Nacelle inlet lip anti-icing with engine oil

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

Patent

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Details

F01D 25/24 (2006.01) B64D 15/06 (2006.01) B64D 33/02 (2006.01) F01D 25/02 (2006.01) F01D 25/14 (2006.01) F01D 25/18 (2006.01) F02C 7/047 (2006.01) F02C 7/14 (2006.01)

Patent

CA 2471259

A nacelle for housing a gas turbine engine having a pressurized oil system for lubricating components thereof comprises an inlet lip defining a leading edge of the nacelle, the inlet lip having a conduit therein in fluid flow communication with the pressurized oil system of the gas turbine engine and defining an oil passage for circulation of pressurized engine oil therethrough. The conduit is in heat transfer communication with an outer surface of the inlet lip.

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