PROSPECTS FOR THE DEVELOPMENT OF GAS TURBINE TECHNOLOGY ON THE BASIS OF ACHIEVEMENTS IN THE AIRCRAFT ENGINE INDUSTRY (ON THE 100TH ANNIVERSARY OF THE BIRTH OF V. N. YERSHOV)

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J. of Mech. Eng., 2017, vol. 20, no. 4, pp. 12-14

DOI:   https://doi.org/10.15407/pmach2017.04.012

Journal Journal of Mechanical Engineering
Publisher A. Podgorny Institute for Mechanical Engineering Problems
National Academy of Science of Ukraine
ISSN 0131-2928 (Print), 2411-0779 (Online)
Issue Vol. 20, no. 4, 2017 (December)
Pages 12–14

 

Authors

V. P. Gerasimenko, National Aerospace University “KhAI” (17 Chkalov St., Kharkov, 61070, Ukraine), e-mail: boyko@d2.khai.edu

M. Yu. Shelkovskiy, Zorya-Mashproekt Gas Turbine Research and Development Complex (42-a, Bohoyavlenskyy Ave., Mykolaiv, 54018, Ukraine), e-mail: maikl.shelkovsy@gmail.com

 

Abstract

This paper considers a significant contribution to the improvement of compressors by scientific schools, founded by Academician G. F. Proskura and his student – Honored Worker of Higher Education of Ukraine, Doctor of Technical Science, Professor V. N. Yershov. It is shown that specific speed is a fairly convenient sign of recognition of the type and optimal shape of a compressor impeller, pump, fan, to ensure its maximum efficiency, the necessary pressure, and air consumption.

 

Keywords: compressor, efficiency, speed ratio, blade elongation

 

References

  1. Kampsti, N. (2000). Ajerodinamika kompressorov. Moscow: Mir, 688 p.
  2. Ovsjannikov, B. V. & Borovskij, B. I. (1971). Teorija i raschet agregatov pitanija zhidkostnyh raketnyh dvigatelej. Moscow: Mashinostroenie, 540 p.
  3. Jekkert, B. (1959). Osevye i centrobezhnye kompressory. Primenenie, teorija, raschet. Moscow: Mashgiz, 679 p.
  4. Horlok, Dzh. H. (1972). Osevye turbiny (gazovaja dinamka i termodinamika). Moscow: Mashinostroenie, 344 p.

 

Received 02 November 2017