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: | Перспективные средства измерения температуры в авиационных ГТД |
| Authors: | Новосадов Д. А. Загадов И. А. |
| Keywords: | пирометрия онлайн методы измерения монокристаллические датчики температуры измерение температуры автономные методы измерения авиационные газотурбинные двигатели термокраска термографические люминофоры стеклокерамические решетки системы реального времени системы мониторинга температуры online measurement methods offline measurement methods glass ceramic gratings aviation industry aircraft gas turbine engines авиационная отрасль thermographic phosphors thermal paint temperature monitoring systems temperature measurement single crystal temperature sensors real time systems pyrometry |
| Issue Date: | 2025 |
| Citation: | Новосадов, Д. А. Перспективные средства измерения температуры в авиационных ГТД = Promising temperature measurement technologies for aviation gas turbine engines / Д. А. Новосадов, И. А. Загадов // 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. 47-49. |
| Abstract: | The paper reviews advanced temperature measurement methods for the hot section of aviation gas turbine engines. Real-time and autonomous systems are considered, including thermal paints, pyrometers, thermocouples, and thermographic phosphors. Key advantages, limitations, and potential combined use are discussed, with focus on applicability in confined engine environments. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43181 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-47-49.pdf | 408.89 kB | Adobe PDF | View/Open |
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