Centrifugal acceleration stabilizer

Patent metadata

Field	Value
Publication number	US-12163535-B2
Application number	US-202318465313-A
Country	US
Kind code	B2
Filing date	Sep 12, 2023
Priority date	May 6, 2022
Publication date	Dec 10, 2024
Grant date	Dec 10, 2024

Abstract

A dynamic compressor includes an impeller having impeller vanes disposed around a hub, a shroud, and a diffuser having a shroud surface adjacent to the shroud and a hub surface adjacent to the hub, wherein the diffuser is circumferentially disposed around the impeller. The diffuser includes a plurality of diffuser vanes extending from the hub surface to the shroud surface, each having a vane leading edge and a vane trailing edge. The diffuser includes a centrifugal acceleration stabilizer ring formed in the shroud surface located in a vaneless region defined between an impeller trailing edge and the vane leading edge. The centrifugal acceleration stabilizer ring stabilizes the flow of the fluid by changing the circumferentially-flowing high velocity fluid flow exiting the impeller into a radially-flowing high velocity fluid flow before entering the diffuser, improving the efficiency of the dynamic compressor.

First claim

What is claimed is:

1. A centrifugal compressor comprising:
an impeller having a plurality of impeller vanes disposed around a hub, the impeller configured to rotate about an axis of rotation to receive a fluid flow at least substantially aligned with the axis of rotation, accelerate the fluid flow to a high velocity fluid flow, and dispense the high velocity fluid flow in a direction at least generally perpendicular to the axis of rotation;
a shroud configured to surround the impeller and direct the high velocity fluid flow dispensed by the impeller; and
a diffuser having a shroud surface adjacent to the shroud and a hub surface adjacent to the hub, the diffuser circumferentially disposed around the impeller and configured to receive the high velocity fluid flow from the impeller and convert the high velocity fluid flow into a high pressure fluid flow, the diffuser defining a diffuser;
wherein the diffuser includes a centrifugal acceleration stabilizer ring disposed in the shroud surface, the centrifugal acceleration stabilizer ring configured to increase the radial velocity of a lower momentum region of a flow field flowing in the diffuser, resulting in a more uniform flow field across the diffuser passage, before re-expanding the area of the diffuser passage to facilitate diffusion, and where the centrifugal acceleration stabilizer ring has a height within a range between three percent (3%) and twenty percent (20%) of a distance between the shroud surface and the hub surface.

2. The centrifugal compressor of claim 1 , wherein a cross-sectional profile of the centrifugal acceleration stabilizer ring is defined by a curved protrusion.

3. The centrifugal compressor of claim 2 , wherein the cross-sectional profile of the centrifugal acceleration stabilizer ring is defined by a semi-circular protrusion.

4. The centrifugal compressor of claim 2 , wherein the cross-sectional profile of the centrifugal acceleration stabilizer ring is defined by a curved protrusion having a substantially flat top surface.

5. The centrifugal compressor of claim 1 , wherein the impeller is one of a semi-open impeller or a closed impeller.

6. The centrifugal compressor of claim 1 , wherein the diffuser is a parallel-wall diffuser.

7. The centrifugal compressor of claim 1 , wherein the diffuser comprises a plurality of diffuser vanes extending from the hub surface to the shroud surface, respective ones of the plurality of diffuser vanes having a vane leading edge and a vane trailing edge, and where the centrifugal acceleration stabilizer ring is located in a vaneless region between an impeller trailing edge and the vane leading edge.

8. The centrifugal compressor of claim 7 , wherein the vaneless region has a radial length within a range between ten percent (10%) and twenty-five percent (25%) of an impeller radius.

9. The centrifugal compressor of claim 8 , wherein the centrifugal acceleration stabilizer ring extends along the entirety of the vaneless region.

10. The centrifugal compressor of claim 7 , wherein the centrifugal acceleration stabilizer ring extends over a partial radial length of the vaneless region.

11. A centrifugal compressor comprising:
an impeller having a plurality of impeller vanes disposed around a hub and an impeller trailing edge, the impeller configured to rotate about an axis of rotation to receive a fluid flow at least substantially aligned with the axis of rotation, accelerate the fluid flow to a high velocity fluid flow, and dispense the high velocity fluid flow in a direction at least generally perpendicular to the axis of rotation;
a shroud configured to surround the impeller and direct the high velocity fluid flow dispensed by the impeller; and
a parallel-walled diffuser having a shroud surface adjacent to the shroud and a hub surface adjacent to the hub, the parallel-walled diffuser circumferentially disposed around the impeller and configured to receive the high velocity fluid flow from the impeller and convert the high velocity fluid flow into a high pressure fluid flow, the parallel-walled diffuser defining a diffuser passage;
wherein the parallel-walled diffuser includes a centrifugal acceleration stabilizer ring formed in the shroud surface, the centrifugal acceleration stabilizer ring configured to increase the radial velocity of a lower momentum region of a flow field flowing in the diffuser, resulting in a more uniform flow field across the diffuser passage, before re-expanding the area of the diffuser passage to facilitate diffusion, and where the centrifugal acceleration stabilizer ring has a height within a range between three percent (3%) and twenty percent (20%) of a distance between the shroud surface and the hub surface.

12. The centrifugal compressor of claim 11 , wherein the parallel-walled diffuser comprises a plurality of diffuser vanes extending from the hub surface to the shroud surface, respective ones of the plurality of diffuser vanes having a vane leading edge and a vane trailing edge, and where the centrifugal acceleration stabilizer ring is located in a vaneless region between an impeller trailing edge and the vane leading edge.

13. The centrifugal compressor of claim 12 , wherein the vaneless region has a radial length within a range between ten percent (10%) and twenty-five percent (25%) of an impeller radius.

14. The centrifugal compressor of claim 12 , wherein the centrifugal acceleration stabilizer ring extends over a partial radial length of the vaneless region.

15. The centrifugal compressor of claim 12 wherein the centrifugal acceleration stabilizer ring extends along the entirety of the vaneless region.

16. The centrifugal compressor of claim 11 , wherein a cross-sectional profile of the centrifugal acceleration stabilizer ring is defined by a curved protrusion.

17. The centrifugal compressor of claim 11 , wherein the impeller is one of a semi-open impeller or a closed impeller.

18. A centrifugal compressor comprising:
an impeller configured to rotate about an axis of rotation to receive a fluid flow at least substantially aligned with the axis of rotation, accelerate the fluid flow to a high velocity fluid flow, and dispense the high velocity fluid flow in a direction at least generally perpendicular to the axis of rotation;
a shroud configured to surround the impeller and direct the high velocity fluid flow dispensed by the impeller; and
a diffuser having a shroud surface adjacent to the shroud and a hub surface adjacent to the hub, the diffuser circumferentially disposed around the impeller and configured to receive the high velocity fluid flow from the impeller and convert the high velocity fluid flow into a high pressure fluid flow, the diffuser defining a diffuser passage;
wherein the diffuser includes a centrifugal acceleration stabilizer ring disposed in the shroud surface, the centrifugal acceleration stabilizer ring configured to increase the radial velocity of a lower momentum region of a flow field flowing in the diffuser, resulting in a more uniform flow field across the diffuser passage, before re-expanding the area of the diffuser passage to facilitate diffusion, and where the centrifugal acceleration stabilizer ring has a height within a range between three percent (3%) and twenty percent (20%) of a distance between the shroud surface and the hub surface.

19. The centrifugal compressor of claim 18 , wherein the diffuser comprises a plurality of diffuser vanes extending from the hub surface to the shroud surface, respective ones of the plurality of diffuser vanes having a vane leadi

Assignees

• Ingersoll Rand Industrial Us Inc

Inventors

• Swiatek Chester V
• Grigoriev Mikhail
• Brown Paul C
• Impastato Charles

Classifications

• F05D2250/52

  Outlet · CPC title

• F04D29/464

  adjusting flow cross-section, otherwise than by using adjustable stator blades · CPC title

• F04D29/444 Primary

  Bladed diffusers · CPC title

• F04D29/441

  especially adapted for elastic fluid pumps · CPC title

• F04D17/10

  for compressing or evacuating · CPC title