IP Library Granted Patent US 11,489,386
Granted Patent B2
US 11,489,386 · App. 16/718,360 · Granted Nov 1, 2022

Wet and dry cavity generator systems and methods of manufacturing the same

Inventors: Hao Huang (Troy, OH); James Mahle (Vandalia, OH); Xiaochuan Jia (Centerville, OH)
Assignee: GE Aviation Systems LLC
H02K1/325B33Y80/00B64D41/00H02K1/24H02K9/19H02K15/022H02K19/22H02K19/38B33Y10/00
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Quick Facts
Patent No.
US 11,489,386
App. No.
16/718,360
Granted
Nov 1, 2022
Kind
B2
Abstract

A method for manufacturing a main rotor for a generator is provided. The method includes printing at least part of a rotor shaft by a three-dimensional printing process. The step of printing at least part of the rotor shaft includes printing a plurality of closed outlets and a plurality of open outlets. A rotor core is printed by the three-dimensional printing process. The step of printing the rotor core includes printing a plurality of liquid coolant conduits that extend through the rotor core and fluidly connecting the plurality of liquid coolant conduits to the plurality of closed openings.

Claims (16)

1. A method for manufacturing a main rotor for a generator, the method comprising:

printing at least part of a rotor shaft by a three-dimensional printing process, wherein the step of printing at least part of the rotor shaft comprises printing a plurality of closed outlets and a plurality of open outlets; and

printing a rotor core by the three-dimensional printing process, wherein the step of printing the rotor core comprises printing a plurality of liquid coolant conduits that extend through the rotor core and fluidly connecting the plurality of liquid coolant conduits to the plurality of closed outlets.

2. The method of claim 1 , wherein the rotor core comprises a central portion and a plurality of rotor poles that extend radially outward from the central portion.

3. The method of claim 2 , wherein the plurality of liquid coolant conduits are printed in successive layers of the rotor core within the plurality of rotor poles.

4. The method of claim 3 , wherein the plurality of rotor poles each comprise a pole body that extends radially outward from the central portion and a pole shoe at an end of the pole body, wherein the plurality of liquid conduits is a first plurality of liquid coolant conduits, the rotor core comprising a second plurality of liquid coolant conduits printed in the successive layers within each pole body.

5. The method of claim 1 , wherein the open outlets are printed on the rotor shaft at a location outside of the rotor core.

6. The method of claim 1 further comprising selecting one of a combination wet and dry cavity configuration three-dimensional computer model, a wet cavity configuration three-dimensional computer model or a dry cavity configuration three-dimensional computer model.

7. The method of claim 1 comprising:

selecting a dry cavity configuration three-dimensional computer model;

printing at least part of another rotor shaft by a three-dimensional printing process, wherein the step of printing at least part of the another rotor shaft comprises printing another plurality of closed outlets without printing at least some open outlets; and

printing another rotor core by the three-dimensional printing process, wherein the step of printing the another rotor core comprises printing another plurality of liquid coolant conduits that extend through the another rotor core and fluidly connecting the another plurality of liquid coolant conduits to the another plurality of closed outlets.

8. The method of claim 1 comprising:

selecting a dry cavity configuration three-dimensional computer model;

printing at least part of another rotor shaft by a three-dimensional printing process, wherein the step of printing at least part of the another rotor shaft comprises printing another plurality of open outlets without printing at least some closed outlets; and

printing another rotor core by the three-dimensional printing process, wherein the step of printing the another rotor core comprises printing another plurality of liquid coolant conduits that extend through the another rotor core and connect to a closed area of the rotor shaft.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 18, 2019
From: HUANG, HAO; MAHLE, JAMES; JIA, XIAOCHUAN
To: GE AVIATION SYSTEMS LLC
Reel/Frame 051315/0349 →
Continuity (1)
Related Publication 20210194305A1 · Jun 24, 2021
Cited By (1)
US 12,646,990