{"created":"2023-06-20T15:11:28.500045+00:00","id":41139,"links":{},"metadata":{"_buckets":{"deposit":"293fb721-12e1-4a70-b1fe-bb3bf8693d04"},"_deposit":{"created_by":1,"id":"41139","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41139"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041139","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["450729","450728"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research and development of combustors for gas turbine and jet engines in the National Aerospace Laboratory"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"113","bibliographicPageStart":"1","bibliographicVolumeNumber":"676","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ガスタービンとジェットエンジンの燃焼器に関する開発技術の具体的手法について概説した。特に航空技術研究所で研究開発を行ったSTOL(短距離離着陸)機用ターボファンエンジンFJR710と高効率ガスタービンAGTJ-100Aの高圧燃焼器を中心に、当時の技術と開発した手法について記述した。ガスタービン燃焼器研究に必要な参考資料所在や実験的技術についても記述した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The basic technology and experiences in the National Aerospace Laboratory for the development of gas turbine combustors are described. Particular emphasis is placed on the combustor development for the turbofan engine FJR710 for a short take-off and landing plane and on the high efficiency gas turbine, AGTJ-100A, for use as a power plant. Basic experimental techniques and knowledge for research and development of the gas turbine combustors are also described.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004160000","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 TM-676","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"田丸, 卓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tamaru, Takashi","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":"naltm00676.pdf","filesize":[{"value":"15.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00676.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41139/files/naltm00676.pdf"},"version_id":"d83a28bb-a61c-415e-b4a1-4a665027b0b1"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"航空宇宙技術研究所","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスタービン","subitem_subject_scheme":"Other"},{"subitem_subject":"ジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼器","subitem_subject_scheme":"Other"},{"subitem_subject":"研究開発","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL機","subitem_subject_scheme":"Other"},{"subitem_subject":"ターボファンエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"高効率ガスタービン","subitem_subject_scheme":"Other"},{"subitem_subject":"高圧燃焼器","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼器形態","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼器性能試験","subitem_subject_scheme":"Other"},{"subitem_subject":"エンジン流入空気","subitem_subject_scheme":"Other"},{"subitem_subject":"燃料混合気形成","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼室","subitem_subject_scheme":"Other"},{"subitem_subject":"FJR 710","subitem_subject_scheme":"Other"},{"subitem_subject":"National Aerospace Laboratory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gas turbine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"jet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research and development","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbofan engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high efficiency gas turbine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high pressure combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustor form","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustor performance test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engine inlet air","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel mixture formation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustion chamber","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FJR 710","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":"航技研におけるガスタービンおよびジェットエンジン燃焼器研究開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研におけるガスタービンおよびジェットエンジン燃焼器研究開発"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41139","relation_version_is_last":true,"title":["航技研におけるガスタービンおよびジェットエンジン燃焼器研究開発"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:13:22.378695+00:00"}