IP Library Granted Patent US 11,271,456
Granted Patent B2
US 11,271,456 · App. 16/538,290 · Granted Mar 8, 2022

Method and assembly of an electric machine

Inventors: Hao Huang (Troy, OH); Xiaochuan Jia (Centerville, OH)
Assignee: GE Aviation Systems LLC
H02K9/197H02K1/32H02K3/24H02K7/1823H02K7/20H02K2213/03
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,271,456
App. No.
16/538,290
Granted
Mar 8, 2022
Kind
B2
Abstract

An electric machine assembly having a main machine stator core having at least one stator post, a set of stator windings wound about the at least one stator post and having a first end and an opposing second end, a coolant inlet housing defining an inlet passage, a coolant outlet housing defining an outlet passage, proximate to the coolant inlet housing, and wherein the coolant inlet passage and the coolant outlet passage define a coolant circuit configured to receive a supply of coolant to remove heat generated in the set of stator windings.

Claims (32)

1. An electric machine assembly comprising:

a housing;

a shaft configured to operably couple with a source of rotational force and rotate about a rotational axis and having a shaft cooling passage;

an arm carried by and extending radially outward from the shaft and having a first cooling passage different from the shaft cooling passage; and

an exciter rotor and a permanent magnet generator rotor carried by the arm.

2. The electric machine assembly of claim 1 wherein the shaft cooling passage is configured to receive a flow of cooling oil which can further be provided to the first cooling passage.

3. The electric machine assembly of claim 1 wherein the exciter rotor is positioned radially outward from the permanent magnet generator rotor.

4. The electric machine assembly of claim 1 , wherein at least one of a main machine stator, a main machine rotor, the rotatable shaft, or a housing is formed by additive manufacturing.

5. The electric machine assembly of claim 1 , further comprising an exciter stator carried by the housing and positioned proximate to the exciter rotor and a permanent magnet generator stator carried by the housing and positioned proximate to the permanent magnet generator rotor.

6. The electric machine assembly of claim 1 wherein the exciter rotor and the permanent magnet generator rotor at least partially overlap in the axial direction relative to the rotational axis.

7. The electric machine assembly of claim 1 wherein the electric machine generates at least 1 megawatt of electrical power.

8. The electric machine assembly of claim 1 wherein the electric machine includes a power density greater than 7 kiloWatt/kilogram.

9. The electric machine assembly of claim 1 wherein the electric machine is a dry cavity generator.

10. The electric machine assembly of claim 1 further comprising a contained liquid cooling system including a set of cooling passages for liquid coolant to flow through.

11. The electric machine assembly of claim 10 further comprising a main machine rotor carried by the shaft and having at least one rotor pole and at least one second cooling passage located proximate to the at least one rotor pole.

12. The electric machine assembly of claim 10 further comprising a set of stator windings carried by the housing and having a third cooling passage extending through the set of stator windings.

13. The electric machine assembly of claim 10 wherein the liquid coolant is oil.

14. A method of operating an electric machine, comprising:

rotating a rotatable shaft about a rotational axis, the shaft carrying an arm extending radially outward from the shaft, an exciter rotor, and a permanent magnet generator rotor; and

supplying liquid coolant from a rotatable shaft cooling passage to a first contained cooling passage extending through the arm to extract heat from the arm.

15. The method of claim 14 further comprising supplying liquid coolant to a second contained cooling passage extending through at least one set of stator windings mounted proximate to the rotatable shaft to extract heat from the at least one set of stator windings.

16. A gas turbine engine comprising:

an accessory gearbox coupled to a turbine shaft of the gas turbine engine; and

an electric machine assembly mounted to the accessory gearbox, the electric machine assembly comprising:

a housing;

a shaft configured to operably couple with a source of rotational force of the accessory gearbox and rotate about a rotational axis and having a shaft cooling passage;

an arm carried by and extending radially outward from the shaft and having a first cooling passage different from the shaft cooling passage; and

an exciter rotor and a permanent magnet generator rotor carried by the arm.

17. The gas turbine engine of claim 16 wherein the exciter rotor is positioned radially outward from the permanent magnet generator rotor.

18. The gas turbine engine of claim 16 , wherein at least one of a main machine stator, a main machine rotor, the rotatable shaft, or a housing is formed by additive manufacturing.

19. The gas turbine engine of claim 16 , further comprising an exciter stator carried by the housing and positioned proximate to the exciter rotor and a permanent magnet generator stator carried by the housing and positioned proximate to the permanent magnet generator rotor.

20. The gas turbine engine of claim 16 wherein the electric machine assembly is a dry cavity generator.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 12, 2019
From: HUANG, HAO; JIA, XIAOCHUAN
To: GE AVIATION SYSTEMS LLC
Reel/Frame 050027/0853 →
Continuity (2)
Continuation 15468879 · Mar 24, 2017
Related Publication 20200076273A1 · Mar 5, 2020
Cited By (1)
US 12,744,425