Combustion chamber temperature distribution of Gas Generator for GG-ATR engine
| Autor: | FUJIURA, Akitomo, NAMERA, Mio, NAKAMURA, Yuta, NAKATA, Daisuke, EGUCHI, Hikaru, UCHIUMI, Masaharu |
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| Jazyk: | japonština |
| Rok vydání: | 2023 |
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| Zdroj: | 令和4年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2022. |
| Popis: | 令和4年度宇宙輸送シンポジウム（2023年1月12日-13日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)) , 相模原市, 神奈川県 Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan Muroran Institute of Technology is conducting research and development of a Gas Generator Cycle Air Turbo Ramjet (GG-ATR) Engine as a propulsion system for small unmanned supersonic aircraft. A temperature deviation exists inside the combustion chamber of the gas generator installed in this engine. Therefore, we installed elbows, which are known to be effective in improving temperature distribution to confirm the temperature uniformity effect of the elbows. As a result, it was confirmed that the elbow improved the combustion gas temperature by 630K. 資料番号: SA6000184028 STCP-2022-028 |
| Databáze: | OpenAIRE |
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