An engine mount device includes a housing; a carrier that is at least partially inside the housing, the carrier comprising a hole through at least a partial thickness of the carrier, the hole being configured to receive a trunnion pin; and at least one flexure connecting the carrier (140, 220) to the housing. The at least one flexure is configured to provide higher stiffness in one or more radial directions of the hole compared to a stiffness provided in an axial direction of the hole. The housing and/or the carrier comprise one or more snubbing surfaces configured to limit a deflection of the carrier relative to the housing.


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    Titel :

    FLEXURE ISOLATOR AND METHOD OF COMPLIANT ISOLATION


    Weitere Titelangaben:

    BIEGEISOLATOR UND VERFAHREN FÜR KONFORME ISOLIERUNG
    ISOLATEUR D'ÉLÉMENT DE FLEXION ET PROCÉDÉ D'ISOLATION COMPATIBLE


    Beteiligte:

    Erscheinungsdatum :

    09.06.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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