Motor rotor and air gap cooling

• US 9,657,747 B2
• Filed: 07/02/2013
• Issued: 05/23/2017
• Est. Priority Date: 09/06/2012
• Status: Active Grant

• Current Assignee: Carrier Corporation (Carrier Global Corporation)
• Original Assignee: Carrier Corporation (Carrier Global Corporation)
• Inventors: Sishtla, Vishnu M.
• Primary Examiner(s): NGUYEN, HANH N
• Application Number:
  US14/425,480
• Publication Number:
  US 20150204350A1
• Time in Patent Office: 1,421 Days
• Field of Search: 310 52, 310 54, 310 58, 310 64, 310 60 R, 310 61, 310 60 A
• CPC Class Codes: F04D 25/06 the pump being electrically driven F04D25/08 takes precedence
• CPC Class Codes: F04D 29/26 Rotors specially for elastic fluids
• CPC Class Codes: F04D 29/5806 Cooling the drive system
• CPC Class Codes: H02K 1/32 with channels or ducts for flow of cooling medium
• CPC Class Codes: H02K 9/193 with provision for replenishing the cooling medium; with means for preventing leakage of the cooling medium
• CPC Class Codes: H02K 9/197 in which the rotor or stator space is fluid-tight, e.g. to provide for different cooling media for rotor and stator

Abstract

A motor cooling system for a simply supported compressor includes a rotor shaft 24 having a first end 26 and a second end 28. The rotor shaft 24 includes an axial bore 60 and a plurality of shaft radial holes 64 extending from a first end of the axial bore 60, wherein a cooling medium is supplied to the axial bore 60. The cooling system further includes a rotor 22 coupled to the rotor shaft 24 and having a plurality of rotor axial holes 25 and a plurality of rotor radial holes 27. The plurality of rotor radial holes 27 extends from the plurality of rotor axial holes 25. A refrigerant dam 70 is arranged adjacent a first end of the rotor 22 and includes a plurality of dam axial holes 74 fluidly coupled to an interior cavity 72. The dam axial holes 74 align with the rotor axial holes 25 and the interior cavity 72 aligns with the shaft radial holes 64 to form a flow path between the rotor shaft 24 and the rotor 22.

Claims

1. A motor cooling system for a simply supported compressor system comprising:

a rotor shaft having a first end and a second end, the rotor shaft including an axial bore and a plurality of shaft radial holes extending from a first end of the axial bore, wherein a cooling medium is supplied to the axial bore;

a rotor including a plurality of rotor axial holes and a plurality of rotor radial holes extending from the plurality of rotor axial holes, wherein the rotor is coupled to the rotor shaft; and

a refrigerant dam arranged adjacent a first end of the rotor, the refrigerant dam including a plurality of dam axial holes fluidly coupled to an interior cavity, wherein the plurality of dam axial holes are aligned with the plurality of rotor axial holes, and the interior cavity is aligned with the plurality of shaft radial holes such that a flow path is formed between the rotor shaft and the rotor.

2. The motor cooling system according to claim 1, wherein the first end of the rotor shaft is supported by a first bearing and the second end of the rotor shaft is supported by a second bearing.

3. The motor cooling system according to claim 1, wherein the cooling medium is supplied to the axial bore from a conduit connecting a condenser and a cooler.

4. The motor cooling system according to claim 1, wherein the axial bore extends from a first end of the rotor shaft to adjacent the first end of the rotor.

5. The motor cooling system according to claim 1, wherein the plurality of rotor axial holes extend over a portion of a length of the rotor.

6. The motor cooling system according to claim 1, wherein the plurality of rotor axial holes extend over an entire length of the rotor.

7. A motor cooling system for a simply supported compressor system comprising:

a rotor including a plurality of rotor axial holes and a plurality of rotor radial holes extending form the plurality of rotor axial holes, the rotor being mounted to a rotor shaft having a first end and a second end;

a refrigerant dam arranged adjacent a first end of the rotor, the refrigerant dam including a plurality of dam axial holes fluidly coupled to an interior cavity, wherein the plurality of dam axial holes are aligned with the plurality of rotor axial holes; and

a spray bar including an elongated chute mounted adjacent a motor casing, wherein a cooling medium is supplied to the spray bar, and the elongated chute is arranged at an angle such that a free end of the elongated chute is adjacent an interface between the refrigerant dam and the rotor shaft.

8. The motor cooling system according to claim 7, wherein the first end of the rotor shaft is supported by a first bearing and the second end of the rotor shaft is supported by a second bearing.

9. The motor cooling system according to claim 7, wherein the cooling medium is supplied to the axial bore from a conduit connecting a condenser and a cooler.

10. The motor cooling system according to claim 7, further comprising a spacer, wherein the spacer is disposed between the spray bar and the motor casing.

11. The motor cooling system according to claim 10, wherein a labyrinth seal is positioned between the spacer and the first end of the rotor shaft.

12. The motor cooling system according to claim 7, wherein the interface between the refrigerant dam and the rotor shaft includes an opening of the interior cavity.

13. The motor cooling system according to claim 7, wherein the refrigerant dam is formed integrally with the first end of the rotor.

14. The motor cooling system according to claim 7, wherein the plurality of rotor axial holes extend over a portion of a length of the rotor.

15. The motor cooling system according to claim 7, wherein the plurality of rotor axial holes extend over an entire length of the rotor.