Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet
- Authors: Stadnik D.M.1, Sverbilov V.Y.1, Makaryants G.M.1, Makaryants M.V.2
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Affiliations:
- Samara State Aerospace University
- Space Rocket Center "TsSKBProgress", Samara
- Issue: Vol 11, No 4 (2012)
- Pages: 184-192
- Section: MECHANICAL ENGINEERING AND POWER ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/2271
- DOI: https://doi.org/10.18287/2541-7533-2012-0-4(35)-184-192
- ID: 2271
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Abstract
The paper presents the analysis of the influence of a throttle installed at the inlet of a pilot-operated gas pressure control valve on the system dynamics in terms of providing the required accuracy and stability over a wide flow range.
About the authors
D. M. Stadnik
Samara State Aerospace University
Author for correspondence.
Email: sdm-63@bk.ru
Postgraduate Student, Engineer of the Department of Automatic Systems of Generating Units
Russian FederationV. Ya. Sverbilov
Samara State Aerospace University
Email: v.sverbilov@mail.ru
Candidate of Technical Science
Assоciate Professor of the Department of Automatic Systems of Generating Units
Russian FederationG. M. Makaryants
Samara State Aerospace University
Email: georgy.makaryants@gmail.ru
Candidate of Technical Science
Assоciate Professor of the Department of Automatic Systems of Generating Units
Russian FederationM. V. Makaryants
Space Rocket Center "TsSKBProgress", Samara
Email: mikhail.makaryants@gmail.ru
Chief of Division
Russian FederationReferences
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