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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    Title :

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


    Additional title:

    Sae Technical Papers


    Contributors:
    Hatch, Colin (author) / Moser, Richard (author) / Gent, Roger (author)

    Conference:

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



    Publication date :

    2015-06-15




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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