Resilient rotor assembly for interior permanent magnet motor

Patent metadata

Field	Value
Publication number	US-9472997-B2
Application number	US-201314036515-A
Country	US
Kind code	B2
Filing date	Sep 25, 2013
Priority date	May 25, 2010
Publication date	Oct 18, 2016
Grant date	Oct 18, 2016

Abstract

An electric motor comprises a shaft, an interior magnet rotor core comprising a central bore and a pair of opposing ends faces, and at least one resilient structure inserted within the central bore between the pair of opposing end faces. The at least one resilient component is inserted within the central bore between the pair of opposing end faces such that the at least one resilient component does not extend beyond one of the opposing end faces. The resilient component comprises an outer rigid structure inserted within the central bore, a resilient component inserted within the outer rigid structure, and an inner rigid structure inserted within the resilient component, wherein the shaft is inserted through the inner rigid structure.

First claim

What is claimed is:

1. An electric motor comprising:
a shaft;
an interior magnet rotor core comprising a central bore and a pair of opposing ends faces; and
at least one resilient structure inserted within said central bore between said pair of opposing end faces such that said at least one resilient component does not extend beyond at least one of said opposing end faces, said resilient structure comprising:
an outer rigid structure inserted within said central bore;
a resilient component inserted within said outer rigid structure; and
an inner rigid structure inserted within said resilient component, wherein said shaft is inserted through said inner rigid structure.

2. An electric motor according to claim 1 , wherein said outer rigid structure and said inner rigid structure are laminated structures having a plurality of laminated sheets.

3. An electric motor according to claim 1 , wherein said resilient structure is coupled between said shaft and said rotor core without welding said resilient structure to said shaft or said rotor core.

4. An electric motor according to claim 3 , wherein said outer rigid structure is configured to be coupled within said rotor core without welding said outer rigid structure to said rotor core and said inner rigid structure is configured to be coupled to said shaft without welding said inner rigid structure to said shaft.

5. An electric motor according to claim 1 , wherein said inner rigid structure and at least a corresponding portion of said shaft are keyed such that rotation of said rotor core facilitates rotation of said shaft.

6. An electric motor according to claim 1 , wherein at least a portion of said rotor core comprises said outer rigid structure.

7. An electric motor according to claim 1 , wherein said outer rigid structure comprises:
a flange extending around a perimeter of said outer rigid structure and over at least a portion of at least one of said opposing end faces, said flange comprising at least one hole therethrough; and
at least one attachment device configured for engagement with said flange and a corresponding bore within said rotor core.

8. An electric motor according to claim 1 , wherein said at least one resilient structure comprises a resilient structure proximate each of said opposing end faces.

9. An electric motor according to claim 1 , wherein at least one resilient structure comprises a resilient structure positioned substantially mid-way between said opposing end faces.

10. A rotor assembly comprising:
a pair of opposing end faces;
an interior magnet rotor core positioned between said pair of opposing end faces, said rotor core comprising a central rotor core bore therethrough;
a resilient component coupled to said rotor core within said central rotor core bore and between said pair of opposing end faces, said resilient component comprising a central resilient component bore therethrough; and
an inner rigid structure coupled to said resilient component within said central resilient component bore and between said pair of opposing end faces, said inner rigid structure comprising a central inner rigid structure bore therethrough configured to receive a shaft.

11. A rotor assembly according to claim 10 further comprising an outer rigid structure configured to be coupled to said rotor core within said central rotor core bore and comprising a central outer rigid structure bore therethrough that is configured to receive said resilient component.

12. A rotor assembly according to claim 11 , wherein said outer rigid structure is a substantially ring-shaped laminated structure having a plurality of laminated sheets.

13. A rotor assembly according to claim 11 , wherein said outer rigid structure is configured to be coupled within said central rotor core bore using at least one of rivets, nuts and bolts, keyways, and adhesives.

14. A rotor assembly according to claim 11 , wherein said outer rigid structure is configured to be coupled within said central rotor core bore without welding said outer rigid structure within said central rotor core bore.

15. A rotor assembly according to claim 10 , wherein said inner rigid structure is a substantially ring-shaped laminated structure having a plurality of laminated sheets.

16. A method of assembling an interior magnet rotor core motor, said method comprising:
providing an interior magnet rotor core including a central rotor core bore and a pair of opposing ends faces;
coupling an outer rigid structure within the central rotor core bore, the outer rigid structure including a central outer rigid structure bore;
coupling a resilient component within the central outer rigid structure bore, the resilient component including a central resilient component bore;
coupling an inner rigid structure within the central resilient component bore, the inner rigid structure including a central inner rigid structure bore; and
coupling a shaft within the central inner rigid structure bore, wherein the outer rigid structure, the resilient component, and the inner rigid structure are positioned between the pair of opposing end faces such that none of the outer rigid structure, the resilient component, and the inner rigid structure extend beyond at least one of the opposing end faces.

17. The method according to claim 16 , wherein coupling an outer rigid structure within the central rotor core bore comprises coupling the outer rigid structure within the central rotor core bore without welding the outer rigid structure to the rotor core.

18. The method according to claim 16 , wherein coupling an outer rigid structure within the central rotor core bore comprises coupling the outer rigid structure within the central rotor core bore using at least one of rivets, nuts and bolts, keyways, and adhesives.

19. The method according to claim 16 , wherein coupling an outer rigid structure within the central rotor core bore comprises coupling the outer rigid structure within the central rotor core bore using a press fit.

20. The method according to claim 16 , wherein coupling a resilient component within the central outer rigid structure bore comprises coupling the resilient component within the central outer rigid structure bore proximate each of the pair of opposing end faces.

Assignees

• Regal Beloit America Inc

Inventors

• Figgins Daniel S
• Kingrey Harold C
• Hall Jeffrey A
• Shelton Kerry B
• Brahmavar Subhash M
• Lytle Peter B
• Henry Michael W

Classifications

• H02K1/2786

  Outer rotors · CPC title

• H02K1/30 Primary

  using intermediate parts, e.g. spiders · CPC title

• H02K5/24 Primary

  specially adapted for suppression or reduction of noise or vibrations · CPC title

• H02K1/276

  Magnets embedded in the magnetic core, e.g. interior permanent magnets [IPM] · CPC title

• H02K15/03

  having permanent magnets · CPC title