Method of improving compressor bearing reliability

Patent metadata

Field	Value
Publication number	US-10487833-B2
Application number	US-201415104681-A
Country	US
Kind code	B2
Filing date	Oct 16, 2014
Priority date	Dec 18, 2013
Publication date	Nov 26, 2019
Grant date	Nov 26, 2019

Abstract

A compressor assembly includes a housing assembly and a first rotor and second rotor arranged within the housing assembly. The first rotor is supported for rotation by a first inlet bearing adjacent an inlet end of the housing assembly and by a first discharge bearing adjacent a discharge end of the housing assembly. The second rotor is supported for rotation by a second inlet bearing adjacent the inlet end of the housing assembly and by a second discharge bearing adjacent the discharge end of the housing assembly. A first lubricant flow path supplies lubricant to at least two of the first discharge bearing, the first inlet bearing, the second discharge bearing, and the second inlet bearing sequentially.

First claim

The invention claimed is:

1. A compressor assembly, comprising:
a housing assembly;
a first rotor arranged within the housing assembly, the first rotor being supported for rotation by a first inlet bearing adjacent an inlet end of the housing assembly and by a first discharge bearing adjacent a discharge end of the housing assembly;
a second rotor arranged within the housing assembly, the second rotor being supported for rotation by a second inlet bearing adjacent the inlet end of the housing assembly and by a second discharge bearing adjacent the discharge end of the housing assembly; and
a first lubricant flow path configured to supply lubricant from a lubricant reservoir to both the first discharge bearing and the first inlet bearing sequentially; and
a second lubricant flow path configured to supply lubricant from the lubricant reservoir to at least one of the second discharge bearing and the second inlet bearing.

2. The compressor assembly according to claim 1 , where each of the first discharge bearing, the first inlet bearing, the second discharge bearing and the second inlet bearing is arranged downstream from a pressure-reducing orifice.

3. The compressor assembly according to claim 1 , wherein the lubricant supplied to the first lubricant flow path includes a mixture of lubricant and refrigerant, wherein a gaseous portion of the refrigerant in the mixture provided to the first inlet bearing is greater than the gaseous portion of the refrigerant in the mixture provided to the first discharge bearing.

4. The compressor assembly according to claim 3 , wherein a viscosity of the lubricant provided to the first inlet bearing is greater than a viscosity of the lubricant provided to the first discharge bearing.

5. The compressor assembly according to claim 1 , wherein the second lubricant flow path supplies lubricant to the second discharge bearing and the second inlet bearing sequentially.

6. The compressor assembly according to claim 5 , wherein the lubricant supplied to the second lubricant flow path includes a mixture of lubricant and refrigerant, wherein a gaseous portion of the refrigerant in the mixture provided to the second inlet bearing is greater than the gaseous portion of the refrigerant in the mixture provided to the second discharge bearing.

7. The compressor assembly according to claim 6 , wherein a viscosity of the lubricant provided to the second inlet bearing is greater than a viscosity of the lubricant provided to the second discharge bearing.

8. A compressor assembly, comprising:
a housing assembly;
a first rotor arranged within the housing assembly, the first rotor being supported for rotation by a first inlet bearing adjacent an inlet end of the housing assembly and by a first discharge bearing adjacent a discharge end of the housing assembly;
a second rotor arranged within the housing assembly, the second rotor being supported for rotation by a second inlet bearing adjacent the inlet end of the housing assembly and by a second discharge bearing adjacent the discharge end of the housing assembly; and
a lubricant flow path configured to supply lubricant from a lubricant reservoir to each of the first discharge bearing, the first inlet bearing, the second discharge bearing and the second inlet bearing sequentially, wherein the lubricant flow path supplies lubricant to both the first discharge bearing and the second discharge bearing before supplying lubricant to either of the first inlet bearing and the second inlet bearing.

Assignees

• Carrier Corp

Inventors

• Shoulders Stephen L

Classifications

• F04C23/008

  Hermetic pumps · CPC title

• F04C2240/50

  Bearings · CPC title

• F04C18/16

  with helical teeth, e.g. chevron-shaped, screw type {(for non-parallel axes of movement F04C18/48)} · CPC title

• F04B39/0284

  Constructional details, e.g. reservoirs in the casing (swash-plate compressors F04B27/0878, F04B27/109) · CPC title

• F04C29/028 Primary

  Means for improving or restricting lubricant flow · CPC title