Variable-speed multi-stage refrigerant centrifugal compressor with diffusers

US10072663B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10072663-B2
Application numberUS-201214373712-A
CountryUS
Kind codeB2
Filing dateJan 23, 2012
Priority dateJan 23, 2012
Publication dateSep 11, 2018
Grant dateSep 11, 2018

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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.

First claim

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.

Assignees

Inventors

Classifications

  • F04D17/12Primary

    Multi-stage pumps · CPC title

  • Compression machines, plants or systems with non-reversible cycle (F25B3/00, F25B5/00, F25B6/00, F25B7/00, F25B9/00 take precedence) · CPC title

  • of turbine type · CPC title

  • with means for changing the flow-path through the stages, e.g. series-parallel, e.g. side-loads, (surge control F04D27/02) · CPC title

  • Outlet · CPC title

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Frequently asked questions

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What does patent US10072663B2 cover?
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.
Who is the assignee on this patent?
Sun Lin, Brasz Joost, Rasmussen Mogens, and 1 more
What technology area does this patent fall under?
Primary CPC classification F04D17/12. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Sep 11 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).