Gas turbine engine oil buffering
A turbine engine, air flow technology, applied in gas turbine installations, engine components, engine functions, etc., can solve the problems of buffer air overheating, providing sufficient compartment pressurization, etc.
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[0026] This application describes a new pressurization and ventilation system for bearing compartments and shafts of gas turbine engines. In particular, the present application describes an assembly and method for providing damping and / or ventilation air to a bearing compartment and / or shaft of a gas turbine engine. The described gas turbine engine includes a dedicated centrifugal compressor that compresses discharge air from a low pressure compressor section and / or fan section of the gas turbine engine. Compressed air is delivered to the engine core to cushion the bearing compartment and / or vent one or more shafts. A centrifugal compressor compresses discharge air to a higher pressure more efficiently than a conventional axial compressor array because it avoids the kinetic energy losses and throttling losses experienced with a conventional axial compressor array at the compressor casing. By employing a centrifugal compressor, air is drawn from the fan section and / or low pres...
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