A rotor blade assembly for a tiltrotor aircraft comprising a rotor blade pivotally connected to a yoke with dual concentric blade bolts having a common central axis providing a pivotal axis inboard of an outboard CF bearing and the yoke tip. In use, the compact folded arrangement of the rotor blades reduces folded aircraft dimensions in response to ever increasing restricted storage space parameters.


    Access

    Download


    Export, share and cite



    Title :

    OUTBOARD CENTRIFUGAL FORCE BEARING WITH INBOARD BLADE FOLD AXIS IN A FOLDING ROTOR BLADE ASSEMBLY


    Contributors:

    Publication date :

    2019-06-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Outboard centrifugal force bearing with inboard blade fold axis in a folding rotor blade assembly

    PAULSON JARED MARK / BALDWIN TYLER WAYNE / CRAVENER KYLE THOMAS | European Patent Office | 2020

    Free access

    Dual blade fold bolts and inboard centrifugal bearing in a folding rotor blade assembly

    PAULSON JARED MARK / BALDWIN TYLER WAYNE / CRAVENER KYLE THOMAS | European Patent Office | 2020

    Free access

    DUAL BLADE FOLD BOLTS AND INBOARD CENTRIFUGAL BEARING IN A FOLDING ROTOR BLADE ASSEMBLY

    PAULSON JARED MARK / BALDWIN TYLER WAYNE / CRAVENER KYLE THOMAS | European Patent Office | 2019

    Free access

    Inboard centrifugal force bearing attachment

    MARESH ANDREW / SCHANK TROY CYRIL / TZENG CHYAUSONG et al. | European Patent Office | 2021

    Free access

    INBOARD CENTRIFUGAL FORCE BEARING ATTACHMENT

    MARESH ANDREW / SCHANK TROY CYRIL / TZENG CHYAUSONG et al. | European Patent Office | 2019

    Free access