An actuator (13) is provided for an aircraft engine and includes a tubular base layer (30) and a visco-elastic layer (40) adhesively disposed on the tubular base layer (30). An aircraft engine comprising an engine case (11), a cowl door (12) and such an actuator (13) is also provided.


    Access

    Download


    Export, share and cite



    Title :

    ACTUATOR WITH VIBRATION ATTENUATION USING VISCO ELASTIC MATERIALS


    Additional title:

    AKTUATOR MIT SCHWINGUNGSDÄMPFUNG UNTER VERWENDUNG VON VISKOELASTISCHEN MATERIALIEN
    ACTIONNEUR AVEC ATTÉNUATION DE VIBRATIONS UTILISANT DES MATÉRIAUX VISCO-ÉLASTIQUES



    Publication date :

    2019-04-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16F SPRINGS , Federn



    ACTUATOR WITH VIBRATION ATTENUATION USING VISCO ELASTIC MATERIALS

    VINJANAMPATI PAVAN KUMAR / JANAKIRAMAN RAJASEKARAN | European Patent Office | 2019

    Free access

    ACTUATOR WITH VIBRATION ATTENUATION USING VISCO ELASTIC MATERIALS

    VINJANAMPATI PAVAN KUMAR / JANAKIRAMAN RAJASEKARAN | European Patent Office | 2019

    Free access

    Actuator with vibration attenuation using visco elastic materials

    VINJANAMPATI PAVAN KUMAR / JANAKIRAMAN RAJASEKARAN | European Patent Office | 2020

    Free access

    Vibration of a visco-elastic spherical immiscible liquid system

    Bauer, Helmut F. / Eidel, Werner / Deutschland, Bundeswehr, Bundesrepublik | TIBKAT | 1986


    Dynamic Properties of the Visco-Elastic Actuator Designed as an Artificial Muscle

    Saito, M. / Tamura, Y. / Furusho, J. | British Library Online Contents | 1995