{"created":"2023-06-20T15:10:09.883724+00:00","id":39765,"links":{},"metadata":{"_buckets":{"deposit":"23d784e6-b166-49fe-bd46-e1d0b90554b6"},"_deposit":{"created_by":1,"id":"39765","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39765"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039765","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["444266","444267","444262","444273","444264","444268","444271","444263","444272","444265","444269","444270"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Separated core turbofan engine"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"7","bibliographicPageStart":"1","bibliographicVolumeNumber":"1289","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"次世代の高亜音速輸送機用エンジンである超高バイパス比ターボファン・エンジンの研究「超高バイパス比可変形状エンジンの研究」を進めている過程で、新しい概念のエンジンであるコア分離型ターボファン・エンジンを考案した。このエンジンの特徴は、従来のターボファン・エンジンでは一体となっていたファンとコア・エンジンを分離して並列に配置したことである。概念検討の結果、コア分離型ターボファン・エンジンは従来型ターボファン・エンジンに比べて、安定性や構成の柔軟性などに優れており、また、VTOL輸送機用エンジンなどの新しい用途にも適していることを確認した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A new concept for a turbofan engine called the separated core turbofan engine is proposed and studied under the research program of the ultrahigh bypass turbofan engine for the next generation high-subsonic transport aircraft. The concept engine consists of two subunits, a core engine and a fan engine which are separated from each other. The results of the conceptual study show that this engine has many potential advantages over the current turbofan engines in many respects, including stability of operation and flexibility of configuration, and it also has other applications such as in advanced VTOL transport aircraft.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000448000","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: NAL TR-1289","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 原動機部"},{"subitem_text_value":"航空宇宙技術研究所 熱流体力学部"},{"subitem_text_value":"航空宇宙技術研究所 原動機部"},{"subitem_text_value":"航空宇宙技術研究所 原動機部"},{"subitem_text_value":"航空宇宙技術研究所 原動機部"},{"subitem_text_value":"航空宇宙技術研究所 原動機部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aeroengine Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Thermofluid Dynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aeroengine Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aeroengine Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aeroengine Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aeroengine Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"齊藤, 喜夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"遠藤, 征紀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松田, 幸雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"杉山, 七契"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菅原, 昇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 一臣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Yoshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Endo, Masanori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuda, Yukio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sugiyama, Nanahisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sugahara, Noboru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Kazuomi","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr01289.pdf","filesize":[{"value":"637.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01289.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39765/files/naltr01289.pdf"},"version_id":"ab28dcc4-8c5e-4382-a8c7-b5f54bd7bafd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"コア分離型ターボファンエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"高亜音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"超高バイパス比","subitem_subject_scheme":"Other"},{"subitem_subject":"安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"柔軟性","subitem_subject_scheme":"Other"},{"subitem_subject":"推進効率","subitem_subject_scheme":"Other"},{"subitem_subject":"騒音低減","subitem_subject_scheme":"Other"},{"subitem_subject":"最適空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"概念設計","subitem_subject_scheme":"Other"},{"subitem_subject":"VTOL機","subitem_subject_scheme":"Other"},{"subitem_subject":"separated core turbofan engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high subsonic transport aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ultrahigh bypass","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flexibility","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propulsion efficiency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"noise reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimum aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"conceptual design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"VTOL aircraft","subitem_subject_language":"en","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":"コア分離型ターボファン・エンジン","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"コア分離型ターボファン・エンジン"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39765","relation_version_is_last":true,"title":["コア分離型ターボファン・エンジン"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:22.084258+00:00"}