IP Library Granted Patent US 10,962,016
Granted Patent B2
US 10,962,016 · App. 16/075,168 · Granted Mar 30, 2021

Active surge control in centrifugal compressors using microjet injection

Inventors: Joost Brasz (Nordborg, DK); William Bilbow (Tallahassee, FL); Farrukh Alvi (Tallahassee, FL); Erik Fernandez (Oviedo, FL); Jennifer Gavin (Windermere, FL)
F04D17/122F04D27/0215F04D27/0238F04D29/444F04D29/684F04D27/009F04D27/0246F04D29/462F05D2250/52
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Quick Facts
Patent No.
US 10,962,016
App. No.
16/075,168
Granted
Mar 30, 2021
Kind
B2
Abstract

A centrifugal compressor according to an exemplary aspect of the present disclosure includes, among other things, an impeller provided in a main flow path and configured to pressurize a main flow of fluid. The compressor also includes a secondary flow path configured to provide a secondary flow by recirculating a portion of the main flow. The amount of the main flow that becomes the secondary flow is less than or equal to 15%. A method is also disclosed.

Claims (26)

1. A centrifugal compressor, comprising:

an impeller provided in a main flow path and configured to pressurize a main flow of fluid; and

a secondary flow path configured to provide a secondary flow by recirculating a portion of the main flow, wherein less than or equal to 15% of the main flow becomes the secondary flow, wherein the secondary flow is introduced back into the main flow path by a plurality of injection nozzles each having a diameter within a range of 300 to 500 microns, and wherein the injection nozzles are circumferentially spaced-apart from one another by an arc length within a range of 8 to 25 of the diameters.

2. The compressor as recited in claim 1 , wherein less than or equal to 10% of the main flow becomes the secondary flow.

3. The compressor as recited in claim 2 , wherein 8.5% of the main flow becomes the secondary flow.

4. The compressor as recited in claim 1 , including an injection plate, the injection nozzles formed in the injection plate.

5. The compressor as recited in claim 1 , wherein the secondary flow path includes one of a volute and a plenum adjacent inlets of the injection nozzles.

6. The compressor as recited in claim 1 , wherein the plurality of injection nozzles are configured to introduce the secondary flow into the main flow path in a direction normal to a direction of the flow of fluid in the main flow path.

7. The compressor as recited in claim 1 , wherein the plurality of injection nozzles are radially aligned with one another relative to an axis of rotation of the impeller.

8. The compressor as recited in claim 7 , wherein the plurality of injection nozzles are evenly spaced-apart from one another in a circumferential direction.

9. The compressor as recited in claim 8 , wherein the plurality of injection nozzles have the same diameter.

10. The compressor as recited in claim 1 , wherein the secondary flow is reintroduced back into the main flow path at a location downstream of the impeller.

11. The compressor as recited in claim 10 , wherein the impeller is a first impeller within the main flow path, and wherein the compressor further includes a second impeller within the main flow path, the second impeller downstream of the first impeller.

12. The compressor as recited in claim 11 , wherein the secondary flow enters the secondary flow path at a location downstream of the second impeller.

13. The compressor as recited in claim 1 , further including:

a controller; and

a flow regulator provided in the secondary flow path, the flow regulator selectively regulating the secondary flow within the secondary flow path in response to instructions from the controller.

14. A centrifugal compressor, comprising:

an impeller provided in a main flow path and configured to pressurize a main flow of fluid;

a secondary flow path configured to provide a secondary flow into the main flow; and

injection nozzles configured to introduce the secondary flow back into the main flow path, the injection nozzles each having a diameter within a range of 300 to 500 microns, wherein the injection nozzles are radially aligned relative to an axis of rotation of the impeller and are also circumferentially spaced-apart from one another by an arc length within a range of 8 and 25 of the diameters.

15. The compressor as recited in claim 14 , wherein less than or equal to 15% of the main flow is recirculated and becomes the secondary flow.

16. A method of operating a centrifugal compressor, comprising:

establishing a main flow of fluid along a main flow path;

pressurizing the main flow with an impeller; and

selectively providing a secondary flow by recirculating less than or equal to 15% of the main flow, wherein the secondary flow is introduced back into the main flow path by a plurality of injection nozzles, the injection nozzles each having a diameter within a range of 300 to 500 microns, wherein the plurality of injection nozzles are circumferentially spaced-apart from one another by an arc length within a range of 5 and 8 millimeters.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 3, 2018
From: BILBOW, WILLIAM; ALVI, FARRUKH; FERNANDEZ, ERIK; GAVIN, JENNIFER
To: DANFOSS A/S; THE FLORIDA STATE UNIVERSITY RESEARCH FOUNDATION, INCORPORATED
Reel/Frame 046546/0882 →
Continuity (1)
Related Publication 20190040865A1 · Feb 7, 2019
Cited By (2)
US 12,338,829 US 12,460,651