Respiratory apparatus
US-2024342412-A1 · Oct 17, 2024 · US
US10072663B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10072663-B2 |
| Application number | US-201214373712-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 23, 2012 |
| Priority date | Jan 23, 2012 |
| Publication date | Sep 11, 2018 |
| Grant date | Sep 11, 2018 |
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A refrigeration system includes a chiller having a refrigerant loop. A compressor is part of and in fluid communication with the refrigerant loop. The compressor has two stages, one with a variable geometry diffuser and one with a fixed geometry diffuser.
Opening claim text (preview).
What is claimed is: 1. A refrigerant centrifugal compressor comprising: a housing comprising a first compressor inlet and outlet and a second compressor inlet and outlet; first and second impellers arranged in the housing with the first impeller arranged fluidly between the first compressor inlet and outlet and the second impeller arranged fluidly between the second compressor inlet and outlet; and first and second diffusers arranged in the housing with the first diffuser arranged fluidly between an outlet of the first impeller and the second compressor inlet, and the second diffuser arranged fluidly downstream from an outlet of the second impeller, the first and second diffusers being different from one another, wherein the first diffuser is geometrically variable and the second diffuser is geometrically fixed, and wherein the first diffuser includes a plurality of fixed wedge-shaped vanes located fluidly downstream of a moveable diffuser wall element, the plurality of wedge-shaped vanes tapered such that a width dimension of the plurality of wedge-shaped vanes gradually decreases from a trailing edge to a leading edge thereof, the moveable diffuser wall element being serrated with trailing edges of serration overlapping a throat area of the first diffuser; and wherein the refrigerant centrifugal compressor does not utilize variable inlet guide vanes upstream of the first impeller. 2. The refrigerant centrifugal compressor according to claim 1 , wherein vanes of the second diffuser are low solidity vanes, and wherein the trailing edge over leading edge radius ratio of the low solidity vanes is less than 1.2. 3. The refrigerant centrifugal compressor according to claim 2 , wherein a solidity of the second diffuser is less than 0.9. 4. The refrigerant centrifugal compressor according to claim 1 , comprising magnetic bearings supporting a rotor shaft, and a bearing controller configured to command the magnetic bearings in response to a bearing command for magnetically supporting the rotor shaft. 5. The refrigerant centrifugal compressor according to claim 1 , wherein the throat area of the first diffuser is a smallest cross-sectional flow passage between the wedge-shaped vanes. 6. A refrigeration system comprising: a chiller having a refrigerant loop; and a compressor in fluid communication with the refrigerant loop, the compressor having first and second compressor stages having first and second impellers, respectively, the first and second compressor stages further having first and second diffusers, respectively, wherein the first diffuser is arranged fluidly between an outlet of the first impeller and an inlet of the second impeller, and the second diffuser is arranged fluidly downstream from an outlet of the second impeller, wherein the first diffuser is geometrically variable and the second diffuser is geometrically fixed, and wherein the first diffuser includes a plurality of fixed wedge-shaped vanes located fluidly downstream of a moveable diffuser wall element, the plurality of wedge-shaped vanes tapered such that a width dimension of the plurality of wedge-shaped vanes gradually decreases from a trailing edge to a leading edge thereof, the moveable diffuser wall element being serrated with trailing edges of serration overlapping a throat area of the first diffuser; and wherein the compressor does not utilize variable inlet guide vanes upstream of the first impeller. 7. The refrigeration system according to claim 6 , wherein the second diffuser is a low solidity vaned diffuser, a trailing edge over a leading edge radius ratio of the vanes of the low solidity vaned diffuser is less than 1.2, and wherein a solidity of the low solidity vaned diffuser is less than 0.9. 8. The refrigerant system according to claim 6 , wherein the throat area of the first diffuser is a smallest cross-sectional flow passage between the wedge-shaped vanes.
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with means for changing the flow-path through the stages, e.g. series-parallel, e.g. side-loads, (surge control F04D27/02) · CPC title
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