In one embodiment, an apparatus comprises a particle damper for damping a component when the particle damper is attached to the component. The particle damper comprises a plurality of pockets configured to hold a plurality of particles, and the particle damper also comprises an attachment fitting for coupling the particle damper to the component.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT LOAD AND VIBRATION ATTENUATION


    Contributors:

    Publication date :

    2017-11-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



    Aircraft load and vibration attenuation

    SEIFERT MICHAEL S / HOWARD BRETT C / PARHAM JR THOMAS C et al. | European Patent Office | 2020

    Free access

    Anti-vibration load generating aircraft actuation system

    WELSH WILLIAM A / BASKIN BRYAN KENNETH / BUTLER CHRIS PAUL | European Patent Office | 2020

    Free access

    ANTI-VIBRATION LOAD GENERATING AIRCRAFT ACTUATION SYSTEM

    WELSH WILLIAM A / BASKIN BRYAN KENNETH / BUTLER CHRIS PAUL | European Patent Office | 2017

    Free access

    ANTI-VIBRATION LOAD GENERATING AIRCRAFT ACTUATION SYSTEM

    WELSH WILLIAM A / BASKIN BRYAN KENNETH / BUTLER CHRIS PAUL | European Patent Office | 2016

    Free access

    ANTI-VIBRATION LOAD GENERATING AIRCRAFT ACTUATION SYSTEM

    WELSH WILLIAM A / BASKIN BRYAN KENNETH / BUTLER CHRIS PAUL | European Patent Office | 2022

    Free access