Centrifugal compressor assembly and method

Patent metadata

Field	Value
Publication number	US-9556875-B2
Application number	US-201414153882-A
Country	US
Kind code	B2
Filing date	Jan 13, 2014
Priority date	Feb 20, 2008
Publication date	Jan 31, 2017
Grant date	Jan 31, 2017

Abstract

A centrifugal compressor assembly for compressing refrigerant in a 250-ton capacity or larger chiller system comprising a motor, preferably a compact, high energy density motor or permanent magnet motor, for driving a shaft at a range of sustained operating speeds under the control of a variable speed drive. Another embodiment of the centrifugal compressor assembly comprises a mixed flow impeller and a vaneless diffuser sized such that a final stage compressor operates with an optimal specific speed range for targeted combinations of head and capacity, while a non-final stage compressor operates above the optimum specific speed of the final stage compressor. Another embodiment of the centrifugal compressor assembly comprises an integrated inlet flow conditioning assembly to condition flow of refrigerant into an impeller to achieve a target approximately constant angle swirl distribution with minimal guide vane turning.

First claim

We claim:

1. A compressor assembly for compressing a refrigerant in a chiller system comprising:
a. a centrifugal compressor having a 250-ton capacity or larger, said centrifugal compressor having a compressor housing with a compressor inlet for receiving the refrigerant and a compressor outlet for delivering the refrigerant;
b. a shaft;
c. an impeller in fluid communication with said compressor inlet and said compressor outlet, said impeller mounted to said shaft and being operable to compress refrigerant; and
d. a direct drive, variable speed, permanent magnet motor for directly driving the shafts; and
e. a variable speed drive configured to vary a speed of operation of the direct drive, variable speed, permanent magnet motor, wherein the speed of operation is expressed as N s =RPM*sqrt(CFM/60)/ΔH is 3/4 , where RPM is the revolutions per minute, CFM is the volume of fluid flow in cubic feet per minute, ΔH is is a change in isentropic head rise in British thermal units per pound (BTU/lb), and the speed of operation is selected to be in a range of about 95 to about 180.

2. The compressor assembly of claim 1 , wherein the refrigerant is R-123, R-134a, or R-22 in liquid, gas, or multiple phases.

3. The compressor assembly of claim 1 , wherein the refrigerant is an azeotrope, a zeotrope, or a mixture or blend thereof in liquid, gas, or multiple phases.

4. The compressor assembly of claim 1 , wherein the direct drive, variable speed, permanent magnet motor is a hermetic, direct drive, variable speed, permanent magnet motor.

5. The compressor assembly of claim 4 , wherein the direct drive, variable speed, permanent magnet motor has a range of sustained operating speeds within about 4,000 revolutions per minute to about 20,000 revolutions per minute for a R-134a refrigerant.

6. The compressor assembly of claim 4 , wherein the direct drive, variable speed, permanent magnet motor has a range of sustained operating speeds within about 4,000 revolutions per minute to about 8,600 revolutions per minute for a R-123 refrigerant.

7. The compressor assembly of claim 1 , wherein the direct drive, variable speed, permanent magnet motor includes high energy density magnetic materials of at least 20 Mega Gauss Oersted.

8. The compressor assembly of claim 1 , wherein the variable speed drive is a variable frequency drive configured to vary operation of the direct drive, variable speed, permanent magnet motor.

9. The compressor assembly of claim 1 , wherein an internal surface of the impeller is machined, cast, coated, finished, or a combination thereof to less than about 125 RMS.

10. The compressor assembly of claim 1 , wherein an external surface of the impeller is machined, cast, coated, finished, or a combination thereof to less than about 125 RMS.

11. The compressor assembly of claim 1 , wherein the impeller is a radial impeller.

Assignees

• Trane Int Inc
• Trane Int Inc

Inventors

• Haley Paul F
• Dorman Dennis R
• Hamm Jr Frederic Byron
• Foye David M
• Kwiatkowski James A
• James Rick T
• Janssen Randall L
• Plzak William J

Classifications

• F04D17/122 Primary

  the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors · CPC title

• F04D29/4213

  suction ports · CPC title

• F04D29/441

  especially adapted for elastic fluid pumps · CPC title

• F04D25/06 Primary

  the pump being electrically driven (F04D25/08 takes precedence) · CPC title

• F04D17/10

  for compressing or evacuating · CPC title