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US 12,646,990 B2Granted
Rotor assembly and method of cooling
AssigneeGE Aviation Systems LLC
InventorsBalamurugan Sridharan, Anirban Chatterjee
Life of this patent
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Abstract
A rotor assembly includes a rotor core having a rotatable shaft and defining at least one rotor post, a winding wound around the post that defines an end turn, and a winding support assembly including a winding support assembly coupled to the rotatable shaft. The end turn defines a set of channels therethrough and is disposed in a first chamber defined by the winding support assembly.
Claims16
A rotor assembly comprising:
- a rotatable shaft having a rotational axis and defining a coolant conduit in fluid communication with a source of coolant;
- a rotor core rotatably coupled to the rotatable shaft and defining at least one rotor post;
- a set of rotor windings wound around the rotor post and defining a corresponding set of rotor winding end turns;
- and
- a winding support assembly fixed to the rotatable shaft, the winding support assembly including:
- a first winding support disc axially spaced from the rotor core, having an axially inward facing first side defining a first surface, and an axially outward facing second side defining a second surface,
- the first side including an annular first wall having a radially inward facing third surface defining a bore sized to receive the rotatable shaft therethrough, and a radially outward facing fourth surface opposingly spaced from the third surface, the annular first wall being rotatably coupled to the rotatable shaft along the third surface,
- the first side further including a second wall and a third wall radially extending from the fourth surface and, axially extending from the first surface, and circumferentially spaced from each other,
- a fourth wall extending between the second wall and the third wall and radially opposingly spaced from the fourth surface;
- wherein the second wall, the third wall, the fourth wall, the first surface, and the fourth surface cooperatively define a first chamber therebetween;
- and
- wherein the set of rotor winding end turns is received in the first chamber;
- wherein the annular first wall defines a set of first channels extending radially therethrough from the third surface to the fourth surface in fluid communication with the coolant conduit;
- and
- wherein the third surface defines a groove thereon surrounding the rotatable shaft, the groove in fluid communication with the set of first channels.
12 more elements
A method of cooling a set of rotor winding end turns supported by a first winding support disc rotatably coupled to a rotor assembly, the method comprising:
- delivering a fluid coolant flow to the first winding support disc;
- delivering the fluid coolant flow through first channels defined through the first winding support disc and to a first chamber at least partially defined by the first winding support disc;
- delivering the fluid coolant flow radially outward through end turn passages defined between adjacent rotor winding end turns disposed in the first chamber;
- and
- delivering the fluid coolant flow from the first chamber to a second chamber at least partially defined by the first winding support disc;
- and
- delivering the fluid coolant flow to a radially outer portion of a second winding support disc at least partially disposed in the second chamber by redirecting the fluid coolant flow through a second channel defined through the radially outer portion of the second winding support disc in an axially inward direction.
4 more elements
Dependencies are inferred from the claim text.