The invention provides a mechanical aircraft rudder surface structure clamping tool, comprising lateral groove type right and left clamping plates and L-shaped triangular ends. The L-shaped triangular ends are riveted with the upper end face and the lower end face of the left clamping plate and the right clamping plate; bolt holes are formed in the L-shaped triangular ends; the left clamping plate and the right clamping plate are fixed together by bolts back to back. The mechanical aircraft rudder surface structure clamping tool is convenient in operation. Firstly the left clamping plate and the right clamping plate are fixed and then inserted along a seam in use, so that a rudder surface is fixed, and is fixation is not firm, a small amount of gauze is inserted between the left clamping plate and the right clamping plate.


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    Titel :

    Mechanical aircraft rudder surface structure clamping tool


    Beteiligte:
    HUANG YACHAO (Autor:in) / DU XINGGANG (Autor:in) / WANG HONGFEI (Autor:in) / LI CHAOGUANG (Autor:in) / HAN CHANGJING (Autor:in) / WANG XUEQIANG (Autor:in) / LYU WANTAO (Autor:in) / WANG ZHEN (Autor:in) / YU LINGJING (Autor:in) / HU BOHAI (Autor:in)

    Erscheinungsdatum :

    09.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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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