Nacelle inlet lip anti-icing with engine oil

Aeronautics and astronautics – Aircraft structure – Ice prevention

Reexamination Certificate

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Details

C244S13400A, C060S039093

Reexamination Certificate

active

07131612

ABSTRACT:
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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