{"created":"2023-06-20T15:13:57.073035+00:00","id":43918,"links":{},"metadata":{"_buckets":{"deposit":"b855d339-eb72-4504-a4be-52634fc780a5"},"_deposit":{"created_by":1,"id":"43918","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43918"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043918","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["466361","466359","466362","466353","466350","466354","466348","466356","466351","466352","466357","466346","466349","466360","466347","466358","466355","466363"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1977-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"27","bibliographicVolumeNumber":"335","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":"通商産業省工業技術院の主宰する大型工業技術研究開発制度のひとつ,「航空機用ジェットエンジンの研究開発」に関連して,低公害,高性能の航空機用ガスタービンエンジンの燃焼器を開発,研究している。ここでは,ダクトによって導かれた気流によって燃料を微粒化し,鈍頭部に保炎循環流を形成させる新形式の燃焼器,呼称「AS形」燃焼器の環状模型を製作し,入口空気絶対圧力,3.5～10kg/cm2にて燃焼試験をおこなった結果について報告する。燃焼器諸性能については,ほぼ所期の特性が得られた。ことに出口温度分布特性は良好であった。排出特性は,セクタ模型試験の予測通り,排煙,CO,およびTHCについて従来の圧力噴射弁とスワーラをそなえた形式の燃焼器とくらべて著しい低減を得ることができた。窒素酸化物(NOX)については,入口絶対圧力が6kg/cm2で従来の燃焼器並みの排出レベルで,10kg/cm2のときは,約50％の低減を示した。","subitem_description_type":"Abstract"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0335000","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 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