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US07131612B2 Nacelle inlet lip anti-icing with engine oil 有权
机舱入口唇线防油与发动机油

Nacelle inlet lip anti-icing with engine oil
摘要:
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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