Centrifugal compressor with extended operating range
US-10184481-B2 · Jan 22, 2019 · US
US10962016B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10962016-B2 |
| Application number | US-201616075168-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 4, 2016 |
| Priority date | Feb 4, 2016 |
| Publication date | Mar 30, 2021 |
| Grant date | Mar 30, 2021 |
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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.
Opening claim text (preview).
What is claimed is: 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.
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