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Development of anti-coking thermal management technologies for a coaxially-staged lean-burn fuel injector for high-pressure-ratio aero-engines.: First report: Evaluation of thermal protection performance and validation of numerical analysis by experiments in realistic environments.
https://doi.org/10.20637/0002001693
https://doi.org/10.20637/0002001693391d9474-2a7f-41ac-9afa-000767873a8d
名前 / ファイル | ライセンス | アクション |
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Item type | WEKO3_JAXA出版物 / JAXA Publication(1) | |||||||||||||
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公開日 | 2025-02-27 | |||||||||||||
タイトル | ||||||||||||||
タイトル | Development of anti-coking thermal management technologies for a coaxially-staged lean-burn fuel injector for high-pressure-ratio aero-engines.: First report: Evaluation of thermal protection performance and validation of numerical analysis by experiments in realistic environments. | |||||||||||||
言語 | en | |||||||||||||
言語 | ||||||||||||||
言語 | eng | |||||||||||||
キーワード | ||||||||||||||
主題 | Fuel injector design, Lean staged combustor, Injector thermal management, Fuel coking, Thermal oxidation, Aero-engines, Large eddy simulation, Additive manufacturing | |||||||||||||
資源タイプ | ||||||||||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||||||||||
資源タイプ | technical report | |||||||||||||
ID登録 | ||||||||||||||
ID登録 | 10.20637/0002001693 | |||||||||||||
ID登録タイプ | JaLC | |||||||||||||
アクセス権 | ||||||||||||||
アクセス権 | open access | |||||||||||||
アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||||||||||
著者 |
松浦, 一哲
× 松浦, 一哲
× 山本, 武
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著者所属 | ||||||||||||||
著者所属 | En-Core Project Team, Aviation Technology Directorate, Japan Aerospace Exploration Agency (JAXA)(en), En-Core Project Team, Aviation Technology Directorate, Japan Aerospace Exploration Agency (JAXA)(en) 宇宙航空研究開発機構航空技術部門コアエンジン技術実証(En-Core)プロジェクトチーム (JAXA)(ja), 宇宙航空研究開発機構航空技術部門コアエンジン技術実証(En-Core)プロジェクトチーム (JAXA)(ja) |
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出版者 | ||||||||||||||
出版者 | Japan Aerospace Exploration Agency (JAXA)(en) 宇宙航空研究開発機構 (JAXA)(ja) |
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bibliographic_information |
en : JAXA Research and Development Memorandum ja : 宇宙航空研究開発機構研究開発資料 巻 JAXA-RM-24-008E, ページ数 42, 発行日 2025-02-27 |
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抄録 | ||||||||||||||
内容記述タイプ | Other | |||||||||||||
内容記述 | A coaxially-staged lean-burn fuel injector for aero-engines was developed, which was equipped with anti-coking thermal management function. Solid/fluid conjugate heat transfer numerical simulations were performed to evaluate its thermal protection performance. It was shown that the injector of the current design satisfied our criterion, that is, the wet-wall temperatures of its fuel circuits were below 478K, except the regions close to its injection exits. Experiments were also conducted to evaluate the validity of the simulations. At the probe locations where the temperatures were measured, the results of them by the simulations and by the experiments were in good agreement, showing reliability of the simulations for the evaluation of injector performance. In this first report, the main contents are descriptions of numerical/experimental procedures and the results for the injector with one of successful designs in terms of thermal protection. The concept of thermal management design of the injector and its manufacturing process including additive manufacturing are also mentioned briefly. | |||||||||||||
言語 | en | |||||||||||||
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内容記述タイプ | Other | |||||||||||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||||||||||
言語 | en | |||||||||||||
内容記述 | ||||||||||||||
内容記述タイプ | Other | |||||||||||||
内容記述 | 形態: カラー図版あり | |||||||||||||
言語 | ja | |||||||||||||
ISSN ONLINE | ||||||||||||||
収録物識別子タイプ | EISSN | |||||||||||||
収録物識別子 | 2433-2224 | |||||||||||||
出版タイプ | ||||||||||||||
出版タイプ | VoR | |||||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||||
日付 | ||||||||||||||
日付 | 2024-11-29 | |||||||||||||
日付タイプ | Submitted | |||||||||||||
資料番号(Local) | ||||||||||||||
関連識別子 | 資料番号: AA2430024000 | |||||||||||||
レポート番号 | ||||||||||||||
内容記述 | レポート番号: JAXA-RM-24-008E |