Thermal management system for a gas turbine engine
AssigneeHamilton Sundstrand Corporation
InventorsEric Alexander, Gordon Jewess, Patrick Lydon, Tammy Lane
Life of this patent
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Abstract
A thermal management system for a gas turbine engine includes a cooling airflow which enters through an air filter portion of a forward cover for filtration of particulate which may result in FOD to a rotational system of the engine. Filtered cooling airflow flows along a rotor shaft over and through a forward bearing, over and through a permanent magnet generator, then over and through an aft bearing to provide thermal management. Commensurate therewith, the cooling airflow atomizes and communicates a lubricant to the bearings. From the aft bearing, the cooling airflow merges with a primary airflow path from an intake which generally surrounds the forward cover.
Claims15
A thermal management system for a gas turbine engine comprising:
- a forward cover having a filter portion along an axis of rotation of a gas turbine engine;
- a rotor shaft along said axis of rotation;
- a forward rotor shaft bearing which rotationally supports said rotor shaft;
- an aft rotor shaft bearing which rotationally supports said rotor shaft, said forward rotor shaft bearing and said aft rotor shaft bearing in communication with a cooling airflow from said filter portion;
- and
- a forward housing defined about said axis of rotation, said forward housing defining a lubrication passage directed toward said forward rotor bearing, said forward cover mounted to said forward housing.
A thermal management system for a gas turbine engine comprising:
- a forward cover having a filter portion along an axis of rotation of a gas turbine engine;
- a rotor shaft along said axis of rotation;
- a forward rotor shaft bearing which rotationally supports said rotor shaft;
- an aft rotor shaft bearing which rotationally supports said rotor shaft, said forward rotor shaft bearing and said aft rotor shaft bearing in communication with a cooling airflow from said filter portion;
- and
- a permanent magnet generator (PMG) mounted to said rotor shaft, said PMG mounted between said forward rotor shaft bearing and said aft rotor shaft bearing.
A gas turbine engine comprising:
- a rotor shaft defined along an axis of rotation;
- a compressor wheel mounted to said rotor shaft;
- at least one rotor shaft bearing which supports said rotor shaft;
- a forward cover having a filter portion adjacent said rotor shaft;
- a forward housing which defines a forward housing inner support and an air intake to communicate airflow toward said compressor wheel, said forward cover mounted to said forward housing such that cooling airflow through said filter portion is communicated through said forward housing inner support toward said at least one rotor shaft bearing, said forward housing defines at least one lubricant passage directed toward said at least one rotor shaft bearing such that said lubricant passage is in communication with said cooling airflow.
A method of thermal management for a gas turbine engine comprising the steps of:
- (1) communicating a cooling airflow through a filter portion along an axis of rotation of a rotor shaft having a compressor wheel, the cooling airflow in communication with at least one rotor bearing which supports the rotor shaft;
- (2) merging the cooling airflow into a primary airflow path downstream of the at least one bearing, the primary airflow path in communication with the compressor wheel;
- and
- (3) communicating the cooling airflow past a lubricant passage to at least partially atomize a lubricant therefrom such that atomized lubricant is received onto the at least one bearing.
A gas turbine engine comprising:
- a rotor shaft defined along an axis of rotation;
- a compressor wheel mounted to said rotor shaft;
- a forward housing which defines a forward housing inner support and an air intake to communicate a primary airflow toward said compressor wheel;
- and
- a forward cover having a filter portion forward of said rotor shaft and radially inward of said air intake, said forward cover mounted to said forward housing inner support such that a cooling airflow is communicated through said filter portion and into said forward housing inner support;
- a forward rotor shaft bearing forward of said compressor wheel to rotationally support said rotor shaft;
- an aft rotor shaft bearing forward of said compressor wheel and aft of said forward rotor shaft bearing to rotationally support said rotor shaft, said forward rotor shaft bearing and said aft rotor shaft bearing in communication with the cooling airflow, the cooling airflow communicated to merge with the primary airflow from the air intake upstream of said compressor wheel to provide a combined airflow toward the compressor wheel.
Dependencies are inferred from the claim text.