LAMINATED GENERATOR ROTOR STRUCTURE AND RELATED METHOD

• US 20110080068A1
• Filed: 10/06/2009
• Published: 04/07/2011
• Est. Priority Date: 10/06/2009
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Dawson, Richard Nils, Fogarty, James Michael, Wilson, Blake Weldon
• Application Number:
  US12/574,448
• Publication Number:
  US 20110080068A1
• Time in Patent Office: Days
• US Class Current: 310/216.114
• CPC Class Codes: H02K 1/26 Rotor cores with slots for windings
• CPC Class Codes: H02K 15/0006 Disassembling, repairing or modifying dynamo-electric machines repairing of cooling fluid boxes H02K15/0093
• CPC Class Codes: Y10T 29/49012 Rotor

Abstract

A laminated generator rotor structure and a related method for repairing a rotor using a laminated rotor structure are disclosed. In an embodiment, the rotor body includes a stack of laminated plates flanked by end flange members, and placed in compression by at least one stud member passing through the laminated stack and secured by at least one fastener.

Claims

1. A rotor comprising:

a rotor body including a lamination stack, the stack including a plurality of stacked laminations, each lamination having a first thickness, each lamination further having a plurality of radially extending slots arranged about a circumference of each of the plurality of laminations;

a first end flange member located on a first end of the lamination stack;

a second end flange member located on a second end of the lamination stack;

at least one stud member passing longitudinally through at least one hole in the lamination stack, the first end flange member, and the second end flange member,

a first fastener affixed to a first end of each of the at least one stud member;

a second fastener affixed to a second end of each of the at least one stud member;

the first fastener and the second fastener providing a compression to the laminated stack; and

a plurality of coils positioned within the plurality of slots.

2. The rotor of claim 1, further including:

a first spacer member located adjacent to the first end flange member;

a second spacer member located adjacent to the second end flange member;

a non-drive end shaft spindle affixed to the first spacer member; and

a drive-end shaft spindle affixed to the second spacer member,

wherein the at least one stud member passes through at least one hole in each of the first and second spacer members.

3. The rotor of claim 1, wherein the plurality of stacked laminations includes steel, and wherein the at least one stud member includes steel.

4. The rotor of claim 1, wherein the first thickness is between about 2 mm and about 25 mm.

5. The rotor of claim 1, wherein each of the plurality of laminations further includes an electrically insulating coating.

6. The rotor of claim 1, wherein the compression is at a pressure sufficient to provide a necessary bending stiffness to the rotor body and a necessary frictional capability to transmit a torque load from the rotor body to a drive shaft.

7. The rotor of claim 6, wherein the compression is at a pressure of between about 7,000 kPa about 50,000 kPa.

8. The rotor of claim 1, wherein the first end flange member and the second end flange member are shaped to provide nearly uniform pressure over an entirety of a cross section of the lamination stack.

9. The rotor of claim 1, further including a plurality of balancing laminations, each balancing lamination having a second thickness that is greater than the first thickness,

each balancing lamination further including a plurality of holes located on an outer circumference of the balancing lamination between the plurality of slots,

wherein the balancing laminations are located between the laminations having the first thickness in the lamination stack.

10. An electric machine comprising:

a rotor including;

a rotor body including a lamination stack, the stack including a plurality of stacked laminations, each lamination having a first thickness, each lamination further having a plurality of radially extending slots arranged about a circumference of each of the plurality of laminations;

a first end flange member located on a first end of the lamination stack,

a second end flange member located on a second end of the lamination stack,

at least one stud member passing longitudinally through at least one hole in the lamination stack, the first end flange member, and the second end flange member,

a first fastener affixed to a first end of each of the at least one stud member,

at least a second fastener affixed to a second end of each of the at least one stud member,

the first and second fasteners providing a compression to the laminated stack,

a plurality of coils positioned within the plurality of slots; and

a stator surrounding the rotor.

11. The electric machine of claim 10, further comprising:

a first spacer member located adjacent to the first end flange member;

a second spacer member located adjacent to the second end flange member;

a non-drive end shaft spindle affixed to the first spacer member; and

a drive-end shaft spindle affixed to the second spacer member,

wherein the at least one stud member passes through at least one hole in each of the first and second spacer members.

12. The electric machine of claim 10, wherein the plurality of stacked laminations includes steel, and wherein the at least one stud member includes steel.

13. The electric machine of claim 10, wherein the first thickness is between about 2 mm and about 25 mm.

14. The electric machine of claim 10, wherein each of the plurality of laminations further includes an electrically insulating coating.

15. The electric machine of claim 10, wherein the compression is at a pressure of between about 7,000 kPa about 50,000 kPa.

16. The electric machine of claim 10, wherein the first end flange member and second end flange member are shaped to provide nearly uniform pressure over an entirety of a cross section of the lamination stack.

17. The electric machine of claim 10, the rotor further including a plurality of balancing laminations, each balancing lamination having a second thickness that is greater than the first thickness,

each balancing lamination further including a plurality of holes located on an outer circumference of the balancing lamination between the plurality of slots,

wherein the balancing laminations are located between the laminations having the first thickness in the lamination stack.

18. A method comprising:

removing a first end portion of a rotor body;

affixing at least one stud member to a first end of the rotor body;

providing a plurality of laminations, each lamination having at least one hole in the lamination;

stacking the laminations on a first end of the rotor body, including passing the at least one stud member through the at least one hole in the plurality of laminations, the stacking further including forming a laminated stack having a length equal to a length of the first portion of the rotor;

placing an end flange member adjacent to the laminated stack, including passing the at least one stud member through at least one hole in the end flange member;

placing a spacer member adjacent to the end flange member, including passing the at least one stud member through at least one hole in the spacer member;

fastening the laminations, the end flange member, and the spacer member onto the at least one stud member with at least one fastener;

compressing the laminated stack, including tightening the at least one fastener.

19. The method of claim 18, wherein the affixing includes tapping at least one threaded hole in the first end of the rotor body, threading a first end of the at least one stud member, and threadably fastening the first end of the at least one stud member into the at least one hole.

20. The method of claim 18, the providing step further comprising providing a plurality of laminations having a thickness of between about 2 mm and about 25 mm.