Heat pipe-based cooling apparatus and method for turbine engine

Details Heat pipe-based cooling apparatus and method for turbine engine Heat pipe-based cooling apparatus and method for turbine engine

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/06 (2006.01) F02C 7/14 (2006.01)

Patent

CA 2597454

A cooling apparatus (18) is provided for a turbine engine of the type including an cowling (14) with an outer surface (17) defined by a skin (15) exposed to an external air flow. The cooling apparatus (18) includes at least one heat pipe (20) disposed in the cowling (14). The heat pipe (20) has a first end (29) thermally coupled with the outer surface (17) of the casing and a second end (44) thermally coupled to a heat source, such that heat from the heat source can be transferred through the heat pipe (20) to the external air flow.

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