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光ファイバセンサを用いた太陽電池パネルの健全性評価手法の開発
https://jaxa.repo.nii.ac.jp/records/21687
https://jaxa.repo.nii.ac.jp/records/21687696440a6-911e-4b0e-8ca5-d05f289e897d
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2016-03-28 | |||||
タイトル | ||||||
タイトル | 光ファイバセンサを用いた太陽電池パネルの健全性評価手法の開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Composite Materials | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Fiber Bragg Grating | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Solar Array Panel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Damage Detection | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Development of Health Monitoring Method for Solar Array Panel using Optical Fiber Sensors | |||||
著者 |
関根, 一史
× 関根, 一史× 松本, 迪斉× 竹谷, 元× 世古, 博巳× 小林, 裕希× 高橋, 眞人× 宇都宮, 真× Sekine, Kazushi× Matsumoto, Michihito× Takeya, Hajime× Seko, Hiromi× Kobayashi, Yuki× Takahashi, Masato× Utsunomiya, Shin |
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出版者 | ||||||
出版者 | Japan Society for Aeronautical and Space Sciences | |||||
出版者(英) | ||||||
出版者 | 日本航空宇宙学会 | |||||
書誌情報 |
日本航空宇宙学会論文集 en : Journal of the Japan Society for Aeronautical and Space Sciences 巻 64, 号 1, p. 6(6)-12(12), 発行日 2016-02-05 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | There is a concern that a thermal stress in a solar array panel under cryogenic environment would damage a solar cell and its interconnector, which might result in a drop of electrical power. Therefore it is important to perform the verification test on the ground to assure the healthiness of solar cells in orbit. In this study, we have developed the health monitoring method for solar array panel using Fiber Bragg Grating (FBG) sensor which is one of optical fiber sensors. In this paper, to reveal the thermal deformation behavior of the substrate composed of very thin Carbon Fiber Reinforced Plastics (CFRP) faceskin and aluminum honeycomb core in cryogenic environment, we measured the strain of CFRP faceskin near the center of honeycomb cell and showed that the depth of dimple increased linearly as temperature lowered. In addition, to confirm the effectiveness of our health monitoring method, we measured the internal strain of solar array panel and showed that we could detect its internal damage by strain change, and we observed the cross section of the damaged area and identified the damage point. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: 図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1344-6460 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11307372 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: DS1540529002 |