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

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Hatch, Hatch, author.
Contributor:
Gent, Roger
Moser, Richard
Conference Name:
SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures (2015-06-22 : Prague, Czech Republic)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2015
Summary:
AbstractLow 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
Notes:
Vendor supplied data
Publisher Number:
2015-01-2142
Access Restriction:
Restricted for use by site license

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