A de-icing system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a forward assembly and a rear assembly adjacent to the forward assembly. One of the forward assembly and the rear assembly is rotatable relative to the other to generate an amount of air friction between said forward and rear assemblies. A method of de-icing a gas turbine engine is also disclosed.
Gas turbine engine de-icing system
27.10.2020
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2021
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