Use of experimental and numerical simulation methods for rational design of the air cooling apparatus for lubrication systems of compressors
https://doi.org/10.29235/1561-8358-2020-65-2-215-223
Abstract
The objective of the present work was to study heat and hydraulic parameters of an air cooling apparatus of oil (ACAO), whose geometry of its flow-through part is changed to decrease hydraulic losses in its air conduit and to increase the cooling efficiency of oil. Using numerical simulation methods of heat transfer, we have developed and tested the computational techniques applied in a wide class of heat exchange apparatuses, including those consisting of the sections of finned flat tubes manufactured by extrusion with subsequent deforming cutting. We have proposed to make a finned part of a heat-exchange surface in the form of porous inserts. This has allowed us to reduce numerical simulation equipment requirements and to decrease computational time. Predicted results well agree with experimental data; their analysis shows that the calculated value of thermal performance of the oil cooler due to the revealed construction drawbacks of the air conduit is by 19 % less than that of the designed one. Based on the results of the numerical simulation studies, a number of recommendations have been made how to improve the layout inside the air cooling apparatus for oil in order to enhance its thermal performance and aerodynamic quality. In particular, we have proposed to mount new fan blades to enhance its performance; to change the construction of the air outlet valve by taking away a baffle that partially overshadows the exit area of the bottom fan; to modify the shape of the bottom collector of the oil cooler in order to make a uniform velocity profile at the entrance of cooling sections. Connecting in series heat exchange sections may be a perspective engineering decision. The outcomes of all proposed engineering decisions can be assessed by numerical simulation methods that will allow us not to design expensive equipment.
About the Authors
M. V. GureevRussian Federation
Mikhail V. Gureev – Research Associate
10, K. Marx Str., 420111, Kazan
I. I. Khabibullin
Russian Federation
Ilmir I. Khabibullin – Ph. D. (Engineering), Leading Engineer
10, K. Marx Str., 420111, Kazan
40, Siberian Tract, 420029, Kazan
A. N. Skrypnik
Russian Federation
Artyom N. Skrypnik – Postgraduate Student, Assistant
10, K. Marx Str., 420111, Kazan
G. S. Marshalova
Belarus
Galina S. Marshalova – Scientific Researcher, Laboratory of Turbulence; Ph. D. (Engineering), Junior Researcher
13a, Sverdlov Str., 220006, Minsk
15, P. Brovka Str., 220072, Minsk
I. A. Popov
Russian Federation
Igor A. Popov – Corresponding Member of the Academy of Sciences of the Republic of Tatarstan, D. Sc. (Engineering), Professor
10, K. Marx Str., 420111, Kazan
R. G. Kadyrov
Russian Federation
Ruslan G. Kadyrov – Postgraduate Student
10, K. Marx Str., 420111, Kazan
V. M. Gureev
Russian Federation
Viktor M. Gureev – D. Sc. (Engineering), Professor
10, K. Marx Str., 420111, Kazan
A. D. Chorny
Belarus
Andrei D. Chorny – Ph. D. (Physics and Mathematics), Associate Professor, Head of the Laboratory of Turbulence
15, P. Brovka Str., 220072, Minsk
Y. V. Zhukova
Belarus
Yuliya V. Zhukova – Ph. D. (Physics and Mathematics), Associate Professor, Leading Researcher, Laboratory of Turbulence
15, P. Brovka Str., 220072, Minsk
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