Mixed-flow compressor configuration for a refrigeration system

Patent metadata

Field	Value
Publication number	US-11585347-B2
Application number	US-202017254510-A
Country	US
Kind code	B2
Filing date	May 15, 2020
Priority date	May 31, 2019
Publication date	Feb 21, 2023
Grant date	Feb 21, 2023

Abstract

A centrifugal compressor includes a casing. An impeller is arranged within the casing. The impeller is rotatable about an axis. A diffuser section is arranged within the casing. The diffuser section is positioned axially downstream from an outlet of the impeller and includes a forward portion fixed relative to the impeller and an aft portion distinct from the forward portion.

First claim

The invention claimed is:

1. A centrifugal compressor comprising:
a casing;
an impeller arranged within the casing, the impeller being rotatable about an axis and including an axially aligned outlet, the axially aligned outlet being configured such that fluid flows through the axially aligned outlet in an axial direction; and
a diffuser section arranged within the casing, the diffuser section being positioned axially downstream from the axially aligned outlet of the impeller, and including a forward portion fixed relative to the impeller and an aft portion, distinct from the forward portion, and wherein a radial height of the diffuser section is constant along the forward portion of the diffuser section.

2. The centrifugal compressor of claim 1 , wherein a radially inward boundary of the forward portion of the diffuser section includes a set of vanes protruding radially outward, and being configured to reduce a flow from supersonic to subsonic speeds.

3. The centrifugal compressor of claim 2 , wherein the set of vanes are configured to reduce a Mach number of the flow by at least 50%.

4. The centrifugal compressor of claim 2 , wherein the set of vanes are configured to reduce the Mach number to a number in the range of 0.4 to 0.8 Mach.

5. The centrifugal compressor of claim 1 , wherein the aft portion is defined by an absence of vanes.

6. The centrifugal compressor of claim 1 , wherein a radial height of the diffuser section increases along at least a portion of the aft portion.

7. The centrifugal compressor of claim 6 , wherein a radially inner wall of the diffuser section converges toward an axis defined by the diffuser section along at least a portion of the aft portion.

8. The centrifugal compressor of claim 7 , wherein a radially outer wall of the diffuser section diverges away from the axis defined by the diffuser section along the portion of the aft portion.

9. The centrifugal compressor of claim 6 , wherein a radially outer wall of the diffuser section diverges away from the axis defined by the diffuser section along the portion of the aft portion.

10. The centrifugal compressor of claim 6 , wherein the radial height increases along at least the portion of the aft portion at a constant rate.

11. The centrifugal compressor of claim 6 , wherein the radial height increases along at least the portion of the aft portion at a varying rate.

12. The centrifugal compressor of claim 1 , wherein the centrifugal compressor is a mixed-flow compressor.

13. The centrifugal compressor of claim 1 , wherein the aft portion is a freely rotating component relative to the forward portion.

14. The centrifugal compressor of claim 1 , wherein the aft portion is a fixed component relative to the forward portion.

15. The centrifugal compressor of claim 1 , wherein the axially aligned outlet is aligned with the entirety of the diffuser section.

16. A centrifugal compressor comprising:
a casing;
an impeller arranged within the casing, the impeller being rotatable about an axis and including an axially aligned outlet, the axially aligned outlet being configured such that fluid flows through the axially aligned outlet in an axial direction; and
a diffuser section arranged within the casing, the diffuser section being positioned axially downstream from the axially aligned outlet of the impeller, and including a forward portion having a constant radial height, and an aft portion having a radial height increasing along a direction of flow.

17. The centrifugal compressor of claim 16 , wherein the aft portion includes at least one of a radially converging inner wall and a radially diverging outer wall along the radial height increase.

18. The centrifugal compressor of claim 17 , wherein the at least one of the radial converging inner wall and the radially diverging outer wall is linear.

19. The centrifugal compressor of claim 17 , wherein the at least one of the radial converging inner wall and the radially diverging outer wall is curved.

20. A method for conditioning a flow in a mixed-flow centrifugal compressor according to claim 16 comprising:
reducing a speed of a fluid flow from an impeller section to below subsonic speeds using a plurality of vanes in a first diffuser section, the first diffuser section being fixed relative to an impeller; and
further reducing the speed of the fluid flow across a second diffuser portion, the second diffuser portion being freely rotating relative to the impeller.

Assignees

• Carrier Corp

Inventors

• Joly Michael M
• Sishtla Vishnu M

Classifications

• F04D17/10 Primary

  for compressing or evacuating · CPC title

• F04D29/444

  Bladed diffusers · CPC title

• F04D29/442

  rotating diffusers · CPC title

• F04D17/025 Primary

  comprising axial flow and radial flow stages · CPC title

• F04D29/284

  for compressors · CPC title