Electric machine rotor

Patent metadata

Field	Value
Publication number	US-11196320-B2
Application number	US-201916690510-A
Country	US
Kind code	B2
Filing date	Nov 21, 2019
Priority date	Nov 21, 2019
Publication date	Dec 7, 2021
Grant date	Dec 7, 2021

Abstract

A rotor of an electric machine includes a main rotor body having a longitudinal axis, the main rotor body comprising: a hollow cylinder body with a first end and a second end; an integral end flange at the first end; a separate end flange disposed at the second end of the cylinder body; and laminations disposed on an outer surface of the cylinder body, the laminations comprising magnetic material.

First claim

What is claimed is:

1. A rotor of an electric machine, the rotor comprising:
a main rotor body having a longitudinal axis, the main rotor body comprising:
a hollow cylinder body with a first end and a second end;
an integral end flange at the first end;

a separate end flange disposed at the second end of the cylinder body; and
laminations disposed on an outer surface of the cylinder body, the laminations comprising magnetic material, wherein an outer diameter of the separate end flange is greater than an outer diameter of the second end of the cylinder, wherein the separate end flange is configured to be press-fit into the second end of the cylinder, and wherein at least a portion of the separate end flange extends longitudinally into the second end of the cylinder and under at least a portion of the magnetic material.

2. The rotor of claim 1 , further comprising:
a spacer disposed between the laminations and the separate end flange such that the laminations does not directly contact the separate end flange.

3. The rotor of claim 1 , wherein the main rotor body further comprises a retention flange on the first end, wherein a diameter of the retention flange is greater than the diameter of the second end of the cylinder.

4. The rotor of claim 3 , further comprising:
a first spacer disposed between the laminations and the separate end flange such that the laminations do not directly contact the separate end flange; and
a second spacer disposed between the laminations and the retention flange such that the laminations do not directly contact the retention flange.

5. The rotor of claim 1 , wherein the portion of the separate end flange that extends into the second end of the cylinder includes at least two longitudinally displaced segments having different outer diameters.

6. The rotor of claim 5 , wherein, when press-fit into the second end of the cylinder, an outer surface of a first segment of the at least two segments does not contact the cylinder and an outer surface of a second segment of the at least two segments does contact the cylinder.

7. The rotor of claim 6 , wherein the second segment extends further into the cylinder than the first segment.

8. The rotor of claim 1 , wherein the separate end flange is configured to be attached to the second end of the cylinder via a plurality of bolts.

9. The rotor of claim 8 , wherein the second end of the cylinder includes a plurality of receptacles configured to receive the plurality of bolts, and wherein an inner diameter of the second end of the cylinder is defined by the plurality of receptacles.

10. The rotor of claim 1 , wherein the integral end flange comprises a plurality of radially disposed slots.

11. The rotor of claim 1 , wherein the separate end flange comprises a hollow shaft disposed along the longitudinal axis, and wherein the integral end flange comprises a hollow shaft disposed along the longitudinal axis having a same outer diameter as the hollow shaft of the separate end flange.

12. The rotor of claim 1 , wherein the main rotor body is monolithic.

13. The rotor of claim 1 , further comprising a sleeve disposed radially over the laminations.

14. An airframe comprising:
a combustion engine;
an electric starter generator comprising a rotor that includes
a main rotor body having a longitudinal axis, the main rotor body comprising:
a hollow cylinder body with a first end and a second end;
an integral end flange at the first end;

a separate end flange disposed at the second end of the cylinder body; and
laminations disposed on an outer surface of the cylinder body, the laminations comprising magnetic material, wherein an outer diameter of the separate end flange is greater than an outer diameter of the second end of the cylinder, wherein the separate end flange is configured to be press-fit into the second end of the cylinder, and wherein at least a portion of the separate end flange extends longitudinally into the second end of the cylinder and under at least a portion of the magnetic material; and

a shaft connected to the separate end flange and the combustion engine.

15. The airframe of claim 14 , further comprising:
a spacer disposed between the laminations and the separate end flange such that the laminations does not directly contact the separate end flange.

16. The airframe of claim 14 , wherein the main rotor body further comprises a retention flange on the first end, wherein a diameter of the retention flange is greater than the diameter of the second end of the cylinder.

17. The airframe of claim 16 , further comprising:
a first spacer disposed between the laminations and the separate end flange such that the laminations do not directly contact the separate end flange; and
a second spacer disposed between the laminations and the retention flange such that the laminations do not directly contact the retention flange.

18. The airframe of claim 14 , wherein the portion of the separate end flange that extends into the second end of the cylinder includes at least two longitudinally displaced segments having different outer diameters.

19. The airframe of claim 18 , wherein, when press-fit into the second end of the cylinder, an outer surface of a first segment of the at least two segments does not contact the cylinder and an outer surface of a second segment of the at least two segments does contact the cylinder.

20. The airframe of claim 14 , wherein the separate end flange comprises a hollow shaft disposed along the longitudinal axis, and wherein the integral end flange comprises a hollow shaft disposed along the longitudinal axis having a same outer diameter as the hollow shaft of the separate end flange.

Assignees

• Rolls Royce Plc
• Rolls Royce Corp

Inventors

• Boden Mark
• Klemen Donald
• Terrell Jonathan
• Maners Brian

Classifications

• H02K7/003

  Couplings; Details of shafts (means for mounting rotors on shafts H02K1/28) · CPC title

• H02K1/30

  using intermediate parts, e.g. spiders · CPC title

• H02K5/225

  Terminal boxes or connection arrangements (specially adapted for submersible motors H02K5/132) · CPC title

• H02K1/2706

  Inner rotors · CPC title

• H02K5/15 Primary

  Mounting arrangements for bearing-shields or end plates · CPC title