IP Library › Granted Patent US 12,209,584
Granted Patent B2
US 12,209,584 · App. 17/972,813 · Granted Jan 28, 2025

Submersible centrifual pump having a hydrostatic support including thrust and support disks

Inventors: Anton Shakirov (Limatol, CY); Vitaly Koropetskiy (Moscow, RU); Iaroslav Alekseev (Moscow, RU); Vadim Batalov (Moscow, RU)
Assignee: LEX SUMBERSIBLE PUMPS FZE
F04C18/107E21B43/121F04C2/16F04C15/0023F04C23/001F04C27/008F04C29/12F04D17/12F04D29/057F04D29/162F04D29/4213F04C2240/10F04C2240/20F04C2240/30F04C2240/50F04C2240/54F04C2240/60F04C2240/802F04D3/02
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Quick Facts
Patent No.
US 12,209,584
App. No.
17/972,813
Granted
Jan 28, 2025
Kind
B2
Abstract

A method and apparatus to increase the labyrinth screw pump life, achieved by a decrease in axial forces in thrust tribo-couplings by creating a chamber into which high pressure at the exit from the stage is transmitted through the additional holes of the rotor, thereby creating an opposite axial force, which reduces the contact pressure on the friction surface of the thrust bearing.

Claims (13)

1. A submersible multistage borehole centrifugal pump comprising:

a cylindrical housing;

a cylindrical stator rotationally fixed inside of the cylindrical housing;

a cylindrical rotor disposed inside of the cylindrical stator;

a rotor shaft in the housing that causes the cylindrical rotor to spin;

a discharge end of the cylindrical rotor configured with a hole to discharge production fluid;

an intake end of the cylindrical rotor configured with a hole to allow intake of production fluid;

a first thrust bearing attached to the rotor shaft on the intake end of a first modular pump stage;

a discharge thrust bearing attached to the rotor shaft on the discharge end of the first modular pump stage;

an unloading thrust bearing attached to the rotor shaft positioned between the intake thrust bearing and the intake end of the rotor;

a cavity in the unloading thrust bearing configured to receive production fluid from the discharge end of the rotor; and

holes located inside of the cylindrical rotor positioned substantially half way

between the rotor shaft and an outside edge of the rotor, wherein the holes of the cylindrical rotor run between the discharge end of the rotor and the unloading thrust bearing cavity, wherein a counter action against axial force on the rotor shaft is provided by the production fluid flowing in the holes from the discharge end of the rotor into the cavity in the unloading thrust bearing, wherein the production fluid in the cavity presses against the unloading thrust bearing thereby counteracting and reducing the axial force on the rotor shaft, wherein the pump operates at a speed of between 10,000 rpm and 12,000 rpm, and wherein the production fluid is one of high-viscous fluid, a low viscous fluid, a condensate, or a mixture of gas.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 17, 2024
From: SHAKIROV, ANTON; BATALOV, VADIM; KOROPETSKIY, VITALY; ALEEKSEEV, IAROSLAV
To: LEX SUBMERSIBLE PUMPS FZE
Reel/Frame 069602/0820 →
Continuity (7)
Division 17717889 · Apr 11, 2022
Provisional Application 63298734 · Jan 12, 2022
Provisional Application 63283340 · Nov 26, 2021
Provisional Application 63283342 · Nov 26, 2021
Provisional Application 63283343 · Nov 26, 2021
Provisional Application 63175596 · Apr 16, 2021
Related Publication 20230193903A1 · Jun 22, 2023
References Cited (19)
US 8696331B2 · Cunningham · 2014 [cited by applicant]
US 8770271B2 · Fielder et al. · 2014 [cited by applicant]
US 9242032B2 · LaRose et al. · 2016 [cited by applicant]
US 10323644B1 · Shakirov · 2019 [cited by examiner]
US 10385856B1 · Shakirov · 2019 [cited by examiner]
US 10584566B2 · Crane et al. · 2020 [cited by applicant]
US 11867176B1 · Shakirov · 2024 [cited by examiner]
US 20040096320A1 · Yevtushenko · 2004 [cited by applicant]
US 20090098003A1 · Kothnur et al. · 2009 [cited by applicant]
US 20150308434A1 · Crane · 2015 [cited by examiner]
US 20200072226A1 · Villarreal · 2020 [cited by applicant]
CN 208221130U · 2018 [cited by applicant]
RU 2376505C2 · 2009 [cited by applicant]
RU 2593325C1 · 2016 [cited by examiner]
RU 2726977C1 · 2020 [cited by applicant]
RU 202692U1 · 2021 [cited by examiner]
Axial Thrust, Link: https://www.ksb.com/centrifugal-pump-lexicon/axial-thrust/191862/. [cited by applicant]
Cylindrical roller thrust bearings; Link: https://www.skf.com/group/products/rolling-bearings/roller-bearings/cylindrical-roller-thrust-bearings. [cited by applicant]
Xia, B. et al., Investigation of axial thrust deviation between the theory and experiment for high-speed mine submersible pump; Advances in Mechanical Engineering; 2018, vol. 10(8); pp. 1-13; DOI: 10.1177/16878140187892… [cited by applicant]