A mounting arrangement for mounting a rotary engine (2) to an aircraft structure, wherein the engine has a three orthogonal axes comprising: a roll axis (5); a pitch axis (14); and a yaw axis (15). The mounting arrangement comprises: one-degree-of-freedom links with reaction axes passing through the roll axis (5). A separate roll constraint has a moment reaction about the roll axis (5) to decouple the torque roll mode from the other one-degree-of-freedom links.


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    Title :

    MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION


    Additional title:

    LAGERANORDNUNG ZUR PENDELSCHWINGUNGSISOLIERUNG
    AGENCEMENT DE MONTAGE POUR ISOLER LES VIBRATIONS D'UN ROULEAU DE COUPLE


    Contributors:

    Publication date :

    2023-11-15


    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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