Smagin Denis Igorevich (Head of the laboratory, Moscow Aviation Institute (National Research University))
Starostin Konstantin Igorevich (Principal engineer, Moscow Aviation Institute (National Research University))
Savelyev Roman Sergeevich (Principal engineer, Moscow Aviation Institute (National Research University))
Napreenko Konstantin Sergeevich (Category 2 engineer, Moscow Aviation Institute (National Research University))
Vasiliev Nikolay Georgievich (Technician, Moscow Aviation Institute (National Research University))
Krasavin Yegor Eduardovich (Technician, Moscow Aviation Institute (National Research University))
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The article considers a mathematical model of an air conditioning system for a promising medium-haul aircraft. The key feature of this system is the use of an electric centrifugal air compressor as a source of compressed air. The methodology for determining the design parameters of an air compressor based on the results of modeling the air conditioning system in several modes is shown.
Keywords:mathematical model, air conditioning system, centrifugal compressor, air cooling unit, air cycle, compression–evaporation cycle.
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Citation link: Smagin D. I., Starostin K. I., Savelyev R. S., Napreenko K. S., Vasiliev N. G., Krasavin Y. E. Method for determining the design parameters of a centrifugal air compressor based on a mathematical model of a non-selective air conditioning system // Современная наука: актуальные проблемы теории и практики. Серия: Естественные и Технические Науки. -2020. -№10. -С. 115-121 DOI 10.37882/2223-2966.2020.10.28 |
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