{"created":"2023-06-19T08:36:48.685274+00:00","id":3295,"links":{},"metadata":{"_buckets":{"deposit":"f88ee0f2-d775-43c9-b508-0f689969450f"},"_deposit":{"created_by":2,"id":"3295","owners":[2],"pid":{"revision_id":0,"type":"depid","value":"3295"},"status":"published"},"_oai":{"id":"oai:gunma-u.repo.nii.ac.jp:00003295","sets":["572:575:576"]},"author_link":["7970","7969","7971","7973","7972"],"item_6_alternative_title_18":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"Development of Micro Gas Turbine Combustor with a Recirculation Zone Induced by an Upward Swirl : 2nd Report, Effect of a Fuel Atomization on Combustion Characteristics and Measurement of Combustion Gas Flow in a Primary Zone(Thermal Engineering)"}]},"item_6_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-05-25","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"740","bibliographicPageEnd":"964","bibliographicPageStart":"957","bibliographicVolumeNumber":"74","bibliographic_titles":[{"bibliographic_title":"日本機械学會論文集. B編"}]}]},"item_6_date_61":{"attribute_name":"更新日","attribute_value_mlt":[{"subitem_date_issued_datetime":"2017-03-27","subitem_date_issued_type":"Created"}]},"item_6_description_14":{"attribute_name":"フォーマット","attribute_value_mlt":[{"subitem_description":"application/pdf","subitem_description_type":"Other"}]},"item_6_description_39":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"subitem_description":"Journal Article","subitem_description_type":"Other"}]},"item_6_description_4":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"A low NO_x combustor for kerosene-fueled micro gas turbine based on a new concept was proposed. The combustor consisted of primary and secondary combustion zones, and they were connected by a throat. A swirler was set between the primary and secondary combustion zones. In order to enhance recirculation of burned gas in the primary combustion zone, combustion air was introduced through the swirler and forced to flow upward to the combustor bottom. In this study, fundamental combustion characteristics such as lean combustion limit, exhaust gas composition and combustion gas temperature were measured using three fuel atomizers which rated flow rates were 3.0 gallon/h, 4.5 gallon/h and 6.0 gallon/h respectively. It was shown that the combustion stability and emission characteristics in the case of 3.0 gallon/h nozzle were superior to those in other cases. Further, gas velocity in the primary combustion zone was measured by Leaser Doppler Anemometer (LDA) and behavior of the recirculation of burned gas was investigated","subitem_description_type":"Abstract"}]},"item_6_publisher_32":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本機械学会"}]},"item_6_rights_12":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"本文データは学協会の許諾に基づきCiNiiから複製したものである"}]},"item_6_source_id_7":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0387-5016","subitem_source_identifier_type":"ISSN"}]},"item_6_source_id_9":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00187441","subitem_source_identifier_type":"NCID"}]},"item_6_version_type_15":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐々木, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"天野, 俊輔"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 哲也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"古畑, 朋彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"新井, 雅隆"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-11-25"}],"displaytype":"detail","filename":"E_ari_74-957.pdf","filesize":[{"value":"861.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"E_ari_74-957.pdf","url":"https://gunma-u.repo.nii.ac.jp/record/3295/files/E_ari_74-957.pdf"},"version_id":"f41153fb-36c9-4a6b-a37f-9d967f09a934"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Micro gas Turbine","subitem_subject_scheme":"Other"},{"subitem_subject":"Swirl","subitem_subject_scheme":"Other"},{"subitem_subject":"Spray Combustion","subitem_subject_scheme":"Other"},{"subitem_subject":"Atomization","subitem_subject_scheme":"Other"},{"subitem_subject":"Low NO x","subitem_subject_scheme":"Other"},{"subitem_subject":"Combusion Stability","subitem_subject_scheme":"Other"},{"subitem_subject":"Upward Swirl","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":"遡上スワールにより形成された循環流領域を持つマイクロガスタービン燃焼器の開発 : 第2報,燃料微粒化特性の燃焼特性に及ぼす影響と一次燃焼領域内の流動計測(熱工学,内燃機関,動力など)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"遡上スワールにより形成された循環流領域を持つマイクロガスタービン燃焼器の開発 : 第2報,燃料微粒化特性の燃焼特性に及ぼす影響と一次燃焼領域内の流動計測(熱工学,内燃機関,動力など)"},{"subitem_title":"Development of Micro Gas Turbine Combustor with a Recirculation Zone Induced by an Upward Swirl : 2nd Report, Effect of a Fuel Atomization on Combustion Characteristics and Measurement of Combustion Gas Flow in a Primary Zone(Thermal Engineering)","subitem_title_language":"en"}]},"item_type_id":"6","owner":"2","path":["576"],"pubdate":{"attribute_name":"公開日","attribute_value":"2010-06-22"},"publish_date":"2010-06-22","publish_status":"0","recid":"3295","relation_version_is_last":true,"title":["遡上スワールにより形成された循環流領域を持つマイクロガスタービン燃焼器の開発 : 第2報,燃料微粒化特性の燃焼特性に及ぼす影響と一次燃焼領域内の流動計測(熱工学,内燃機関,動力など)"],"weko_creator_id":"2","weko_shared_id":-1},"updated":"2023-06-19T13:05:55.821465+00:00"}