An embodiment device (202) includes a clamp body (208) having a clamp opening (302), an extension opening (606) and a traverse block (312) having an internally threaded portion, a reaction plate (204) having a recess (406) in a first face at a first side of the reaction plate (204) and one or more pins (408) disposed in the recess (406) extending away from the first face, and further having an extension (402) extending along a long axis of the reaction plate (204) through the extension opening (606), and bearing blocks (308; 310) disposed on a second side of the reaction plate (204) opposite the first side, where the traverse block (312) is disposed between the bearing blocks (308; 310). An actuator (206) is aligned parallel to the long axis of the reaction plate (204) and extending through each of the bearing blocks (308; 310) and through the traverse block (312), and the actuator (206) has an eternally threaded portion engaged with the internally threaded portion of the clamp body (208).


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    Title :

    METHOD FOR REMOVING MAIN ROTOR BLADES FROM MAIN ROTOR HUB YOKE


    Additional title:

    VORRICHTUNG UND VERFAHREN ZUR ENTFERNUNG DER HAUPTROTORBLÄTTER AUS EINER HAUPTROTORNABENGABEL
    APPAREIL ET PROCÉDÉ PERMETTANT DE RETIRER DES PALES DE ROTOR PRINCIPAL DE LA CULASSE DE MOYEU DE ROTOR PRINCIPAL


    Contributors:

    Publication date :

    2020-04-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B25B TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING, OR HOLDING , Werkzeuge oder Werkbankvorrichtungen zum Befestigen, Verbinden, Lösen oder Halten, soweit nicht anderweitig vorgesehen / 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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