{"created":"2023-06-20T14:53:33.613726+00:00","id":21753,"links":{},"metadata":{"_buckets":{"deposit":"6338c77b-0b6a-47e7-9af0-2d20e84f7524"},"_deposit":{"created_by":1,"id":"21753","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"21753"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00021753","sets":["1887:1888"]},"author_link":["204206","204209","204211","204213","204210","204212","204208","204207"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Potential of Aircraft Electric Propulsion with SOFC/Gas Turbine Hybrid System"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-05-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"5","bibliographicPageEnd":"136(20)","bibliographicPageStart":"129(13)","bibliographicVolumeNumber":"65","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会誌"},{"bibliographic_title":"Aeronautical and Space Sciences Japan","bibliographic_titleLang":"en"}]}]},"item_7_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"CO2低減要求をはじめ2050年までを視野にした航空機の環境適合性要求は非常に厳しいものであり, 各国機関では, 機体・推進ともに新しい概念ならびに代替燃料の適用を模索して活発に検討を行っている. 水素社会の到来を見据え, 代替燃料の可能性を踏まえた航空機電動推進に関する検討が行われている. 本稿では, 欧米を中心に活発に検討が行われているコアとファンを分離することで有効バイパス比を飛躍的に増大させるコア分離電動ファンエンジンを想定し, 特にコア発電機の効率向上を目指した固体酸化物型燃料電池とガスタービンを組み合わせたハイブリッド発電機の航空機推進系動力としての有効性について検討した. 固体酸化物型燃料電池を航空機飛行環境で運用する際の課題と克服手段を提案し, 提案したシステムにおいて効率向上効果を見込む簡単な解析結果を示した.","subitem_description_type":"Abstract"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: 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 illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: DS1740116002","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Japan Society for Aeronautical and Space Sciences"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0021-4663","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":"AN00189072","subitem_source_identifier_type":"NCID"}]},"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":"岡井, 敬一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野村, 浩司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田頭, 剛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西沢, 啓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okai, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nomura, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tagashira, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishizawa, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Aircraft Electric Propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Distributed Propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SOFC (Solid Oxide Fuel Cell)/GT (Gas Turbine) Hybrid System","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"航空機電動推進用燃料電池ハイブリッドシステムの可能性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空機電動推進用燃料電池ハイブリッドシステムの可能性"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2017-06-16"},"publish_date":"2017-06-16","publish_status":"0","recid":"21753","relation_version_is_last":true,"title":["航空機電動推進用燃料電池ハイブリッドシステムの可能性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:31:06.844609+00:00"}