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ビスマレイミド系耐熱複合材料の長期耐熱性評価
https://jaxa.repo.nii.ac.jp/records/48254
https://jaxa.repo.nii.ac.jp/records/48254cc2fa0ed-ac5c-47cd-9304-b34db0f9b011
名前 / ファイル | ライセンス | アクション |
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AA2130012000.pdf (4.2 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 | 2022-01-28 | |||||
タイトル | ||||||
タイトル | ビスマレイミド系耐熱複合材料の長期耐熱性評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 耐熱複合材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 評価 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ビスマレイミド系 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 三次元複合材 | |||||
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 | Long Term Durability of Bismaleimide Heat-Resistant Composite Materials | |||||
著者 |
高戸谷, 健
× 高戸谷, 健× 熊澤, 寿× TAKATOYA, Takeshi× KUMAZAWA, Hisashi |
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著者所属 | ||||||
宇宙航空研究開発機構航空技術部門航空システム研究ユニット(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空技術部門構造・複合材技術研究ユニット(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Aviation Systems Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Structures and Advanced Composite Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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研究開発資料 en : JAXA Research and Development Memorandum 巻 JAXA-RM-21-005, p. 1-13, 発行日 2022-01-28 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 耐熱複合材料を超音速機やエンジン周辺の構造に適用するための力学特性を明らかにすることを目標として、耐熱樹脂としてビスマレイミド系樹脂に着目し、高温曝露が有孔圧縮強度に及ぼす影響を評価した。本報告で高温曝露した温度では、長期の高温曝露で強度が大幅に低下することが明らかになった。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | As a conventional epoxy resin system had not enough heat endurance, new heat-resistant resin systems were needed to be developed in the aircraft use, such as supersonic transport structure, the parts around the jet engines and so on. In this report, fundamental properties of the bismaleimide heat-resistant resin system with the three-dimensional textile composite are characterized under room temperature condition. After long-term high temperature expose, the open hole compressive test was carried out and strength properties were obtained. The result showed that the strength was largely decreased under high temperature long term exposure conditions. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2224 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2130012000 | |||||
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-RM-21-005 |