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複合接着構造の破壊力学特性の温度依存性評価:宇宙機構造技術の研究
https://jaxa.repo.nii.ac.jp/records/6257
https://jaxa.repo.nii.ac.jp/records/62572af7a81b-8ccb-495d-8dc5-3484919f54c1
名前 / ファイル | ライセンス | アクション |
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49054001.pdf (1.5 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 | 複合接着構造の破壊力学特性の温度依存性評価:宇宙機構造技術の研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機構造材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軽量宇宙構造物 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 複合材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱応力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 応力-歪関係 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱膨張 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 接着結合ジョイント | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アルミニウム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極低温 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft construction material | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | light-weight space structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | composite material | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal stress | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stress-strain relationship | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal expansion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | adhesively bonded joint | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aluminum | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cryogenic temperature | |||||
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 | Temperature-dependent fracture performance for multiphase bond structures: Research on space structural technology | |||||
著者 |
He, Jianmei
× He, Jianmei× 下田, 孝幸× He, Jianmei× Shimoda, Takayuki |
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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(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
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16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems 巻 JAXA-SP-05-008, p. 3-6, 発行日 2006-01-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Adhesively-bonded structure between advanced CFRP composites and aluminum metal (A1) plays an important role in the development of a lightweight space structure. Accurately understanding the temperature-dependent fracture behaviors of such multiphase bond structures is very important from design safety and durability viewpoints. Substantial thermal stress-strain, which is caused by the mismatch of thermal expansion ratios between adhesives, CFRP composites and aluminum metal could lead to the strength deterioration of such multiphase bond structures over a wide temperature range. In this study, temperature-dependent Mode-2 fracture performance of adhesively-bonded joints between CFRP and A1 was experimentally investigated using a candidate structure adhesive film named AF 163-2K. | |||||
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: AA0049054001 | |||||
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-05-008 |