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環状(アニュラ形)燃焼器高圧燃焼試験装置
https://jaxa.repo.nii.ac.jp/records/44794
https://jaxa.repo.nii.ac.jp/records/44794f791330e-62f5-4775-bea7-ee3ffb1e1045
名前 / ファイル | ライセンス | アクション |
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naltr00540.pdf (3.1 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 | 環状(アニュラ形)燃焼器高圧燃焼試験装置 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | High-Pressure Annular Combustor Test Facility at NAL | |||||
著者 |
鈴木, 邦男
× 鈴木, 邦男× 堀内, 正司× 松木, 正勝× 鳥崎, 忠雄× SUZUKI, Kunio× HORIUCHI, Shoji× MATSUKI, Masakatsu× TORISAKI, Tadao |
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著者所属 | ||||||
機械技術研究所 | ||||||
著者所属 | ||||||
元・航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所航空機公害研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所航空機公害研究グループ | ||||||
著者所属(英) | ||||||
en | ||||||
Former Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-540 巻 540, p. 24, 発行日 1978-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A facility for testing annular combustors for turbofan engines is operated in the National Aerospace Laboratory(Tokyo). The facility provides a maximum air-flow rate of 25kg/s and an operating pressure up to 15kg/cm2 abs. can be attained. An air-temperature of up to 723K at the combustor inlet is permitted. Special provision is taken at the facility to reduce both pollutants in the exhaust gas emissions, and noise, because the laboratory is situated in a residential district. The main features of the facility and the planning involved in its design are described. Construction of the facility was sponsored by the Ministry of International Trade and Industry, which is handling the National Project for development of a turbofan engine. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0540000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-540 |