Non-metallic structural rotor enclosure

• US 6,495,942 B1
• Filed: 01/26/2000
• Issued: 12/17/2002
• Est. Priority Date: 01/26/2000
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Wang, Yu, Kaminski, Christopher A., Keck, Richard J.
• Primary Examiner(s): Ramirez, Nestor
• Assistant Examiner(s): Perez, Guillermo
• Application Number:
  US09/491,504
• Time in Patent Office: 1,056 Days
• Field of Search: 310/89, 310/262, 310/85, 310/261, 310/45, 310/211, 310/264, 310/271, 310/214
• US Class Current: 310/262
• CPC Class Codes: H02K 1/24 Rotor cores with salient poles ; Variable reluctance rotors
• CPC Class Codes: H02K 1/32 with channels or ducts for flow of cooling medium

Abstract

A non-metallic structural enclosure for a generator rotor replaces conventional containment components including rotor wedges, rotor teeth and retaining rings. The enclosure includes a non-metallic tube formed of a plurality of spaced rings or of a continuous tube including ventilation holes or slots. The simplified rotor assembly serves to restrain the winding against centrifugal forces with a more highly optimized use of space and materials. The arrangement allows more space for copper and ventilation, thereby benefiting both efficiency and the performance of the machine. The use of individual rings has the additional benefit of providing restraint against centrifugal forces without reducing the effectiveness of cross slots in the rotor body from correcting peripheral dissymmetries in rotor stiffness. The rings also provide openings for ventilation without introducing stress concentrations in the enclosure.

Claims

1. An enclosure for a rotor in a generator including the rotor, rotor windings and a stator and without rotor wedges, rotor teeth and retaining rings, the enclosure comprising a non-metallic tube that is sized to entirely contain the rotor windings.

2. An enclosure for a rotor according to claim 1, wherein the non-metallic tube is formed of a plurality of rings.

3. An enclosure for a rotor according to claim 2, wherein the rings are spaced at predetermined intervals.

4. An enclosure for a rotor according to claim 3, wherein the rings are spaced axially such that cross slots in the rotor lie between the rings.

5. A rotor according to claim 4, wherein the cross slots located between rings provide corrections to dissymmetry in rotor stiffness around a periphery of the rotor.

6. A rotor according to claim 3, wherein the spaces between adjacent rings provide discharge openings for winding ventilation without introducing stress concentrations in the enclosure.

7. An enclosure for a rotor according to claim 1, wherein the non-metallic tube is formed of a low density composite material.

8. An enclosure for a rotor according to claim 7, wherein the low density composite material is a carbon fiber—

glass fiber epoxy composite.

9. An enclosure for a rotor according to claim 1, wherein the non-metallic tube is formed of a continuous tube, and wherein a plurality of ventilation holes are formed in the continuous tube, the ventilation holes providing winding ventilation away from the rotor.

10. A rotor in a generator comprising:

a magnetic core having at least two poles;

a plurality of winding assemblies, one for each pole; and

an enclosure entirely housing and retaining the core and the winding assemblies without rotor wedges, rotor teeth and retaining rings, wherein the enclosure comprises a non-metallic tube.

11. A rotor according to claim 10, wherein the non-metallic tube is formed of a plurality of rings.

12. A rotor according to claim 11, wherein the rings are spaced at predetermined intervals.

13. A rotor according to claim 10, wherein the non-metallic tube is formed of a low density composite material.

14. A rotor according to claim 13, wherein the low density composite material is a carbon fiber—

glass fiber epoxy composite.

15. A rotor according to claim 10, wherein the non-metallic tube is formed of a continuous tube, and wherein a plurality of ventilation holes are formed in the continuous tube, the ventilation holes providing winding ventilation away from the rotor.