The present invention relates to a generator drive disconnect device, of a generator arranged to be driven by an aircraft engine. The disconnect device comprises: a drive transfer means (1) having a first, connected configuration, and a second, disconnected configuration; a disconnect biasing means (200), configured to bias the drive transfer means to the disconnected configuration; and a fluid cavity (300), configured such that provision of a pressurised fluid in the fluid cavity biases the drive transfer means to the connected configuration.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft engine generator disconnect drive


    Publication date :

    2018-03-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



    FINAL DRIVE DISCONNECT MECHANISM

    COMBS ROBERT F / BARKER CHARLES A / PRIEST JAMES | European Patent Office | 2016

    Free access

    Final drive disconnect mechanism

    COMBS ROBERT F / BARKER CHARLES A / PRIEST JAMES | European Patent Office | 2017

    Free access

    FINAL DRIVE DISCONNECT MECHANISM

    COMBS ROBERT F / BARKER CHARLES A / PRIEST JAMES | European Patent Office | 2015

    Free access

    FINAL DRIVE DISCONNECT MECHANISM

    COMBS ROBERT F / BARKER CHARLES A / PRIEST JAMES | European Patent Office | 2019

    Free access

    FINAL DRIVE DISCONNECT MECHANISM

    COMBS ROBERT F / BARKER CHARLES A / PRIEST JAMES | European Patent Office | 2018

    Free access