Variable-tilt helicopter rotor mast proposed to improve helicopter performance and reduce vibration, especially at upper end of forward-speed range of helicopters. Achieved by use of universal coupling in main rotor mast or by tilting entire engine-and-transmission platform. Performance, energy efficiency, and safety enhanced.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Variable-Tilt Helicopter Rotor Mast


    Contributors:

    Published in:

    Publication date :

    1995-11-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :



    lift measurement tilt rotor mast sell

    PARK SANG HUN | European Patent Office | 2025

    Free access

    Quad Tilt Rotor Aerodynamics in Helicopter Mode

    Gupta, V. / Baeder, J. D. / American Helicopter Society | British Library Conference Proceedings | 2005


    Creating a New Generation Helicopter - Tilt Rotor

    Urbach, A. / Soskoveca, K. / Sorokins, A. et al. | British Library Conference Proceedings | 2012


    Method for forming tilt-rotor-driven helicopter-rotor dual-purpose aircraft

    YANG QINGTAI / YANG JIANJUN | European Patent Office | 2021

    Free access