Methods and apparatus for operating gas turbine engines

Details Methods and apparatus for operating gas turbine engines Methods and apparatus for operating gas turbine engines

F - Mech Eng,Light,Heat,Weapons

01

D

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

Patent

CA 2432841

A method for operating an aircraft engine (10) facilitates preventing ice accumulation on the aircraft engine. The method comprises coupling a semi- permeable membrane (66) to the engine adjacent an outer surface (68) of the engine, coupling a fluid reservoir (62) to the aircraft engine in flow communication with the semi-permeable membrane, and supplying fluid from the fluid reservoir to the semi- permeable membrane to facilitate preventing ice accumulation on the aircraft engine outer surface.

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