Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors

US11536277B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11536277-B2
Application numberUS-202117453456-A
CountryUS
Kind codeB2
Filing dateNov 3, 2021
Priority dateApr 30, 2020
Publication dateDec 27, 2022
Grant dateDec 27, 2022

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

Centrifugal compressors can incorporate a side stream flow of intermediate pressure vapor between stages of that compressor. The side stream flow can be controlled by a side stream injection port controlled by a throttle ring disposed between stages of the compressor. The throttle ring can allow or obstruct flow through the side stream injection port. The throttle ring can extend and retract in a direction substantially perpendicular to the direction of flow from the first stage impeller to the second stage impeller. A method of operating a centrifugal compressor can include actuating a throttle ring by rotating a drive ring to adjust a flow of interstage fluid into the second stage impeller.

First claim

Opening claim text (preview).

What is claimed is: 1. A centrifugal compressor for compressing a fluid, comprising: a first stage impeller; a second stage impeller; a plurality of guide vanes forming channels located between the first stage impeller and the second stage impeller, the channels configured to direct an interstage flow of the fluid from the first stage impeller to the second stage impeller; a side stream injection port located between the first stage impeller and the second stage impeller, the side stream injection port configured to receive a side stream of the fluid; and a throttle ring configured to move through the side stream injection port between an extended position and a retracted position, a drive ring; and linkage assemblies connecting the drive ring to the throttle ring such that rotation of the drive ring moves the throttle ring in an axial direction between the retracted position and the extended position, wherein in the extended position, the throttle ring obstructs flow of the side stream of the fluid through the side stream injection port and partially obstructs the interstage flow of the fluid through the channels, and in the retracted position, the throttle ring allows the side stream of the fluid to flow through the side stream injection port. 2. The centrifugal compressor of claim 1 , wherein the throttle ring includes teeth, and in the extended position, the teeth of the throttle ring are disposed in and obstruct the channels. 3. The centrifugal compressor of claim 2 , wherein the teeth extend in the axial direction and include tips that curve radially inward. 4. The centrifugal compressor of claim 2 , wherein in the retracted position, the teeth of the throttle ring are disposed in the side stream injection port. 5. The centrifugal compressor of claim 2 , wherein the teeth of the throttle ring obstruct less of the channels in the retracted position than in the extended position, and the throttle ring obstructs more of the side stream injection port in the retracted position than in the extended position. 6. The centrifugal compressor of claim 2 , wherein in the retracted position, the fluid in the side stream flows over the throttle ring into the side stream injection port, and in the extended position, the fluid in the interstage flow passes through the channels by flowing across tips of the teeth. 7. The centrifugal compressor of claim 1 , wherein in the retracted position, the throttle ring blocks the side stream injection port. 8. The centrifugal compressor of claim 1 , wherein in the retracted position: the interstage flow of the fluid from the first stage impeller has a higher flowrate than in the extended position, and the side stream has a higher flowrate through the side stream injection port than in the extended position. 9. The centrifugal compressor of claim 1 , wherein the throttle ring includes radial shafts, each linkage assembly of the linkage assemblies include pairs of a drive linkage and a support linkage connected to the radial shafts of the throttle ring, the drive linkage and the support linkage in each of the pairs connected to the same respective one of the radial shafts on the throttle ring. 10. The centrifugal compressor of claim 9 , further comprising: a housing, the throttle ring, the drive ring, and the plurality of guide vanes disposed within the housing, wherein the drive linkages connect the drive ring to the throttle ring, the drive linkages configured to transfer rotation of the drive ring into axial movement of the throttle ring, and the support linkages connect the throttle ring to the housing, the support linkages configured to prevent rotation of the throttle ring. 11. The centrifugal compressor of claim 1 , further comprising: an actuator and an actuation linkage assembly, the actuation linkage assembly connects the actuator to the drive ring, and the actuator configured to extend causing the rotation of the drive ring and configured to retract causing an opposite rotation of the drive ring. 12. A method of operating a centrifugal compressor, the centrifugal compressor including a first stage impeller, a second stage impeller, and a plurality of guide vanes and a side stream injection port each respectively located between the first stage impeller and the second stage impeller, and the method comprising: compressing a fluid with the first stage impeller; directing, via channels formed by the plurality of guide vanes, an interstage flow of the fluid discharged from the first stage impeller to an inlet of the second stage impeller; and actuating a throttle ring to adjust a flow of the fluid in the interstage flow into the second stage impeller, the centrifugal compressor including the throttle ring, a drive ring, and linkage assemblies connecting the drive ring to the throttle ring, and the actuating of the throttle ring including: moving the throttle ring in an axial direction between a retracted position and an extended position by a rotation of the drive ring, the rotation of the drive ring causing the throttle ring to move in the axial direction, wherein in the extended position, flow of the side stream of the fluid through the side stream injection port is obstructed by the throttle ring and flow of the interstage fluid through the channels is partially obstructed by the throttle ring, and in the retracted position, the side stream of the fluid flows through the side stream injection port and into the inlet of the second stage impeller. 13. The method of claim 12 , wherein the throttle ring includes teeth, and the moving of the throttle ring in the axial direction between the retracted position and the extended position includes: moving the throttle ring from the retracted position to the extended position, which includes moving the teeth into the channels, and moving the throttle ring from the extended position to the retracted position, which includes withdrawing the teeth from the channels. 14. The method of claim 13 , wherein moving the throttle ring from the extended position to the retracted position includes moving the teeth along the axial direction into the side stream injection port. 15. The method of claim 12 , wherein the centrifugal compressor includes an actuator and an actuation linkage assembly, the actuation linkage assembly connects the actuator to the drive ring, and the moving of the throttle ring in the axial direction between the retracted position and the extended position by rotating the drive ring includes: extending the actuator to rotate the drive ring in a first direction, and retracting the actuator to rotate the drive ring in an opposite direction.

Assignees

Inventors

Classifications

  • Bladed diffusers · CPC title

  • F04D17/122Primary

    the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors · CPC title

  • especially adapted for elastic fluid pumps · CPC title

  • adjusting flow cross-section, otherwise than by using adjustable stator blades · CPC title

  • by fluid injection · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US11536277B2 cover?
Centrifugal compressors can incorporate a side stream flow of intermediate pressure vapor between stages of that compressor. The side stream flow can be controlled by a side stream injection port controlled by a throttle ring disposed between stages of the compressor. The throttle ring can allow or obstruct flow through the side stream injection port. The throttle ring can extend and retract in…
Who is the assignee on this patent?
Trane Int Inc
What technology area does this patent fall under?
Primary CPC classification F04D17/122. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 27 2022 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 9 related publications on this page (citations in our corpus or others sharing the same primary CPC).