Stator assembly

Patent metadata

Field	Value
Publication number	US-11211836-B2
Application number	US-201916402879-A
Country	US
Kind code	B2
Filing date	May 3, 2019
Priority date	Jul 27, 2018
Publication date	Dec 28, 2021
Grant date	Dec 28, 2021

Abstract

A permanent magnet generator, includes a cylindrical rotor assembly having a set of circumferentially-spaced permanent magnets arranged at an outer radius of the rotor assembly, and spaced from one another by non-magnetic spacing element, and a stator assembly configured to coaxially receive the rotor assembly. The stator assembly includes a cylindrical stator core, a circumferentially spaced set of posts extending from the stator core and defining a set of stator slots between adjacent posts, and a set of conductive windings wound about the stator slots.

First claim

What is claimed is:

1. A stator assembly, comprising:
a cylindrical stator core;
a circumferentially spaced set of posts extending from the stator core and defining a set of stator slots between adjacent posts;
a first set of conductive windings wound about a first subset of stator slots in a first continuous circumferential portion of the stator core; and
a second set of conductive windings wound about a second subset of stator slots in a second continuous circumferential portion of the stator core, and wherein the second continuous circumferential portion is different from the first continuous circumferential portion;
wherein the first continuous circumferential portion of the stator core is circumferentially spaced from the second circumferential portion of the stator core by at least one adjacent slot, and the at least one adjacent slot is one of at least one empty adjacent slot or at least one adjacent slot having a non-conductive material within the slot.

2. The stator assembly of claim 1 wherein the stator assembly is a permanent magnet generator stator assembly.

3. The stator assembly of claim 2 wherein a power output of the first set of conductive windings is preselected to control a synchronous operation of a generator including the permanent magnet generator stator assembly.

4. The stator assembly of claim 3 wherein a power output of the second set of conductive windings is preselected to connect to a specific electrical load.

5. The stator assembly of claim 4 wherein the specific electrical load is at least one of an essential load, a flight critical load, a vehicle management system, a vehicle management system, or a flight computer.

6. The stator assembly of claim 2 wherein a power output of the first set of conductive windings is connected with an exciter stator of a generator including the permanent magnet generator stator assembly.

7. The stator assembly of claim 1 wherein the first set of conductive windings further includes at least two conductive windings wound about the first subset of stator slots in the first continuous circumferential portion and are configured to generate a corresponding at least two phases of power at a power output of the at least two conductive windings.

8. The stator assembly of claim 7 wherein the first set of conductive windings includes three conductive windings would about the first subset of stator slots and are configured to generate three phase power at respective power outputs of the three conductive windings.

9. The stator assembly of claim 1 wherein the first set of conductive windings and the second set of conductive windings are electrically isolated from one another.

10. The stator assembly of claim 1 wherein the first set of conductive windings and the second set of conductive windings are magnetically isolated from one another.

11. The stator assembly of claim 1 wherein the first set of conductive windings and the second set of conductive windings are mechanically isolated from one another.

12. The stator assembly of claim 1 wherein the first continuous circumferential portion extends about a larger circumferential portion of the stator core than the second continuous circumferential portion.

13. The stator assembly of claim 12 wherein the first set of conductive winding is configured to generate a larger power output than a power output of the second conductive winding.

14. A permanent magnet generator, comprising:
a cylindrical rotor assembly having a set of circumferentially-spaced permanent magnets arranged at an outer radius of the rotor assembly, and spaced from one another by non-magnetic spacing element; and
a stator assembly configured to coaxially receive the rotor assembly, and comprising:
a cylindrical stator core;
a circumferentially spaced set of posts extending from the stator core and defining a set of stator slots between adjacent posts;
a first set of conductive windings wound about a first subset of stator slots in a first continuous circumferential portion of the stator core; and
a second set of conductive windings wound about a second subset of stator slots in a second continuous circumferential portion of the stator core, and wherein the second continuous circumferential portion is different from the first continuous circumferential portion;

wherein the first continuous circumferential portion of the stator core is circumferentially spaced from the second circumferential portion of the stator core by at least one adjacent slot, and the at least one adjacent slot is one of at least one empty adjacent slot or at least one adjacent slot having a non-conductive material within the slot; and
whereby, the permanent magnet generator is configured to generate at least a first power output from the first set of conductive windings and a second power output from the second set of conductive windings when the rotor assembly is rotated relative to the stator assembly.

15. The permanent magnet generator of claim 14 wherein the first set of conductive windings further includes at least two conductive windings having a respective at least two power outputs, the at least two conductive windings wound about the first subset of stator slots in the first continuous circumferential portion and are configured to generate a corresponding at least two phases of power at the at least two power outputs when the rotor assembly is rotated relative to the stator assembly.

16. The permanent magnet generator of claim 14 wherein the first continuous circumferential portion extends about a larger circumferential portion of the stator core than the second continuous circumferential portion.

17. The permanent magnet generator of claim 16 wherein the first power output is larger than the second power output.

Assignees

• Ge Aviation Systems Llc

Inventors

• Huang Hao
• Jia Xiaochuan

Classifications

• H02K7/20

  Structural association with auxiliary dynamo-electric machines, e.g. with electric starter motors or exciters · CPC title

• H02K3/12

  arranged in slots · CPC title

• H02K16/04

  Machines with one rotor and two stators · CPC title

• H02K3/28 Primary

  Layout of windings or of connections between windings (windings for pole-changing H02K17/06, H02K17/14, H02K19/12, H02K19/32) · CPC title

• H02K3/493

  magnetic · CPC title