Claims
- 1. A rotor assembly for use in an electric machine, comprising:
an iron core having a plurality of spaced slots extending along an exterior surface area of said core; a plurality of extruded aluminum bars being configured to be axially inserted into said plurality of slots in said exterior surface area, said plurality of extruded aluminum bars being of a length wherein a portion of said aluminum bar extends outwardly from either end of said iron core when said bars are inserted into said slots; and a pair of extruded end rings positioned of either end of said iron core, each of said pair of end rings having an exterior configuration similar to said iron core wherein the placement of one of said pair of end rings adjacent to said iron core allows said portion of said aluminum bar to be received therein.
- 2. The rotor assembly as in claim 1, wherein said pair of extruded end rings each having a plurality of slot openings configured to align with the plurality of slots of said iron core.
- 3. The rotor assembly as in claim 2, where said pair of extruded end rings are cut from an extruded member, said extruded member having an outer configuration similar to the outer configuration of said iron core.
- 4. The rotor assembly as in claim 3, where said extruded member is aluminum.
- 5. The rotor assembly as in claim 4, where said pair of extruded end rings are formed to said plurality of aluminum bars.
- 6. The rotor assembly as in claim 4, where said pair of extruded end rings are welded to said plurality of aluminum bars.
- 7. The rotor assembly as in claim 6, wherein the welds are located at the outer ends of the end rings.
- 8. The rotor assembly as in claim 1, wherein said plurality of extruded bars are copper and said extruded member is copper.
- 9. The rotor assembly as in claim 1, wherein said bars have a circular cross section and said slots are configured into a circular channel for receipt of said bars.
- 10. A method of manufacturing a rotor assembly, comprising:
forming an iron core having a plurality of spaced slots extending through an outer surface area of said core; extruding a plurality of aluminum bars with an exterior configuration similar to the configuration of said plurality of spaced slots, said plurality of aluminum bars having a length greater than the length of said plurality of spaced slots; axially inserting said plurality of aluminum bars into said plurality of spaced slots; inserting a pair of extruded end rings onto a portion of said plurality of aluminum bars extending outwardly from said iron core; and securing said pair of extruded end rings to said plurality of aluminum bars.
- 11. The method as in claim 10, wherein said pair of extruded end rings each have a plurality of openings configured for receipt of said portion of said plurality of aluminum bars.
- 12. The method as in claim 11, wherein said end rings are secured to said plurality of aluminum bars by welding said plurality of aluminum bars to said end rings at the outer most surface of said end rings.
- 13. The method as in claim 12, wherein said welding is performed by a tungsten inert gas (TIG) welding process.
- 14. A method for manufacturing a plurality of end rings for use in rotor assembly, comprising:
extruding an aluminum ring of a first thickness, said aluminum end ring having an outer configuration similar to an outer configuration of a iron core of the rotor assembly; and cutting at least one end ring from said aluminum ring said at least one end ring having a thickness less than said first thickness.
- 15. The rotor assembly as in claim 3, where said extruded member is copper.
- 16. The method as in claim 11, wherein said end rings are secured to said plurality of aluminum bars by cold forming said plurality of aluminum bars to said end rings at the outer most surface of said end rings.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
[0001] The U.S. Government may have a license in this invention and the right in limited circumstances to require the patent owner to license to others on reasonable terms as provided for by the terms of Contract No. DE-FC08-00NV13673.