working efficiency is improved; meanwhile, professional maintaining person do not need to arrive at site, so that product cost is reduced.


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    Title :

    Double-layer folded aircraft traction rod


    Contributors:
    WANG YUANLIN (author) / SUN SHOULIN (author) / JIN QI (author) / LI SHILIN (author) / HE JIANDONG (author) / HU DEQIANG (author) / YUE WENJUAN (author)

    Publication date :

    2015-04-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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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