The analysis of temperature regime of low-speed stage with change in ratio of time and return stroke of piston

Authors

  • Vladimir Leonidovich Yusha Omsk State Technical University, Omsk, Russia https://orcid.org/0000-0001-9858-7687
  • Sergey Sergeevich Busarov Omsk State Technical University, Omsk, Russia
  • Aleksey Vasilievich Nedovenchany Omsk State Technical University, Omsk, Russia

DOI:

https://doi.org/10.25206/2588-0373-2018-2-4-21-28

Keywords:

linear drive, the law of motion, low-speed long stroke piston compressor, forward and reverse stroke workflow, adjustable drive

Abstract

The paper presents theoretical studies on the control of a linear hydraulic drive by changing the ratio of compression time (forward stroke) and suction time (return stroke). The effect of the operating mode of the drive on the efficiency of the working cycle is estimated.

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Author Biographies

Vladimir Leonidovich Yusha, Omsk State Technical University, Omsk, Russia

Doctor of Technical Sciences, Professor, Head of Refrigeration and Compressor Engineering and Technology Department.

Sergey Sergeevich Busarov, Omsk State Technical University, Omsk, Russia

Candidate of Technical Sciences, Associate Professor of Refrigeration and Compressor Engineering and Technology Department.

Aleksey Vasilievich Nedovenchany, Omsk State Technical University, Omsk, Russia

Graduate Student of Refrigeration and Compressor Engineering and Technology Department.

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Abstract views: 9

Published

2018-12-20

How to Cite

Yusha В. Л., Busarov С. С., & Nedovenchany А. В. (2018). The analysis of temperature regime of low-speed stage with change in ratio of time and return stroke of piston. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 2(4), 21–28. https://doi.org/10.25206/2588-0373-2018-2-4-21-28

Issue

Vol. 2 No. 4 (2018)

Section

Power and chemical engineering

License

Non-exclusive rights to the article are transferred to the journal in full accordance with the Creative Commons License BY-NC-SA 4.0 «Attribution-NonCommercial-ShareAlike 4.0 Worldwide License (CC BY-NC-SA 4.0»)

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