WEKO3
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航空エンジン用燃料噴射弁評価のための高圧噴霧試験装置の開発
https://jaxa.repo.nii.ac.jp/records/2631
https://jaxa.repo.nii.ac.jp/records/263199a841b4-6240-4df5-ac25-fcbd1df3a87f
名前 / ファイル | ライセンス | アクション |
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63526000.pdf (8.4 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 航空エンジン用燃料噴射弁評価のための高圧噴霧試験装置の開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機エンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 性能試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃料噴射器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 評価 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高圧 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃料燃焼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ケロシン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃焼室 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | performance test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuel injector | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | evaluation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high pressure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuel combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | kerosene | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustion chamber | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Development of high-pressure spray test facility for evaluation of aero-engine fuel injector performance | |||||
著者 |
松浦, 一哲
× 松浦, 一哲× 黒澤, 要治× 山田, 秀志× 林, 茂× Matsuura, Kazuaki× Kurosawa, Yoji× Yamada, Hideshi× Hayashi, Shigeru |
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著者所属 | ||||||
宇宙航空研究開発機構 航空プログラムグループ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 航空プログラムグループ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 航空プログラムグループ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 航空プログラムグループ | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発資料 en : JAXA Research and Development Memorandum 巻 JAXA-RM-06-010, 発行日 2007-03-30 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper describes the development of a high-pressure spray test facility for performance evaluation of aero-engine fuel injectors. The facility provides test conditions of elevated inlet air-pressure up to 1 MPa. The maximal airflow rate is 1.2 kg/s at 0.8 MPa so that the facility is even capable of evaluating the performance of the next generation low emission burners based on lean premixed pre-vaporized combustion. The facility features a test section equipped with large high-pressure windows and an auxiliary air-purge system. The former gives optical access to various measurement techniques, and the latter keeps droplets away from the window surface and thus provides a clear view of sprays for a period sufficiently long for the measurements. The paper presents features and functions of the facility, together with some of the spray measurement techniques having been applied so far, along with examples of the measurement results. Suggestions for future work are also made, including those for further improvements of the facility. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1121 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11983593 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063526000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RM-06-010 |