A mount mechanism used to mount an accessory gear box on an engine case in an aircraft engine, includes a pair of first brackets fastened to one of the engine case and the accessory gear box, the pair of first brackets being apart from each other in a circumferential direction of the engine case; a link extending in such a manner that the pair of first brackets are connected to each other via the link, both end portions of the link being coupled to the pair of first brackets by a pair of first pins, respectively; an annular anti-vibration element penetrated by each of the pair of first pins, the annular anti-vibration element being retained by at least one of each of the pair of first brackets and the end portion of the link; and a second bracket fastened to the other of the engine case and the accessory gear box, the second bracket box being coupled to the link by a second pin at a location between the pair of first brackets.


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    Titel :

    MOUNT MECHANISM FOR ACCESSORY GEARBOX


    Weitere Titelangaben:

    MONTAGEMECHANISMUS FÜR HILFSGETRIEBE
    MÉCANISME DE MONTAGE POUR BOÎTIER D'ENTRAÎNEMENT DES ACCESSOIRES


    Beteiligte:
    YASUDA RYO (Autor:in) / SHIMIZU HIROHITO (Autor:in) / FUJII HIROSHI (Autor:in) / IMAI TAKUYA (Autor:in) / OOTSUJI HIROAKI (Autor:in) / AKAHORI HIROFUMI (Autor:in)

    Erscheinungsdatum :

    2020-02-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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