Simulation of the work process of a two-stage pump with a first-stage hydraulic drive
- Authors: Matveev V.N.1, Shabliy L.S.1, Krivtsov A.V.1, Zubanov V.M.1, Ivanov A.I.2, Kositsin I.P.2, Baturin N.V.2
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Affiliations:
- Samara National Research University
- «KUZNETSOV» public company, Samara
- Issue: Vol 15, No 4 (2016)
- Pages: 102-113
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/3315
- DOI: https://doi.org/10.18287/2541-7533-2016-15-4-102-113
- ID: 3315
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Abstract
This article describes a method of CFD-modeling of a two-stage high-pressure pump. The main feature of the pump is the hydraulic drive of the low-pressure stage that takes energy from a high-pressure flow. The speed of the turbine is determined by the power balance of a low-pressure rotor. The modeling technique presented in this paper includes two major advantages over previous studies. The first feature is the determination of the speed of rotational velocity during the CFD-calculation by a special methodology. The second feature is cavitation simulation to assess its impact on the pre-pump workflow at a relatively low inlet pressure. Recommendations for the use of software (ANSYS CFX, NUMECA AutoGrid5, ANSYS ICEM CFD) are an important part of the simulation technology described. These recommendations concern the choice of the modeling area, mesh generation, choice of turbulence models, verification of convergence, post-processing of the results. The adequacy of the CFD-model was evaluated by comparing the calculated and experimental performance obtained on a test rig. The use of the resulting methodology of pump simulation improves the productivity and increases the efficiency of pumps with a hydro-drive of the low-pressure stage.
Keywords
About the authors
V. N. Matveev
Samara National Research University
Author for correspondence.
Email: valeriym2008@rambler.ru
Doctor of Science (Engineering)
Professor of the Department of Aircraft Engine Theory
L. S. Shabliy
Samara National Research University
Email: mlbp@yandex.ru
Candidate of Science (Engineering)
Associate professor of the Department of Aircraft Engine Theory
A. V. Krivtsov
Samara National Research University
Email: a2000009@rambler.ru
Assistant Lecturer of the Department of Aircraft Engine Theory
Russian FederationV. M. Zubanov
Samara National Research University
Email: waskes91@gmail.com
Assistant Lecturer of the Department of Aircraft Engine Theory
Russian FederationA. I. Ivanov
«KUZNETSOV» public company, Samara
Email: alex_slavross@mail.ru
Head of the Department of Rocket Engines
Russian FederationI. P. Kositsin
«KUZNETSOV» public company, Samara
Email: alex_slavross@mail.ru
Candidate of Science (Engineering)
leading engineer
N. V. Baturin
«KUZNETSOV» public company, Samara
Email: nik-o-las@mail.ru
leading engineer
Russian FederationReferences
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