Electric machine arc path protection

Patent metadata

Field	Value
Publication number	US-10951095-B2
Application number	US-201816051982-A
Country	US
Kind code	B2
Filing date	Aug 1, 2018
Priority date	Aug 1, 2018
Publication date	Mar 16, 2021
Grant date	Mar 16, 2021

Abstract

In one an exemplary aspect of the present disclosure, an engine includes a drive shaft; an electric machine including a stator assembly and a rotor assembly, the rotor assembly rotatable relative to the stator assembly; and an electrical break, the drive shaft coupled to the rotor assembly through the electrical break.

First claim

What is claimed is:

1. An engine defining an axial direction, the engine comprising:
a drive shaft;
an electric machine comprising a stator assembly and a rotor assembly, the rotor assembly rotatable relative to the stator assembly, the rotor assembly comprising a rotor shaft; and
an electrical break, the drive shaft coupled to the rotor shaft of the rotor assembly through the electrical break, wherein the drive shaft and the rotor shaft overlap along the axial direction, and wherein electrical break is positioned at least partially between the drive shaft and the rotor shaft.

2. The engine of claim 1 , wherein the electrical break is configured to transfer substantially all of a torque between the drive shaft and the rotor assembly of the electric machine.

3. The engine of claim 1 , wherein the engine is a turbine engine comprising a compressor and a turbine, wherein the drive shaft is coupled to at least one of the compressor or the turbine of the turbine engine.

4. The engine of claim 3 , wherein the turbine engine is at least one of a turbofan engine, a turboshaft engine, a turbojet engine, or a turboprop engine.

5. The engine of claim 3 , wherein the turbine engine is an auxiliary power unit.

6. The engine of claim 3 , wherein the turbine engine defines a core air flowpath, and wherein the electric machine is positioned inward of at least a portion of the core air flowpath along a radial direction.

7. The engine of claim 1 , wherein the engine is an aeronautical fan engine, wherein the aeronautical fan engine comprises a fan having a plurality of fan blades, and wherein the drive shaft is coupled to the plurality of fan blades for driving the plurality of fan blades.

8. The engine of claim 1 , wherein the electrical break is formed substantially completely of a non-electrically conductive material having an electrical resistivity greater than about 1×10 10 ρ (Ω·m).

9. The engine of claim 8 , wherein the non-electrically conductive material is a plastic material.

10. The engine of claim 1 , wherein the electric machine comprises a plurality of air bearings, and wherein the rotor assembly and the stator assembly are rotatably coupled using the plurality of air bearings.

11. The engine of claim 10 , wherein the rotor assembly and the stator assembly are rotatably coupled completely using the plurality of air bearings during operation of the engine, the plurality of air bearings including at least one radial air bearing and at least one thrust air bearing.

12. The engine of claim 1 , wherein the electric machine comprises a plurality of mechanical bearings, wherein the rotor assembly and the stator assembly are rotatably coupled using the plurality of mechanical bearings, and wherein each of the plurality of mechanical bearings comprise an electrical insulation.

13. The engine of claim 1 , further comprising:
a stationary member, wherein the stator assembly of the electric machine is coupled to the stationary member, and wherein the stationary member comprises an electrical isolation section.

14. The engine of claim 1 , wherein the engine is configured to generate at least about 250 horsepower during operation, and wherein the drive shaft is configured to transfer at least about 250 pound-feet of torque during operation.

15. The engine of claim 1 , wherein the engine is configured to generate at least about 2,000 horsepower during operation, and wherein the drive shaft is configured to transfer at least about 1,500 pound-feet of torque during operation.

16. A method for operating an engine defining an axial direction, the method comprising:
rotating a rotor assembly of an electric machine relative to a stator assembly of the electric machine with a drive shaft of the engine by transferring substantially all of a thrust between the rotor assembly and the drive through an electrical break;
wherein the drive shaft is coupled to a rotor shaft of the rotor assembly through the electrical break, wherein the drive shaft and the rotor shaft overlap along the axial direction, and wherein electrical break is positioned at least partially between the drive shaft and the rotor shaft.

17. The method of claim 16 , wherein rotating the rotor assembly relative to the stator assembly with the drive shaft by transferring substantially all of the thrust between the rotor assembly and the drive shaft through the electrical break comprises driving the rotor assembly with the drive shaft.

18. The engine of claim 1 , wherein the rotor shaft includes teeth extending along a radial direction of the engine, wherein the driveshaft includes teeth extending along a radial direction of the engine, and wherein the electrical break is positioned at least partially between the teeth of the driveshaft and the teeth of the rotor shaft along a circumferential direction of the engine.

19. The engine of claim 1 , wherein the electrical break extends between the rotor shaft and the driveshaft along a radial direction of the engine.

Assignees

• Gen Electric

Inventors

• Miller Brandon Wayne
• Niergarth Daniel Alan
• Kroger Christopher James
• Stevenson Christian Xavier

Classifications

• F05D2260/404

  through magnetic drive coupling · CPC title

• F02C7/32

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• F05D2220/76

  an electrical generator · CPC title

• F01D25/162

  Bearing supports · CPC title

• F02C6/00 Primary

  Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use · CPC title