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US 2026/0291315 A1Published application
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, a rotatable shaft and a winding support assembly. The winding support assembly is coupled to the rotatable shaft. The winding support assembly includes a first winding support disc and a retaining ring. The first winding support disc is axially spaced from the rotor core and has an axially inward facing first side defining a first surface and an axially outward facing second side defining a second surface. The retaining ring circumscribes the first winding support disc.
Claims17
A rotor assembly comprising:
- a rotatable shaft having a rotational axis;
- a rotor core rotatably coupled to the rotatable shaft and defining at least one rotor post;
- 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 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;
- and
- 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.
7 more elements
Dependencies are inferred from the claim text.