Helicopter ice protection design criteria was developed and technological shortcoming in meeting helicopter mission requirements is that of helicopter rotor blade ice protection. Airframe components are protected using existing technology while the rotor blade protected using the cyclic electrothermal deicing concept.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Overview of helicopter ice protection system developments


    Contributors:


    Publication date :

    1979-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    An Overview of Early European Developments in Helicopter Technology

    Leishman, J.G. | British Library Conference Proceedings | 2009


    Modern developments in helicopter

    Liptrot, R.N. | Engineering Index Backfile | 1931


    U.S. Army Helicopter Icing Developments

    Ward, Robert N. | SAE Technical Papers | 1982


    Overview of the helicopter industry

    ZUGSCHWERT, JOHN | AIAA | 1989


    Helicopter rotor tail rotor failure protection system and helicopter

    CHEN XI / GAO XUAN / FEI ZHONGYANG et al. | European Patent Office | 2023

    Free access