WEKO3
アイテム
{"_buckets": {"deposit": "1fe8d3e8-adf7-4090-87f4-46d430081aa7"}, "_deposit": {"created_by": 1, "id": "22712", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "22712"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00022712", "sets": ["1888"]}, "author_link": ["213120", "213117", "213118", "213119"], "item_7_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2015-09", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "109", "bibliographicPageStart": "102", "bibliographicVolumeNumber": "76", "bibliographic_titles": [{}, {"bibliographic_title": "Composites. Part A, Applied science and manufacturing", "bibliographic_titleLang": "en"}]}]}, "item_7_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "A Tyranno ZMI fiber/TiSi2-Si matrix composite was fabricated via melt infiltration (MI) of a Si-16at%Ti alloy at 1375 C under vacuum. The Si-Ti alloy was used as an infiltrant to conduct MI processing below 1400 C and inhibit the strength degradation of the amorphous SiC fibers. The alloy matrix formed was dense and comprised primarily of TiSi2-Si eutectic structures. The TiSi2-Si matrix composite melt-infiltrated at 1375 C showed a pseudo-plastic tensile stress-strain behavior followed by final fracture at ~290 MPa and ~0.9% strain. When the MI temperature was increased to 1450 C, however, substantial reduction in the stiffness and ultimate strength occurred under tensile loading. Microstructural observations revealed that these degradations were attributed to the damages that occurred on the reinforcing fibers and pyrolytic carbon interfaces during the MI process. The present experimental results clearly demonstrated the effectiveness of the low-temperature MI process in strengthening Tyranno ZMI fiber composites and reducing the processing cost.", "subitem_description_type": "Other"}]}, "item_7_description_18": {"attribute_name": "内容記述", "attribute_value_mlt": [{"subitem_description": "形態: カラー図版あり", "subitem_description_type": "Other"}]}, "item_7_description_19": {"attribute_name": "内容記述(英)", "attribute_value_mlt": [{"subitem_description": "Physical characteristics: Original contains color illustrations", "subitem_description_type": "Other"}]}, "item_7_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: PA1620007000", "subitem_description_type": "Other"}]}, "item_7_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Elsevier"}]}, "item_7_relation_25": {"attribute_name": "DOI", "attribute_value_mlt": [{"subitem_relation_name": [{"subitem_relation_name_text": "info:doi/10.1016/j.compositesa.2015.05.018"}], "subitem_relation_type_id": {"subitem_relation_type_id_text": "http://dx.doi.org/10.1016/j.compositesa.2015.05.018", "subitem_relation_type_select": "DOI"}}]}, "item_7_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1359-835X", "subitem_source_identifier_type": "ISSN"}]}, "item_7_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AA11069434", "subitem_source_identifier_type": "NCID"}]}, "item_7_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 学術雑誌論文"}]}, "item_7_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_7_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 10"}]}, "item_7_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "宇宙航空研究開発機構航空本部複合材技術研究センター(JAXA)"}, {"subitem_text_value": "宇宙航空研究開発機構航空本部複合材技術研究センター(JAXA)"}]}, "item_7_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Advanced Composite Research Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Advanced Composite Research Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"}]}, "item_access_right": {"attribute_name": "アクセス権", "attribute_value_mlt": [{"subitem_access_right": "metadata only access", "subitem_access_right_uri": "http://purl.org/coar/access_right/c_14cb"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "青木, 卓哉"}], "nameIdentifiers": [{"nameIdentifier": "213117", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "小笠原, 俊夫"}], "nameIdentifiers": [{"nameIdentifier": "213118", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Aoki, Takuya", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "213119", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ogasawara, Toshio", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "213120", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "A. Ceramic-matrix composites (CMCs)", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "B. Mechanical properties", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "B. Microstructures", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "E. Liquid metal infiltration", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}]}, "item_language": {"attribute_name": "言語", "attribute_value_mlt": [{"subitem_language": "eng"}]}, "item_resource_type": {"attribute_name": "資源タイプ", "attribute_value_mlt": [{"resourcetype": "journal article", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "Tyranno ZMI fiber/TiSi2-Si matrix composites for high-temperature structural applications", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Tyranno ZMI fiber/TiSi2-Si matrix composites for high-temperature structural applications", "subitem_title_language": "en"}]}, "item_type_id": "7", "owner": "1", "path": ["1888"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/22712", "pubdate": {"attribute_name": "公開日", "attribute_value": "2016-07-06"}, "publish_date": "2016-07-06", "publish_status": "0", "recid": "22712", "relation": {}, "relation_version_is_last": true, "title": ["Tyranno ZMI fiber/TiSi2-Si matrix composites for high-temperature structural applications"], "weko_shared_id": -1}
Tyranno ZMI fiber/TiSi2-Si matrix composites for high-temperature structural applications
https://jaxa.repo.nii.ac.jp/records/22712
https://jaxa.repo.nii.ac.jp/records/22712ab8f3f40-b0f4-4114-92b2-80af45021190
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-07-06 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Tyranno ZMI fiber/TiSi2-Si matrix composites for high-temperature structural applications | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | A. Ceramic-matrix composites (CMCs) | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | B. Mechanical properties | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | B. Microstructures | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | E. Liquid metal infiltration | |||||
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 | |||||
著者 |
青木, 卓哉
× 青木, 卓哉× 小笠原, 俊夫× Aoki, Takuya× Ogasawara, Toshio |
|||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部複合材技術研究センター(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部複合材技術研究センター(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Advanced Composite Research Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Advanced Composite Research Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者(英) | ||||||
出版者 | Elsevier | |||||
書誌情報 |
en : Composites. Part A, Applied science and manufacturing 巻 76, p. 102-109, 発行日 2015-09 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A Tyranno ZMI fiber/TiSi2-Si matrix composite was fabricated via melt infiltration (MI) of a Si-16at%Ti alloy at 1375 C under vacuum. The Si-Ti alloy was used as an infiltrant to conduct MI processing below 1400 C and inhibit the strength degradation of the amorphous SiC fibers. The alloy matrix formed was dense and comprised primarily of TiSi2-Si eutectic structures. The TiSi2-Si matrix composite melt-infiltrated at 1375 C showed a pseudo-plastic tensile stress-strain behavior followed by final fracture at ~290 MPa and ~0.9% strain. When the MI temperature was increased to 1450 C, however, substantial reduction in the stiffness and ultimate strength occurred under tensile loading. Microstructural observations revealed that these degradations were attributed to the damages that occurred on the reinforcing fibers and pyrolytic carbon interfaces during the MI process. The present experimental results clearly demonstrated the effectiveness of the low-temperature MI process in strengthening Tyranno ZMI fiber composites and reducing the processing cost. | |||||
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 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1359-835X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11069434 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1016/j.compositesa.2015.05.018 | |||||
関連名称 | info:doi/10.1016/j.compositesa.2015.05.018 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1620007000 |