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


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION


    Weitere Titelangaben:

    DISPOSITIF DE MONTAGE POUR L`ISOLATION DES VIBRATIONS DU ROULEAU DE COUPLE


    Beteiligte:

    Erscheinungsdatum :

    17.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION

    TOMES NATHAN / GAGNON-MARTIN DAVID | Europäisches Patentamt | 2023

    Freier Zugriff

    Mount arrangement for torque roll vibration isolation

    TOMES NATHAN / GAGNON-MARTIN DAVID | Europäisches Patentamt | 2022

    Freier Zugriff

    MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION

    TOMES NATHAN / GAGNON-MARTIN DAVID | Europäisches Patentamt | 2020

    Freier Zugriff

    Microgravity Vibration Isolation Mount

    Tryggvason, B. V. / Salcudean, S. E. / Stewart, W. Y. et al. | British Library Conference Proceedings | 1994


    VIBRATION ISOLATION MOUNT DEVICE

    IIDA SHIGERU | Europäisches Patentamt | 2015

    Freier Zugriff