Granted Patent B2

US 12,646,990 · App. 18/538,344 · Granted Jun 2, 2026

Inventors: Balamurugan Sridharan (Bengaluru, IN); Anirban Chatterjee (Bengaluru, IN)

Assignee: GE Aviation Systems LLC

H02K3/24H02K1/26H02K1/32H02K3/48

Abstract

Claims (33)

1 . 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.

2 . The rotor assembly of claim 1 , wherein the fourth wall defines a set of apertures therethrough in fluid communication with the set of first channels and the first chamber.

3 . The rotor assembly of claim 2 , further comprising a retaining ring circumscribing the first winding support disc, the retaining ring having an annular first leg circumscribing and radially spaced from the fourth wall, wherein the annular first leg and the fourth wall cooperatively define a second chamber therebetween.

4 . The rotor assembly of claim 3 , wherein the set of apertures of the fourth wall are in fluid communication with the second chamber.

5 . The rotor assembly of claim 3 , wherein the retaining ring further includes an annular second leg extending radially inward from the annular first leg, the annular second leg coupled to the second surface.

6 . The rotor assembly of claim 5 , wherein the second surface defines an annular recess along a circumferential periphery of the second side, wherein the annular second leg is received in the annular recess.

7 . The rotor assembly of claim 6 , wherein the second surface and the annular second leg cooperatively define a continuous axially outward facing surface.

8 . The rotor assembly of claim 3 , further comprising a second winding support disc comprising a radially central portion and a radially outer portion, the radially central portion coupled to the rotatable shaft, and further coupled to the radially outer portion via a set of radially extending spokes, the radially outer portion overlying the set of rotor winding end turns and being circumscribed by the retaining ring.

9 . The rotor assembly of claim 8 , wherein the radially outer portion defines a set of radially extending second channels defined therethrough in fluid communication with the first chamber.

10 . The rotor assembly of claim 8 , wherein each respective spoke is disposed between a corresponding end turn of the set of rotor windings and the rotor core.

11 . The rotor assembly of claim 8 , wherein the radially outer portion is disposed in the second chamber.

12 . The rotor assembly of claim 1 , wherein the set of rotor winding end turns define end turn passages extending radially therethrough.

13 . 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.

14 . The method of claim 13 , wherein the second channel extends through the radially outer portion of the second winding support disc at an angle with respect to an axis of rotation of the rotor assembly.

15 . The method of claim 13 , further comprising delivering the fluid coolant flow by the second winding support disc axially outward toward the rotor winding end turns.

16 . The method of claim 13 , further comprising delivering the fluid coolant flow by the second winding support disc radially outward from the second winding support disc.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (38)