Two-stage refrigerant compressor and operation method thereof
US-2024418169-A1 · Dec 19, 2024 · US
US9382911B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9382911-B2 |
| Application number | US-201414479964-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 8, 2014 |
| Priority date | Nov 14, 2013 |
| Publication date | Jul 5, 2016 |
| Grant date | Jul 5, 2016 |
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One exemplary embodiment of this disclosure relates to a centrifugal refrigerant compressor system. The system includes a condenser, an evaporator, and an economizer between the condenser and the evaporator. The system further includes a centrifugal compressor having a first impeller and a second impeller downstream of the first impeller. The compressor includes at least one port. Fluid from a recirculation flow path and an economizer flow path is introduced into a main flow path of the compressor by way of the at least one port.
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What is claimed is: 1. A centrifugal refrigerant compressor system, comprising: a condenser; an evaporator; an economizer between the condenser and the evaporator; and a centrifugal compressor including a first impeller and a second impeller downstream of the first impeller, the compressor including at least one port provided at a location downstream of the first impeller, wherein fluid from a recirculation flow path and an economizer flow path is introduced into a main flow path of the compressor by way of the at least one port, wherein the recirculation flow path is provided directly between an outlet of the compressor and the at least one port, wherein the at least one port is a single port provided downstream of the first impeller and upstream of the second impeller, and wherein the port is provided adjacent a return channel between the first and second impellers. 2. The refrigerant system as recited in claim 1 , wherein the economizer flow path is sourced from the economizer. 3. The refrigerant system as recited in claim 1 , wherein the compressor includes one of a variable geometry diffuser and inlet guide vanes. 4. The refrigerant system as recited in claim 3 , wherein the compressor includes a variable geometry diffuser downstream of the first impeller, and wherein the compressor further includes a stationary vane diffuser downstream of the second impeller. 5. The refrigerant system as recited in claim 3 , wherein the compressor includes inlet guide vanes, and wherein the compressor further includes first and second vaneless diffusers downstream of the first and second impellers, respectively. 6. The refrigerant system as recited in claim 1 , wherein the compressor further includes a stationary vane diffuser downstream of the first impeller, and wherein the port is adjacent the stationary vane diffuser. 7. A centrifugal refrigerant compressor, comprising: a first impeller; a second impeller downstream of the first impeller; and a single port in fluid communication with a recirculation flow path and an economizer flow path, wherein the recirculation flow path is provided directly between an outlet of the centrifugal refrigerant compressor and the port, wherein the port is provided downstream of the first impeller, and wherein the port is configured to inject fluid from the recirculation flow path and the economizer flow path into a return channel between the first and second impellers. 8. The centrifugal refrigerant compressor as recited in claim 7 , wherein the outlet of the centrifugal refrigerant compressor is provided by a volute. 9. The refrigerant system as recited in claim 1 , wherein the outlet of the compressor is provided by a volute.
Mechanical Engineering · mapped topic
Economisers · CPC title
of turbine type · CPC title
by bleeding, bypassing or recycling fluids (influencing the boundary layer by an uncontrolled bleeding of the working fluid F04D29/681) · CPC title
with multi-stage compression (with cascade operation F25B7/00) · CPC title
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