Samara University Repository
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This is an open electronic archive created to preserve and disseminate the scientific results of our university. The works of researchers, faculty members, and students are available to everyone for academic and research purposes.
The repository contains dissertations, research articles, educational and methodological materials, monographs, and regulatory documents. The collections cover a wide range of fields: from aerospace technologies, engine engineering, and computer science to history, linguistics, mathematics, and ecology. The archive brings together the scientific heritage of the university, including materials prepared during the period of Samara State Aerospace University and Samara State University.
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| Title: | Применение параметрического оптимизатора для достижения требуемых прочностных характеристик диска турбины |
| Authors: | Селищев П. А. Зеленкевич А. Д. Столь О. В. |
| Keywords: | cyclic durability finite element modeling free turbines gas turbine engines parametric optimization plastic deformations rotor calculation models strength characteristics stress concentrators turbine disk configuration газотурбинные двигатели конечно-элементное моделирование конфигурация диска турбины концентраторы напряжений параметрическая оптимизация пластические деформации прочностные характеристики расчетные модели ротора свободные турбины циклическая долговечность |
| Issue Date: | 2025 |
| Citation: | Селищев, П. А. Применение параметрического оптимизатора для достижения требуемых прочностных характеристик диска турбины = Application of parametric optimizer to achieve required strength characteristics of turbine disk / П. А. Селищев, А. Д. Зеленкевич, О. В. Столь // Перспективы развития двигателестроения : материалы междунар. науч.-техн. конф. им. Н. Д. Кузнецова (18–20 июня 2025 г.) / Самар. нац. исслед. ун-т им. С. П. Королева (Самар. ун-т) ; редкол.: Е. В. Шахматов, А. И. Ермаков. - Самара : Изд-во Самар. ун-та, 2025. - С. 218-220. |
| Abstract: | Some of the main strength characteristics of the rotary parts of a gas turbine engine (GTE) are: reserves of local static strength, bearing capacity and cyclic durability. The object of the study is the disk of the first stage of the free turbine (FT) of the GTE. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43306 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-218-220.pdf | 376.14 kB | Adobe PDF | View/Open |
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