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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    Title :

    FLEXURE ISOLATOR AND METHOD OF COMPLIANT ISOLATION


    Additional title:

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


    Contributors:

    Publication date :

    2021-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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