Experimental study of cyclone filters of pneumatic automatic control system of gas turbine engine for increasing degree of purification

Authors

  • Nikolaj Vitalievich Vologodskij Joint-stock company «Omsk Machine-Building Design Bureau», Russia, Omsk
  • Andrey Vadimovich Pronevich Joint-stock company «Omsk Machine-Building Design Bureau», Russia, Omsk
  • Aleksey Borisovich Yakovlev Omsk State Technical University, Omsk, Russia https://orcid.org/0000-0002-1987-2138

DOI:

https://doi.org/10.25206/2588-0373-2020-4-3-101-109

Keywords:

aircraft engine, pneumatic systems, separation, centrifugal dust collector, cleaning degree

Abstract

An experimental study of cyclone filters of various designs is conducted. The parameters that allow increasing the degree of air purification from dust are identified: air pressure at the filter inlet, working air temperature, as well as the diameter of the nozzle of the purified air consumer simulator and the diameter of the ventilation nozzle. The results obtained make it possible to increase the reliability of pneumatic units and reduce the erosive wear of their working cavities.

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Author Biographies

Nikolaj Vitalievich Vologodskij, Joint-stock company «Omsk Machine-Building Design Bureau», Russia, Omsk

Lead Designer, Head of 21 Teams of the Design Department, JSC «Omsk Machine-Building Design Bureau».

Andrey Vadimovich Pronevich, Joint-stock company «Omsk Machine-Building Design Bureau», Russia, Omsk

Test Engineer, 21 Teams of the Design Department, JSC «Omsk Machine-Building Design Bureau».

Aleksey Borisovich Yakovlev, Omsk State Technical University, Omsk, Russia

Candidate of Technical Sciences, Associate Professor, Head of Aircraft and Rocket Engineering Department, Omsk State Technical University.

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Abstract views: 24

Published

2020-10-20

How to Cite

Vologodskij Н. В., Pronevich А. В., & Yakovlev А. Б. (2020). Experimental study of cyclone filters of pneumatic automatic control system of gas turbine engine for increasing degree of purification. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 4(3), 101–109. https://doi.org/10.25206/2588-0373-2020-4-3-101-109

Issue

Section

Aviation and rocket-space engineering