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A System Design and Demonstrative Field Test of Wind Turbine with a 14M Dia.Rotor
https://jaxa.repo.nii.ac.jp/records/45315
https://jaxa.repo.nii.ac.jp/records/45315d3552989-e338-4e4e-8400-9e15995273c9
名前 / ファイル | ライセンス | アクション |
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naltr01056.pdf (4.1 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 | ||||||
言語 | en | |||||
タイトル | A System Design and Demonstrative Field Test of Wind Turbine with a 14M Dia.Rotor | |||||
言語 | ||||||
言語 | eng | |||||
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 | ||||||
その他のタイトル | 直径14m風車のシステム設計とフィールド実証試験 | |||||
著者 |
外立, 政隆
× 外立, 政隆× 伊藤, 忠× 半沢, 麻雄× 野中, 修× 野原, 利雄× 小松, 行夫× 遠藤, 浩× HASHIDATE, Masataka× ITO, Tadashi× HANZAWA, Asao× NONAKA, Osamu× NOHARA, Toshio× KAMATSU, Yukio× ENDO, Hiroshi |
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著者所属 | ||||||
航空宇宙技術研究所空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所機体部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空力性能部 | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Airframe Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division, 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-1056 巻 1056, p. 38, 発行日 1990-02 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The National Aerospace Laboratory participated in a comprehensive program for developing the technology of for conversion and storage of wind energy which was promoted by the Science and Technology Agency of Japan, undertaking the research and development of a horizontal axis type wind turbine with a 14m dia.rotor. This report describes the system design and the ground-based hybrid dynamic simulation and the demonstrative field test of the 14m Wind Turbine. The test results confirm the following excellent characteristics. 1)The minimum operational wind speed is as low as 3m/s. 2)The rotational speed is kept almost constant within the accuracy of ±4 min-1. 3)The output-power is 22kW on the rotor axis at the rated wind speed of 8m/s. 4)The maximum aerodynamics power coefficient is about 48% at the operational pitch angle. 5)The maximum rate of heat generation is 5.2×10(exp 4) kJ/hr at a wind speed of 10m/s. | |||||
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: NALTR1056000 | |||||
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-1056 |