Laminated dynamoelectric machine rotor having cast conductors and radial coolant ducts and method of making same

• US 4,341,966 A
• Filed: 06/09/1980
• Issued: 07/27/1982
• Est. Priority Date: 06/09/1980
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Pangburn, William W.
• Primary Examiner(s): Duggan, Donovan F.
• Application Number:
  US06/157,576
• Time in Patent Office: 778 Days
• Field of Search: 310/61, 310/64, 310/65, 310/211
• US Class Current: 310/61
• CPC Class Codes: H02K 1/32 with channels or ducts for flow of cooling medium
• CPC Class Codes: H02K 17/16 having rotors with internally short-circuited windings, e.g. cage rotors

Abstract

A rotor comprising stacked laminations having conductor slots and axial passageways provided with closed-slot spacer assemblies that are stacked in groups between selected axially spaced rotor laminations to hold said laminations apart while sealing the conductor slots thereby to form radial cooling ducts through the laminations of the selected axially spaced groups and around the closed-slot spacer assemblies. According to the method of the invention, the spacer assemblies are secured in selected operating position by being staked to certain of the main rotor laminations, and a characteristic staking procedure is used to secure individual plates of each of the assemblies together.

Claims

1. In a laminated rotor having cast conductors in spaced axially-extending passageways adjacent the peripheral surface of the stacked rotor laminations and having radial coolant ducts extending between spaced groups of the rotor laminations, the improvement comprising;

(a) a plurality of laminated spacer assemblies, each comprising a plurality of metal plates, locking means for securing such plates to each other in stacked relationship, and wall means defining an aperture through each plate, the apertures in all of said plates of each spacer assembly being positioned in alignment to define a conductor passageway through the assembly, and

(b) mounting means fastening each of said spacer assemblies, respectively, to at least one rotor lamination of a respective juxtaposed group of rotor laminations with each spacer assembly conductor aperture aligned with a respective axially-extending passageway through the rotor laminations, thereby to define continuous axially-extending conductor passageways through the aligned rotor laminations and spacer assemblies, said continuous conductor passageways each being sealed from the radial coolant ducts by said wall means of the respective spacer assemblies.

2. An invention as defined in claim 1 wherein the metal plates forming said spacer assembly laminations are each about the same thickness as the thickness of one of the rotor laminations, and wherein each aperture through the respective spacer assembly plate members is approximately the same area and configuration in cross-section as the respective aligned passageways through the rotor.

3. An invention as defined in claim 1 wherein said locking means for securing the plates of the respective spacer assemblies to each other comprises inter-locking staked portions on adjacent plates of the spacer assemblies.

4. An invention as defined in claim 3 wherein each plate of said spacer assemblies includes two spaced staked positions that each comprises a depression in one side thereof and a boss on an opposite side thereof, said two staked portions of each plate being positioned on a line that generally parallels a longitudinal axis of the conductor aperture in said plate, and one of said staked portions of each plate being positioned adjacent the end of said plate farthest from the conductor aperture therein.

5. An invention as defined in claim 4 wherein said mounting means each comprises a fusion weld between said one rotor lamination and the spacer assembly plate closest thereto.

6. An invention as defined in claim 3 wherein each plate of each spacer assembly includes two spaced staked portions that each comprises a depression in one side thereof and a boss on an opposite side thereof, said bosses on all but one plate being nested in aligned depressions or apertures, respectively, in an adjacent plate.

7. An invention as defined in claim 6 wherein one lamination in each group of rotor laminations includes a plurality of pairs of additional spaced apertures each pair being, respectively, adjacent one of said conductor-receiving apertures therein, each of said apertures in the additional pairs of apertures being positioned to receive therein, respectively, one of the bosses on the closest plate of one of the plurality of respective adjacent spacer assemblies, thereby to fix said spacer assemblies in predetermined positions relative to said one rotor lamination.

8. An invention as defined in claim 7 wherein each said closest plate of each spacer assembly includes two additional spaced apertures arranged to receive therein, respectively, one of the bosses on the adjacent plate in the spacer assembly, thereby to fix the remaining plates in the spacer assembly in a predetermined position relative to said closest plate.

9. An invention as defined in claim 8 wherein said two additional spaced apertures in each of said closest plates are separated by a distance substantially equal to the distance between the two bosses on said closest plate.

10. An invention as defined in claim 9 wherein the two additional spaced apertures in each of said closest plates are substantially identical in configuration to the two depressions in the next adjacent plate on each spacer assembly.

11. An invention as defined in claim 8 wherein each said mounting means includes a fusion weld between said one lamination of each group of laminations and said closest plate of the respectively adjacent assemblies.

12. An invention as defined in claim 11 wherein said fusion weld is formed by a laser beam applied to the side of said one lamination of each group of laminations that is opposite to the side thereof on which said spacer assemblies are mounted.

13. An invention as defined in claim 8 wherein each spacer assembly includes in the plate thereof most remote from said one rotor lamination a pair of apertures that are spaced apart a distance substantially equal to the distance between the bosses on said closest plate of the spacer assembly to said one rotor lamination, each aperture in said most remote plate being at least as large in area as the area of one of the bosses on said closest plate.