{"created":"2023-06-20T14:35:42.090567+00:00","id":1978,"links":{},"metadata":{"_buckets":{"deposit":"07fe85eb-b01f-4298-9216-30321ebe5678"},"_deposit":{"created_by":1,"id":"1978","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"1978"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00001978","sets":["1887:1893","9:10:75:84"]},"author_link":["1994","1995","1993","1992"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Mechanical Evaluation of Polycyanate Heat-Resistant Composite Materials for Supersonic Transport Structures"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-10-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"43","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-13-003","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"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，耐熱樹脂としてポリシアネート系樹脂に着目し，引張・有孔引張・有孔圧縮・層間せん断試験を実施し強度データを取得するとともに，高温および高温曝露が強度に及ぼす影響を評価した．さらに，得られた基礎データを元に，静粛超音研究機の構造要素としてラダーを想定したサブコンポーネントを設計・製作・評価してその妥当性を検証したところ，変形量など検討の余地があるものの検討すべき技術課題は解決できたと考えており，耐熱樹脂の有用性確認できた成果について報告する．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"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 polycyanate heat-resistant resin system with the three dimensional textile composite are characterized under room temperature and high temperature conditions. The tensile, open hole tensile, open hole compressive, and double notch shear test were carried out and stiffness and strength properties were obtained. After that, the scale model of the rudder in the silent supersonic technology demonstrator was designed using the obtained properties, manufactured and evaluated. The result showed that this resin system had a capability of the application of the aircraft structures under high temperature conditions.","subitem_description_type":"Other"}]},"item_3_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_3_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_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0062050000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RR-13-003","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_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機体システム研究グループ(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空本部構造技術研究グループ(JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aircraft Systems Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Structures Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高戸谷, 健"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"熊澤, 寿"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takatoya, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kumazawa, Hisashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-15"}],"displaytype":"detail","filename":"62050000.pdf","filesize":[{"value":"15.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"62050000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/1978/files/62050000.pdf"},"version_id":"2deb7584-1c06-4c1e-995e-9f1d54392f63"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"耐熱複合材料","subitem_subject_scheme":"Other"},{"subitem_subject":"評価","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速機","subitem_subject_scheme":"Other"},{"subitem_subject":"ポリシアネート系","subitem_subject_scheme":"Other"},{"subitem_subject":"三次元複合材","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"超音速機の構造材料用ポリシアネート系耐熱複合材料の力学特性評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速機の構造材料用ポリシアネート系耐熱複合材料の力学特性評価"}]},"item_type_id":"3","owner":"1","path":["84","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"1978","relation_version_is_last":true,"title":["超音速機の構造材料用ポリシアネート系耐熱複合材料の力学特性評価"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:31:09.729292+00:00"}