复合材料部件电加热防冰性能试验

doi:10.7527/S1000-6893.2013.0320

Abstract

Abstract:

An experiment of electro-thermal anti-icing on a composite assembly is presented. The experiment is run in a small open-circuit icing research tunnel based on a refrigerant system composed of a freon refrigerator and air turbines, and a spray system consisting of air/fluid nozzles. Temperature distribution is provided for different anti-icing methods by altering air speeds, icing conditions and electro-heating powers. The results show that anti-icing electro-heating power increases with air speed, and air temperature and the liquid water content have a coupled effect on the power needed. Temperature and its gradients in the assembly is in proportion to electro-heating power. Multi-zone heating methods lead to reasonable temperature distribution of the assembly under the same anti-icing thermal loads.

Key words: aircraft engines, icing wind tunnel test, electro-heating, anti-icing, composite

CLC Number:

V228.7⁺1

MA Hui, ZHANG Dalin, MENG Fanxin, CHEN Weijian. Experiment of Electro-thermal Anti-icing on a Composite Assembly[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(8): 1846-1853.

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Experiment of Electro-thermal Anti-icing on a Composite Assembly

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