Methods and apparatus for operating gas turbine engines

F - Mech Eng,Light,Heat,Weapons – 01 – D

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F01D 25/02 (2006.01) F02C 7/047 (2006.01)

Patent

CA 2557066

A method for assembling a turbine engine (10) to facilitate preventing ice accumulation on the turbine engine during engine operation. The method includes coupling a manifold to the gas turbine engine such that the manifold (102) is coupled in thermal communication with a heat source, coupling a first heat pipe (100) to the manifold such that the first heat pipe partially circumscribes the gas turbine engine in a clockwise orientation, and coupling a second heat pipe to the manifold such that the second heat pipe partially circumscribes the gas turbine engine in a counter- clockwise orientation.

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