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アクティブ制御による振動燃焼の抑制
https://jaxa.repo.nii.ac.jp/records/6028
https://jaxa.repo.nii.ac.jp/records/6028d2fe083b-3f67-44b1-9fb2-1b51a169faf6
名前 / ファイル | ライセンス | アクション |
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49500044.pdf (1.1 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 | アクティブ制御による振動燃焼の抑制 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃焼振動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動燃焼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ガスタービン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃焼室 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 与混合炎 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 希薄燃焼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 火炎安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃焼制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 能動制御 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustion vibration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustion-driven oscillation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gas turbine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustion chamber | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | premixed flame | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lean combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flame stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustion control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | active control | |||||
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 | Active control of combustion-driven oscillations in a gas-turbine combustor | |||||
著者 |
立花, 繁
× 立花, 繁× Zimmer, Laurent× 黒澤, 要治× 鈴木, 和雄× Tachibana, Shigeru× Zimmer, Laurent× Kurosawa, Yoji× Suzuki, Kazuo |
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著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
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 総合技術研究本部 事業推進部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Program Management and Integration Department, Institute of Aerospace Technology | ||||||
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特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 en : JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency 巻 JAXA-SP-06-006, p. 201-206, 発行日 2006-11-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An active control of combustion driven oscillations occurring in a lean premixed model combustor is demonstrated by means of a secondary fuel injection. An unstable condition, which leads to self-excited pressure oscillations beyond 170 dB, is chosen as control target. Keeping the inlet air temperature, the air mass flow rate and the overall equivalence ratio, respectively, at 700 K, 78 g/s and 0.50, different secondary fuel injection strategies are examined. One is a steady injection method and the other is a feedback control, which was designed by the mixed H(sup 2)/H(sup infinity) control algorithm. The feedback control with three percent of secondary fuel performs peak pressure reduction of 27 dB, which is almost 10 dB larger than that of the steady injection method. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049500044 | |||||
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-SP-06-006 |