A System Design and Demonstrative Field Test of Wind Turbine with a 14M Dia.Rotor

Material type: 文書・図像類

Author: 外立, 政隆ほか

Publisher: 航空宇宙技術研究所

Publication date: 1990-02

Material Format: Digital

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Note (General)：: The National Aerospace Laboratory participated in a comprehensive program for developing the technology of for conversion and storage of wind energy w...

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Material Type: 文書・図像類
Title: A System Design and Demonstrative Field Test of Wind Turbine with a 14M Dia.Rotor
Author/Editor: 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
Author Heading: 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
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1990-02
Publication Date (W3CDTF): 1990-02
Alternative Title: 直径14m風車のシステム設計とフィールド実証試験
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-1056
No. or year of volume/issue: 1056
Volume: 1056
Pages: 38-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): 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.
資料番号: NALTR1056000
レポート番号: NAL TR-1056
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ