Rotor end caps and a method of cooling a high speed generator

• US 6,734,585 B2
• Filed: 11/16/2001
• Issued: 05/11/2004
• Est. Priority Date: 11/16/2001
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Lengel, James D., Doherty, Kieran P. J., McDowall, Gregor L., Tornquist, Gerald Eugene, Borden, Raymond Walter
• Primary Examiner(s): Mullins, Burton S.
• Assistant Examiner(s): ELKASSABGI, HEBA
• Application Number:
  US09/991,501
• Publication Number:
  US 20030094872A1
• Time in Patent Office: 907 Days
• Field of Search: 310/52, 310/58, 310/60.A, 310/89, 310/91, 310/61, 310/53, 310/64, 310/88
• US Class Current: 310/61
• CPC Class Codes: H02K 1/325 between salient poles
• CPC Class Codes: H02K 3/527 applicable to rotors only
• CPC Class Codes: Y10T 29/49011 Commutator or slip ring assembly
• CPC Class Codes: Y10T 29/49012 Rotor
• CPC Class Codes: Y10T 29/49359 Cooling apparatus making, e.g., air conditioner, refrigerator
• CPC Class Codes: Y10T 29/49732 by attaching repair preform, e.g., remaking, restoring, or patching
• CPC Class Codes: Y10T 29/49826 Assembling or joining

Abstract

An improved apparatus and method of having a pair of end caps on a rotor assembly of a multi-pole high-speed generator is provided for use with a turbine engine. The rotor assembly provides improved balancing and/or cooling during generator operation. The rotor assembly includes a plurality of poles and at least one support wedge positioned between each of the poles. The rotor assembly is mounted on a shaft. An annular flange of the end caps restrains the support wedges in the rotor assembly for improved balancing and maintaining concentricity. The end caps may also include a manifold for circulating a cooling medium through the shaft to and from the support wedges to cool the generator.

Claims

1. A multi-pole high speed generator comprising a stator and a rotor, comprising:

a shaft having an axial bore with at least one orifice at each of a first and second end thereof;

a rotor assembly mounted on the shaft, the rotor assembly including a rotor having a plurality of poles and at least one support wedge positioned between each of the poles, cash of the at least one support wedge having at least one supply port in each end open to at least one axial channel in the at least one support wedge; and

an end cap mounted on the rotor at opposite ends thereof, each of the end caps having means for restraining the at least one support wedge from radially outward movement and means extending from the at least one orifice at each of the first and second ends of the shaft for circulating a cooling medium between the shaft and the at least one support wedge to cool the rotor assembly during operation of the multi-pole high speed generator.

2. The multi-pole high speed generator of claim 1, wherein the end caps define an end wail portion circumferentially surrounded by an annular flange.

3. The multi-pole high speed generator of claim 2, wherein each of the end caps include an end cap bore that is centered in the cad wall portion.

4. The multi-pole high speed generator of claim 3, wherein the end cap bore and the annular flange are shrunk fit, respectively, around the shaft and over axial ends of the at least one support wedge, each cad cap scaling at least an end of the rotor and restraining the at least one support wedge on the rotor.

5. The multi-pole high speed generator of claim 1, wherein each of the end caps includes a plurality of radially circumferentially spaced openings around a peripheral raised edge of the cad caps to selectively receive weights therein to balance the rotor.

6. A multi-pole high speed generator, comprising:

a shaft having an axial bore with at least one orifice extending radially from the bore at each of a first and second end thereof;

a rotor mounted on the shaft, the rotor having a plurality of poles and at least one support wedge positioned between each of the poles, the at least one support wedge having at least one mid supply port end at least one outlet supply port open to at least one axial channel in the at least one support wedge;

a first end cap disposed over a first axial end of the at least one support wedge and having radial fluid flow galleries extending from the at least one orifice at the second end of the shaft through which fluid exits the shaft to the at least one inlet supply port in each of the at least one support wedge hind a second cad cap disposed over a second axial cad of the at least one support wedge and having radial fluid flow galleries extending from the at least one outlet supply port in the at least one support wedge to the at least one orifice at the that end of the shaft through which fluid enters the shaft before exiting the rotor.

7. An end cap for a multi-pole high speed generator having a rotor assembly with a plurality of poles and support wedges therebetween, the end cap comprising:

a central bore;

a circular end wall circumferentially surrounded by an annular flange; and

paired end cap openings in the end wall with each pair at 90°

angles to one another, each of the paired end can openings includes a cooling medium feed port between the openings in each pair of paired end can openings.

8. The end cap for a multi-pole high speed generator of claim 7, wherein the paired end cap openings are arranged circumferentially in the end wall.

9. The end cap for a multi-pole high speed generator of claim 7, wherein the paired end cap openings are arranged along a radial line in the end wall and at of the openings in each pair saves as a cooling medium feed port.

10. The end cap for a multi-pole high spend generator of claim 7, wherein the end cap includes a raised peripheral edge having a plurality of circumferentially spaced provided therein for selective insertion of weights to help balance the generator.

11. The end cap for a multi-pole high speed generator of claim 7, wherein the end cap further includes a manifold at a hub location formed on an interior portion of the end cap.

12. The cad cap for a multi-pole high speed generator of claim 7, wherein the central bore and the annular flange are dimensioned so as to be shrunk fit, respectively, around a shaft of a rotor of the motor assembly and over axial cads of the support wedges.

13. The end cap for a multi-pole high speed generator of claim 7, wherein the manifold includes an annulus and at least one radial cooling medium gallery extending therefrom to at least one supply port formed in the support wedges.