IP Library Granted Patent US 12,410,821
Granted Patent B2
US 12,410,821 · App. 18/125,398 · Granted Sep 9, 2025

Reducing cavitation, noise, and vibration in a pressure exchanger

Inventors: Chinmay Vishwas Deshpande (Fremont, CA); Omprakash Samudrala (San Ramon, CA); Sujan Reddy Gudigopuram (San Ramon, CA); Alexander Patrick Theodossiou (Alameda, CA); Teymour Javaherchi (Piedmont, CA); Anthony Kim Phan (San Jose, CA)
Assignee: Energy Recovery, Inc.
F04F13/00
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Quick Facts
Patent No.
US 12,410,821
App. No.
18/125,398
Granted
Sep 9, 2025
Kind
B2
Abstract

A pressure exchanger includes a rotor configured to exchange pressure between a first fluid at a first pressure and a second fluid at a second pressure. The rotor forms ducts that are routed from a first distal end to a second distal end. The rotor forms chamfers on trailing edge rotor duct walls. The pressure exchanger further includes a first end cover that forms a high pressure in (HPIN) port configured to provide the first fluid at the first pressure into the ducts. The first end cover forms a low pressure out (LPOUT) port configured to receive the first fluid from the ducts at a third pressure. The pressure exchanger further includes a second end cover that forms a low pressure in (LPIN) port configured to provide the second fluid at the second pressure into the ducts and forms a high pressure out (HPOUT) port configured to receive the second fluid from the ducts at a fourth pressure.

Claims (26)

1. A pressure exchanger comprising:

a rotor configured to rotate to exchange pressure between a first fluid at a first pressure and a second fluid at a second pressure, wherein the rotor forms ducts that are routed from a first distal end of the rotor to a second distal end of the rotor, wherein the rotor forms chamfers on trailing edge rotor duct walls without forming chamfers on leading edge rotor duct walls;

a first end cover disposed at the first distal end of the rotor, wherein the first end cover forms a high pressure in (HPIN) port configured to provide the first fluid at the first pressure into the ducts, and wherein the first end cover forms a low pressure out (LPOUT) port configured to receive the first fluid from the ducts at a third pressure that is lower than the first pressure; and

a second end cover disposed at the second distal end of the rotor, wherein the second end cover forms a low pressure in (LPIN) port configured to provide the second fluid at the second pressure into the ducts and forms a high pressure out (HPOUT) port configured to receive the second fluid from the ducts at a fourth pressure that is higher than the second pressure.

2. The pressure exchanger of claim 1 , wherein the second end cover forms a first spot face proximate the HPOUT port.

3. The pressure exchanger of claim 2 , wherein the pressure exchanger forms a second spot face proximate the LPIN port of the second end cover without forming a spot face proximate the LPOUT port of the first end cover to depressurize a high pressure (HP) duct of the rotor at the LPIN port.

4. The pressure exchanger of claim 1 , wherein the first end cover forms the HPIN port without forming a spot face proximate the HPIN port.

5. The pressure exchanger of claim 2 , wherein the second end cover forms a chamfer at the LPIN port that is configured to change a corresponding angle of the first spot face for each concentric row of the ducts of the rotor.

6. The pressure exchanger of claim 5 , wherein the chamfer at the LPIN port is configured to change an angle for each duct to be exposed to the first spot face to change an amount of pressurization of different rows of ducts.

7. The pressure exchanger of claim 2 , wherein the first spot face has a radial extent that is shorter than a duct radial extent of a corresponding duct formed by the rotor to reduce a diameter at which a rotor duct is to open to an end cover port to reduce tangential velocity and cavitation potential.

8. The pressure exchanger of claim 2 , wherein the first spot face comprises a first recess associated with a first concentric row of the ducts and a second recess associated with a second concentric row of the ducts.

9. The pressure exchanger of claim 1 , wherein the rotor forms the ducts in concentric rows that are staggered.

10. The pressure exchanger of claim 1 , wherein a duct opening of the rotor to a corresponding end cover spot face is at an inside duct diameter by adjusting an angle of a spot face edge or curving a spot face wall respective to the duct opening.

11. A pressure exchanger comprising:

a rotor configured to rotate to exchange pressure between a first fluid at a first pressure and a second fluid at a second pressure, wherein the rotor forms ducts that are routed from a first distal end of the rotor to a second distal end of the rotor, wherein the rotor forms the ducts in at least two concentric rows comprising a first concentric row of the ducts, a second concentric row of the ducts, and a third concentric row of the ducts; and

a first end cover disposed at the first distal end of the rotor, wherein the first end cover forms a first port, a second port, and a split spot face proximate the first port, wherein the split spot face comprises a first recess associated with the first concentric row of the ducts and a second recess associated with the second concentric row of the ducts and the third concentric row of the ducts.

12. The pressure exchanger of claim 11 , wherein corresponding ducts in the first concentric row and the second concentric row are staggered.

13. The pressure exchanger of claim 11 , wherein the split spot face has a radial extent that is shorter than a duct radial extent of a corresponding duct formed by the rotor.

14. The pressure exchanger of claim 11 , wherein the pressure exchanger forms the split spot face proximate a low pressure in (LPIN) port without forming a spot face proximate a low pressure out (LPOUT) port to depressurize a high pressure (HP) duct of the rotor at the LPIN port.

15. The pressure exchanger of claim 11 , wherein the rotor forms chamfers on trailing edge rotor duct walls.

16. A pressure exchanger comprising:

a rotor configured to rotate to exchange pressure between a first fluid at a first pressure and a second fluid at a second pressure, wherein the rotor forms ducts that are routed from a first distal end of the rotor to a second distal end of the rotor, wherein the rotor forms the ducts in at least two concentric rows comprising a first concentric row of the ducts and a second concentric row of the ducts; and

a first end cover disposed at the first distal end of the rotor, wherein the first end cover forms a first port, a second port, and a spot face, wherein the first end cover forms a chamfer at the first port, wherein the chamfer changes a corresponding angle of the spot face for each concentric row of the ducts of the rotor, and wherein the chamfer at the first port is configured to change an angle for each duct to be exposed to the spot face to change an amount of pressurization of different rows of ducts.

17. The pressure exchanger of claim 16 , wherein the rotor forms the ducts in concentric rows that are staggered, wherein the spot face has a radial extent that is shorter than that of a corresponding duct to cause fluid tangential velocity and pressure in the corresponding duct to increase with a radial coordinate.

18. The pressure exchanger of claim 16 , wherein the pressure exchanger forms the spot face proximate a low pressure in (LPIN) port without forming a spot face proximate a low pressure out (LPOUT) port to depressurize a high pressure (HP) duct of the rotor at the LPIN port.

19. The pressure exchanger of claim 16 , wherein the rotor forms chamfers on trailing edge rotor duct walls.

Assignments (2)
SECURITY INTEREST Recorded Jan 21, 2026
From: ENERGY RECOVERY, INC.
To: JPMORGAN CHASE BANK, N.A.
Reel/Frame 073535/0966 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 25, 2023
From: DESHPANDE, CHINMAY VISHWAS; SAMUDRALA, OMPRAKASH; GUDIGOPURAM, SUJAN REDDY; THEODOSSIOU, ALEXANDER PATRICK; JAVAHERCHI, TEYMOUR; PHAN, ANTHONY KIM
To: ENERGY RECOVERY, INC.
Reel/Frame 063102/0323 →
Continuity (4)
Provisional Application 63395694 · Aug 5, 2022
Provisional Application 63388991 · Jul 13, 2022
Provisional Application 63323462 · Mar 24, 2022
Related Publication 20230304513A1 · Sep 28, 2023
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