Integrated connector for multi-stage compressor

Patent metadata

Field	Value
Publication number	US-11486618-B2
Application number	US-201916599982-A
Country	US
Kind code	B2
Filing date	Oct 11, 2019
Priority date	Oct 11, 2019
Publication date	Nov 1, 2022
Grant date	Nov 1, 2022

Abstract

This disclosure relates to a compressor having at least two compression stages. In particular, an exemplary compressor includes a first radial compression stage arranged along an axis, a second radial compression stage arranged along the axis, and a connector fluidly connecting an outlet of the first radial compression stage to an inlet of the second radial compression stage. The connector has a plurality of sections arranged about the axis. The compressor may be a refrigerant compressor used in a heating, ventilation, and air conditioning (HVAC) chiller system.

First claim

The invention claimed is:

1. A refrigerant compressor, comprising:
a first radial compression stage arranged along an axis;
a second radial compression stage arranged along the axis; and
a connector fluidly connecting an outlet of the first radial compression stage to an inlet of the second radial compression stage, the connector having a plurality of channels circumferentially spaced-apart from one another about the axis and configured such that fluid flowing within each of the plurality of channels flows from the outlet to the inlet in parallel to fluid flowing within others of the plurality of channels, wherein each channel includes a first radial portion adjacent the outlet, a second radial portion adjacent the inlet, and an axial portion extending between the first and second radial portions, wherein each of the plurality of channels includes a curved portion connecting the first radial portion and the axial portion, wherein each curved portion exhibits an increased height relative to a remainder of the respective channel.

2. The refrigerant compressor as recited in claim 1 , wherein the first and second radial compression stages are arranged within a housing, and the plurality of channels extend outside the housing.

3. The refrigerant compressor as recited in claim 2 , wherein the connector is integrated with an exterior of the housing.

4. The refrigerant compressor as recited in claim 1 , wherein the plurality of channels comprises three channels spaced 120° apart from one another about the axis.

5. The refrigerant compressor as recited in claim 1 , wherein the first and second compression stages are configured to compress a fluid, wherein the fluid is a refrigerant.

6. The refrigerant compressor as recited in claim 1 , wherein the first radial compression stage includes a first impeller arranged on a shaft and the second radial compression stage includes a second impeller arranged on the shaft.

7. The refrigerant compressor as recited in claim 1 , wherein fluid is configured to flow into the first radial compression stage in a first direction and the fluid is configured to flow into the inlet of the second radial compression stage in a second direction that is opposite the first direction.

8. The refrigerant compressor as recited in claim 1 , wherein the refrigerant compressor is used in a heating, ventilation, and air conditioning (HVAC) chiller system.

9. The refrigerant compressor as recited in claim 1 , wherein each channel exhibits an increased volume within the curved portion.

10. A refrigerant system comprising:
a main refrigerant loop including a compressor, a condenser, an evaporator, and an expansion device, wherein the compressor includes:
a first radial compression stage arranged along an axis;
a second radial compression stage arranged along the axis; and
a connector fluidly connecting an outlet of the first radial compression stage to an inlet of the second radial compression stage, the connector having a plurality of channels circumferentially spaced-apart from one another about the axis and configured such that fluid flowing within each of the plurality of channels flows from the outlet to the inlet in parallel to fluid flowing within others of the plurality of channels, wherein each of the plurality of channels includes a section exhibiting an increased volume relative to a remainder of the respective channel, wherein, within each section, a radially inner portion of a wall of each respective channel exhibits a concave contour when viewed from a radially outer perspective.

11. The refrigerant system of claim 10 , wherein fluid is configured to flow into the first radial compression stage in a first direction and the fluid is configured to flow into the inlet of the second radial compression stage in a second direction that is opposite the first direction.

12. The refrigerant system of claim 10 , wherein the first radial compression stage includes a first impeller arranged on a shaft and the second radial compression stage includes a second impeller arranged on the shaft.

13. The refrigerant system of claim 10 , wherein each channel includes a first radial portion adjacent the outlet, a second radial portion adjacent the inlet, and an axial portion extending between the first and second radial portions.

14. The refrigerant system of claim 13 , wherein the section provides a pocket in each channel between the outlet and the inlet.

15. The refrigerant system of claim 14 , wherein the pocket is arranged between the first radial portion and the axial portion.

16. The refrigerant system of claim 10 , wherein the first and second radial compression stages are arranged within a housing, and the plurality of channels extend outside the housing.

17. A refrigerant compressor, comprising:
a first radial compression stage arranged along an axis;
a second radial compression stage arranged along the axis; and
a connector fluidly connecting an outlet of the first radial compression stage to an inlet of the second radial compression stage, the connector having a plurality of sections arranged about the axis,
wherein each of the plurality of sections comprises a channel that communicates fluid from the outlet to the inlet,
wherein each channel includes a first radial portion adjacent the outlet, a second radial portion adjacent the inlet, and an axial portion extending between the first and second radial portions, and
wherein a pocket is formed in each channel between the outlet and the inlet.

18. The refrigerant compressor as recited in claim 17 , wherein the first radial portion is closer to the outlet than the second radial portion, and the second radial portion is closer to the inlet than the first radial portion.

19. The refrigerant compressor as recited in claim 17 , wherein each channel exhibits an increased volume within the pocket relative to areas of the channel adjacent the pocket.

20. The refrigerant compressor as recited in claim 17 , wherein each channel is arranged such that the respective pocket is arranged in a curved section between the first radial portion and the axial portion.

21. The refrigerant compressor as recited in claim 20 , wherein, within each curved section, a radially inner portion of a wall of each respective channel exhibits a concave contour when viewed from a radially outer perspective.

Assignees

• Danfoss As

Inventors

• Schaefer Arnold Martin
• Yan Jin
• Perez Alonso Misael

Classifications

• F04D17/122

  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

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title

• F25B1/10 Primary

  with multi-stage compression (with cascade operation F25B7/00) · CPC title

• F04D1/02

  having non-centrifugal stages, e.g. centripetal · CPC title

• F04D29/28

  for centrifugal or helico-centrifugal pumps {for radial-flow or helico-centrifugal pumps} · CPC title