Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet

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

Russian Federation

Postgraduate Student, Engineer of the Department of Automatic Systems of Generating Units

V. Ya. Sverbilov

Samara State Aerospace University

Email: v.sverbilov@mail.ru

Russian Federation

Candidate of Technical Science

Assоciate Professor of the Department of Automatic Systems of Generating Units

G. M. Makaryants

Samara State Aerospace University

Email: georgy.makaryants@gmail.ru

Russian Federation

Candidate of Technical Science

Assоciate Professor of the Department of Automatic Systems of Generating Units

M. V. Makaryants

Space Rocket Center "TsSKBProgress", Samara

Email: mikhail.makaryants@gmail.ru

Russian Federation

Chief of Division

References

  1. Моль, Р. Гидропневмоавтоматика [Текст] / Р. Моль; пер. с франц. - М.: Машиностроение, 1975. - 352 с.
  2. Залманзон, Л. А. Теория элементов пневмоники [Текст] / Л. А. Залманзон. - М.: Наука, 1969. - 508 с.
  3. Шорин, В. П. Correcting Devices for Control Systems [Текст] / В. П. Шорин, В. Я. Свербилов, Г. В. Шестаков // Proceedings of the Third JHPS International Symposium on Fluid Power: сб. науч. тр. / Yokohama, 1996. - С. 597-601.

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