Multistage pump with axial thrust optimization

US11549512B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11549512-B2
Application numberUS-201917280515-A
CountryUS
Kind codeB2
Filing dateSep 26, 2019
Priority dateSep 27, 2018
Publication dateJan 10, 2023
Grant dateJan 10, 2023

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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 multistage pump with axial thrust optimization is disclosed includes a pump discharge nozzle and a bypass system coupled to the pump discharge nozzle. The bypass system includes a throttle valve operatively coupled to the pump discharge nozzle, and a bypass line provided at the multistage pump. The bypass line is conducts flow from the throttle valve to a clearance gap of an axial thrust balancing arrangement. The throttle valve may be actuated to adjust a balancing flow through the bypass line such that pressure at the clearance gap is adjusted to increase and decrease fluid pressure at the clearance gap to balance axial thrust at different operating states of the multistage pump.

First claim

Opening claim text (preview).

We claim: 1. A multistage pump with axial thrust adjustment, comprising: a pump discharge nozzle; and a bypass system coupled to the pump discharge nozzle, the bypass system including: a bypass line of the multistage pump, and a throttle valve operatively coupled to the pump discharge nozzle, the throttle valve being configured to adjust a balancing flow through the bypass line, and wherein a clearance gap provided for balancing axial thrust in the multistage pump is configured to receive the balancing flow through the bypass line, the throttle valve is actuatable to adjust fluid pressure in the clearance gap to control an amount of axial thrust balancing as a function of an operating state of the multistage pump, and the multi-stage pump is configured to operate the throttle valve in the bypass line in predetermined steps. 2. The multistage pump as claimed in claim 1 , wherein the throttle valve is one or more of manually, automatically, semi-automatically actuatable. 3. The multistage pump as claimed in claim 1 , wherein the throttle valve is actuatable to control the balancing flow operated such that the fluid pressure in the clearance gap is adjusted to a predetermined value based on the multistage pump operating state to reduce residual axial thrust. 4. The multistage pump as claimed in claim 1 , wherein the multistage pump is a centrifugal, high pressure barrel pump with antifriction bearings. 5. The multistage pump as claimed in claim 1 , wherein the pressure in the clearance gap is 24 bar at a pump minimum flow of 60 m 3 /hr. 6. The multistage pump as claimed in claim 1 , wherein the throttle valve in the bypass line is operable in the predetermined steps until the pressure in the clearance gap is increased to 40 bar. 7. A multistage pump with axial thrust adjustment, comprising: a bypass system configured for axial thrust adjustment, the bypass system including: a throttle bush proximal to a clearance gap of an axial thrust balancing arrangement, the throttle bush including a bypass line, wherein the clearance gap is configured to receive a balancing flow through the bypass line to control an amount of axial thrust balancing as a function of an operating state of the multistage pump, the flow control device is configured to actuate at the predetermined pressure value, and the flow control device is configured to not actuate when the multistage pump is operated at a best efficiency flow rate such that there is no flow from an impeller side of the bypass system through the clearance gap. 8. The multistage pump as claimed in claim 7 , wherein the throttle bush includes a flow control device disposed at one end of the bypass line proximal to the clearance gap, and an orifice plate disposed at an end of the bypass line opposite to the end at which the flow control device is disposed. 9. The multistage pump as claimed in claim 8 , wherein the flow control device is spring loaded. 10. The multistage pump as claimed in claim 8 , wherein the flow control device is configured to actuate when the multistage pump is at a part load condition. 11. The multistage pump as claimed in claim 8 , wherein the orifice plate is configured to control a fluid pressure at the clearance gap to a predetermined value.

Assignees

Inventors

Classifications

  • especially adapted for liquid pumps (F04D29/18 takes precedence) · CPC title

  • balancing pistons · CPC title

  • By-passing by increasing clearance between impeller and its casing · CPC title

  • Multi-stage pumps (F04D1/02, F04D13/10 take precedence) · CPC title

  • throttling valves or valves varying the pump inlet opening or the outlet opening · CPC title

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What does patent US11549512B2 cover?
A multistage pump with axial thrust optimization is disclosed includes a pump discharge nozzle and a bypass system coupled to the pump discharge nozzle. The bypass system includes a throttle valve operatively coupled to the pump discharge nozzle, and a bypass line provided at the multistage pump. The bypass line is conducts flow from the throttle valve to a clearance gap of an axial thrust bala…
Who is the assignee on this patent?
Ksb Se & Co Kgaa
What technology area does this patent fall under?
Primary CPC classification F04D29/0416. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 10 2023 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).