An actuator is provided for an aircraft engine and includes a tubular base layer and a visco-elastic layer adhesively disposed on the tubular base layer.


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    Title :

    Actuator with vibration attenuation using visco elastic materials



    Publication date :

    2020-09-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / 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 | 2019

    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