Low power ice protection systems are an important research area that is highlighted in the EU Clean Sky programme.In this paper an icing wind tunnel test of a full-scale wing incorporating both an electro-thermal and a hybrid electro-thermal electro-mechanical system is described. A description of a software tool to analyse both systems as full 3D models is also given. Preliminary comparisons of test data and prediction are shown both for the electro-thermal system and the hybrid system.Initial comparisons show a reasonable correlation in the main with recommendations for a structure tear-down to identify exact internal transducer locations. Recommendations are also made with regard to undertaking tests to determine a more consistent set of mechanical failure properties of ice. Future work in the development of the tool is also discussed.


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    Titel :

    Initial Results from a Hybrid Electro-Thermal Electro-Mechanical Simulation Tool (HETEMS)


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Hatch, Colin (Autor:in) / Moser, Richard (Autor:in) / Gent, Roger (Autor:in)

    Kongress:

    SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures ; 2015



    Erscheinungsdatum :

    15.06.2015




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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