Rotor assembly having bonded lamination stack

• US 6,772,503 B1
• Filed: 08/22/2000
• Issued: 08/10/2004
• Est. Priority Date: 08/22/2000
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Fathimulla, Ayub, Meacham, Walter Lee, Menon, M. N.
• Primary Examiner(s): Rosenbaum, Irene Cuda
• Assistant Examiner(s): Kenny, Stephen
• Application Number:
  US09/643,970
• Time in Patent Office: 1,449 Days
• Field of Search: 295/96, 295/97, 295/98, 296/09, 297/32, 297/38, 310/51, 310/254, 310/261, 310/154, 310/156, 310/214, 310/216, 310/42
• US Class Current: 29/598
• CPC Class Codes: H02K 1/24 Rotor cores with salient poles ; Variable reluctance rotors
• CPC Class Codes: H02K 15/02 of stator or rotor bodies
• CPC Class Codes: Y10T 29/49009 Dynamoelectric machine
• CPC Class Codes: Y10T 29/49012 Rotor
• CPC Class Codes: Y10T 29/49078 Laminated

Abstract

A rotor assembly includes a stack of laminations that are bonded together by a dielectric bonding agent. The laminations and the dielectric bonding agent have matching coefficients of thermal expansion.

Claims

1. A method of fabricating a rotor assembly, comprising:

applying a dielectric bonding agent to surfaces of a plurality of laminations;

wherein the dielectric bonding agent and the laminations have substantially matching coefficients of thermal expansion;

stacking the plurality of laminations; and

applying a thermal cycle to said stack of laminations of sufficient temperature to cure said dielectric bonding agent such that the laminations maintain a bond in operating temperatures up to 1000 degrees Fahrenheit.

2. The method of claim 1, wherein the dielectric bonding agent is selected from a group consisting of metallic oxides, spin-on-glass and silicon nitride.

3. The method of claim 1, further comprising of applying a pressure load to the stacked laminations during the thermal cycle.

4. The method of claim 2, further comprising applying the dielectric bonding agent to end caps, stacking the end caps along with the laminations, and applying the pressure load to the end caps during the thermal cycle.

5. The method of claim 4, further comprising machining geometric forms into the lamination stack after the laminations have been bonded.

6. A method of fabricating a rotor assembly, comprising:

annealing a plurality of laminations;

applying a dielectric bonding agent to surfaces of each lamination of the plurality of laminations;

applying a dielectric bonding agent to the surfaces of end caps;

wherein the dielectric bonding agent and the laminations have substantially matching coefficients of thermal expansion;

stacking the plurality of laminations into a stack;

placing one end cap at each end of the stack;

applying pressure on both end caps to compress the stack;

heating the stack and the end caps to a temperature sufficient to cure the dielectric bonding agent;

such that the cured bonding agent is able to maintain the bond of the stack and of the end caps at operating temperatures up to 1000 degrees F.; and

removing the heating and pressure from the end caps and the stack.

7. The method of claim 6, wherein the dielectric bonding agent is selected from a group consisting of metallic oxides, spin-on-glass and silicon nitride.

8. The method of claim 6, wherein each lamination of the rotor assembly is one piece of metal.

9. The method of claim 8, wherein the surface of each end cap facing the stack is essentially flat.

10. The method of claim 8, wherein the one piece of metal is a soft magnetic material.

11. The method of claim 10, further comprising polishing the surfaces of each lamination prior to applying the dielectric bonding agent to the surfaces of each lamination.

12. The method of claim 11, further comprising annealing each lamination prior to applying the dielectric bonding agent to the surfaces of each lamination.

13. A method of fabricating a rotor assembly, comprising:

annealing each lamination of a plurality of laminations;

applying a dielectric bonding agent to the surfaces of each lamination of the plurality of laminations;

wherein the dielectric bonding agent and the laminations have approximately equal coefficients of thermal expansion;

stacking the laminations; and

applying a thermal cycle to the stacked laminations to cure the dielectric bonding agent;

wherein the temperature at which said thermal cycle is performed

provides a cured bond that can endure operating temperatures up to 1000 degrees Fahrenheit.

14. The method of claim 13, wherein the dielectric bonding agent is selected from a group consisting of metallic oxides, spin-on-glass and silicon nitride.

15. The method of claims 14, further comprising applying a pressure load to the stacked laminations during the thermal cycle.

16. The method of claim 15, further comprising:

applying the dielectric bonding agent to end caps;

stacking the end caps at each end of the stacked laminations; and

additionally applying the pressure load to the end caps during the thermal cycle.

17. The method of claim 16, further comprising removing excess bonding agent from the stacked laminations.