FIELD: engines and pumps.
SUBSTANCE: heat transfer system for turbine engine, which includes annular casing with set of rack elements located in it and passing mainly radially, contains at least one main heat pipe and at least one auxiliary heat pipe. The main heat pipe is located at least partially inside one of rack elements. Auxiliary heat pipe is located outside the fan casing and is thermally connected at least on one side to heat pipe and to heat source; as a result, heat is transferred from heat source via auxiliary heat pipe to the main heat pipe and to the selected rack element.
EFFECT: invention allows simplifying heat transfer in order to prevent or eliminate ice formation, as well as using the working medium that is not flammable in heat pipes.
10 cl, 6 dwg
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