Analysis of the efficiency of balancing pistons of feed pumps

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Abstract

BACKGROUND: Thermo power industry demands the high level of reliability of pump equipment. Regarding that, improvement of reliability of feed pump structure and balancing device in particular is a relevant issue.

AIMS: To perform numerical simulation of a balancing device in order to determine its optimal design and parameters. The study object is the balancing device of the PEN 290-115 feed pump

METHODS: Two types of the balancing piston, two-stage and single-stage, were studied. The series of computational fluid dynamics simulations of the three-dimensional flow of a viscous liquid were performed using the ANSYS CFX software in order to study the efficiency of given designs.

RESULTS: The calculated characteristics of the two designs of the unloading device were obtained. The influence of roughness and radial clearance on the efficiency of a cylindrical piston was studied. The simulation results showed that the radial clearance decrease leads to balancing device losses decrease. The roughness value increase may also lead to the leaks decrease, but its excessive increase leads to friction losses increase, so it is necessary to control both parameters when searching for the optimal roughness value.

CONCLUSIONS: The optimal design of the balancing piston, which combines simplicity of manufacturing, reliability and energy efficiency, is proposed.

About the authors

Alexander A. Zharkovsky

Peter the Great Saint Petersburg Polytechnic University

Email: azharkovsky@gmail.com
ORCID iD: 0000-0002-3044-8768
SPIN-code: 3637-7853
Scopus Author ID: 7004534701
ResearcherId: T-3278-2018

Dr. Sci. (Tech.), Professor of the Higher School of Power Engineering of the Institute of Energy

Russian Federation, 29 Polytechnicheskaya street, 195251 Saint Petersburg

Alexander A. Zakharov

Peter the Great Saint Petersburg Polytechnic University

Author for correspondence.
Email: zakharov.aa.gm@yandex.ru
ORCID iD: 0000-0001-9657-1921
SPIN-code: 5447-4090

Engineer of the Hydromechanical Engineering Laboratory of the Higher School of Power Engineering, Institute of Energy

Russian Federation, 29 Polytechnicheskaya street, 195251 Saint Petersburg

Sergei P. Fedorov

Peter the Great Saint Petersburg Polytechnic University; Power Machines

Email: fedorov_sp@power-m.ru
ORCID iD: 0000-0003-1426-7526
SPIN-code: 5071-5400

Postgraduate student, Head of the Design of Small Hydraulic Machines Department

Russian Federation, 29 Polytechnicheskaya street, 195251 Saint Petersburg; Saint Petersburg

References

  1. Shpil Yu. Trends in the development of feed pumps. Vestnik YuUrGU. 2005;1:32–46.
  2. Gulich JF. Centrifugal Pumps. Berlin, Heidelberg: Springer; 2010. doi: 10.1007/978-3-642-12824-0
  3. Lomakin AA. Centrifugal and axial pumps. Leningrad: Mashinostroenie; 1966.
  4. Bushziper P. Design concept of Sulzer feed pumps. Vestnik YuUrGU. 2005;1:65–72.
  5. Makay E., Szamody O. Survey of feedpump outages. Final report. Morrisville: Energy Re-search and Consultants Corporation; 1978. Report No.: 641. Contract No.: EPRI FP-754. Режим доступа: https://www.osti.gov/servlets/purl/7039347 дата обращения: 11.07.2022.
  6. Akimov S.V. Razrabotka metodov matematicheskogo modelirovaniya i povysheniya ener-goeffektivnosti neftyanykh magistralnykh nasosov putem modernizatsii poverkhnosti elementov protochnoy chasti [dissertation] St. Petersburg; 2022. doi: 10.18720/SPBPU/2/r22-3

Supplementary files

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2. Fig. 1. Schemes of the axial force balancing devices: a - disk, b – single-stage piston, c – two-stage piston.

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3. Fig. 2. Visualization of the studied simulated space for the single-stage piston.

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4. Fig. 3. Visualization of the simulation grid of the studied space for the two-stage piston.

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5. Fig. 4. Dependence of flow rate through the balancing piston on roughness at different values of radial clearance in the range from 0.15 to 0.25 mm.

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6. Fig. 5. Dependence of friction power losses of the balancing piston on roughness at different values of radial clearance in the range from 0.15 to 0.25 mm.

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7. Fig. 6. Dependence of total power losses of the balancing piston on roughness at different values of radial clearance in the range from 0.15 to 0.25 mm.

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8. Fig. 7. Dependence of total power losses (N), friction power losses (Nq) and overflow power losses (Nt) in the balancing piston on clearance value at the roughness value of Ra 25.

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Copyright (c) 2023 Zharkovsky A.A., Zakharov A.A., Fedorov S.P.

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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