Реверс-инжиниринг и численное моделирование течения вязкого газа ступени центробежного компрессора турбостартера ТС-21 для построения напорной характеристики с целью дальнейшей модернизации
https://doi.org/10.25206/2588-0373-2025-9-4-80-87
EDN: YCVDGE
Abstract
В работе представлены результаты 3D-сканирования геометрии проточной части центробежного компрессора ТС-21, а также результаты численного исследования течения вязкого газа в проточной части компрессора. Построены газодинамические характеристики компрессора на основе отсканированной оригинальной геометрии проточной части. Проведена оценка использования реверс-инжиниринга в энергетической и авиационной промышленности. Было выявлено, что помимо использования 3D-сканирования для лопаток рабочих колес необходимо проводить дополнительные операции, так как входные кромки лопаток получались более острые в результате погрешности обработки, вследствие чего возникает ударное обтекание и некорректное проектирование, модернизация промышленного и авиационного динамического оборудования.
About the Authors
A. P. Sheshukov
Peter the Great St. Petersburg Polytechnic University
Russian Federation
Russian Federation
Sheshukov Artem Pavlovich, Master's Student of the Higher School of Power Engineering
Russia, Saint Petersburg, Polytechnicheskaya St., 29, 195251
A. M. Yablokov
Peter the Great St. Petersburg Polytechnic University
Russian Federation
Russian Federation
Yablokov Aleksey Mikhaylovich, Senior Lecturer of the Higher School of Power Engineering
Russia, Saint Petersburg, Polytechnicheskaya St., 29, 195251
L. N. Маренина
Peter the Great St. Petersburg Polytechnic University
Russian Federation
Russian Federation
Marenina Lyubov Nikolaevna, Candidate of Technical Sciences, Senior Lecturer of the Higher School of Power Engineering
Russia, Saint Petersburg, Polytechnicheskaya St., 29, 195251
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Review
For citations:
Sheshukov A.P., Yablokov A.M., L.N. Реверс-инжиниринг и численное моделирование течения вязкого газа ступени центробежного компрессора турбостартера ТС-21 для построения напорной характеристики с целью дальнейшей модернизации. Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering. 2025;9(4):80-87. (In Russ.) https://doi.org/10.25206/2588-0373-2025-9-4-80-87. EDN: YCVDGE
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