The invention provides a helicopter tail output reducing flange. By optimal design in structure, the tail output reducing flange has functions of a tail rotor hub for mounting and fixing a tail blade, functions of the tail rotor hub in the prior art are realized through a flange plate of the tail output reducing flange and optimal design on an outer cover plate, system structure of the tail rotor hub is simplified, overall size of the hub system is reduced, overall weight of the hub system is reduced, and reliability of the system is improved.


    Access

    Download


    Export, share and cite



    Title :

    Helicopter tail output reducing flange


    Contributors:
    YANG XINYUAN (author) / LI LI (author)

    Publication date :

    2015-09-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Helicopter tail propeller

    LIU ZHIQIANG / DING WENQIANG / SHI QIANLIE et al. | European Patent Office | 2020

    Free access

    Helicopter tail speed reducer and helicopter

    YU WEIBO / HU QIANG / LIU JIANBIN et al. | European Patent Office | 2020

    Free access

    HELICOPTER TAIL ASSEMBLY

    KRAJTMAIR-SHTEK VOL FGANG / KHEBENSHPERGER MIKHAEHL | European Patent Office | 2016

    Free access

    A SYSTEMATIC APPROACH TO REDUCING HELICOPTER TAIL DRIVE SHAFT MAINTENANCE

    Sheldon, J. / Steele, J. / Sarlashkar, A. et al. | British Library Conference Proceedings | 2013


    Helicopter without tail rotor

    PENG ZUOJUN / PENG HAO | European Patent Office | 2020

    Free access