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: | Методология выполнения перфорационных отверстий пленочного охлаждения сложной формы |
| Authors: | Коннов И. А. Ефремов Д. В. Беляева М. В. Некрасов В. И. |
| Keywords: | aircraft gas turbine engines electrical discharge machining fan holes film cooling high pressure turbines hole profiling perforation profiled electrode assembly tooling turbine nozzle blades авиационные газотурбинные двигатели веерные отверстия оснастка перфорация пленочное охлаждение профилирование отверстий сборка профилированных электродов сопловые лопатки турбин турбины высокого давления электроэрозионная обработка |
| Issue Date: | 2025 |
| Citation: | Методология выполнения перфорационных отверстий пленочного охлаждения сложной формы = Methodologe for making complex shaped film cooling holes / И. А. Коннов, Д. В. Ефремов, М. В. Беляева, В. И. Некрасов // 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. 381-385. |
| Abstract: | The implementation of advanced nozzle blade sections necessitates novel approaches to designing highly efficient film cooling systems. The article presents a method for manufacturing shape-film cooling holes in the nozzle blade sections of the HPT for modern GTE. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43341 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-381-385.pdf | 727.07 kB | Adobe PDF | View/Open |
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