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.


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    Titel :

    Overview of helicopter ice protection system developments


    Beteiligte:
    Adams, R. I. (Autor:in)


    Erscheinungsdatum :

    1979-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    An Overview of Early European Developments in Helicopter Technology

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    Modern developments in helicopter

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


    U.S. Army Helicopter Icing Developments

    Ward, Robert N. | SAE Technical Papers | 1982


    Helicopter rotor tail rotor failure protection system and helicopter

    CHEN XI / GAO XUAN / FEI ZHONGYANG et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Overview of the helicopter industry

    ZUGSCHWERT, JOHN | AIAA | 1989