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

2015-01-2142

06/15/2015

Event
SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/2015-01-2142
Pages
7
Citation
Hatch, C., Gent, R., and Moser, R., "Initial Results from a Hybrid Electro-Thermal Electro-Mechanical Simulation Tool (HETEMS)," SAE Technical Paper 2015-01-2142, 2015, https://doi.org/10.4271/2015-01-2142.
Additional Details
Publisher
Published
Jun 15, 2015
Product Code
2015-01-2142
Content Type
Technical Paper
Language
English