{"created":"2023-06-20T15:14:14.983650+00:00","id":44232,"links":{},"metadata":{"_buckets":{"deposit":"3d148131-e853-486b-b9f6-3f05bb935959"},"_deposit":{"created_by":1,"id":"44232","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44232"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044232","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["468485","468484","468486","468487"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Residual Strength Tests of Aged Light Aircraft"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-06","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"63","bibliographicVolumeNumber":"750","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":"我が国のメーカーが独自に開発し量産した小型航空機FA-200-180型機３機の経年機体について、機体主構造（特に主翼および胴体）の残存強度評価を目的に静荷重試験を行った。この機体は、約25年の間航空大学校において学生の訓練飛行に使用されたものである。試験結果は、機体開発時試験結果と比較し、３機とも制限荷重の範囲において、経年による機体構造の劣化は見られなかった。制限荷重に対して安全上有害な残留変形は存在せず、更に終極荷重に対して３秒間以上耐荷した。また、破壊荷重は、制限荷重のそれぞれ198％、200％および199％と３機の間でバラツキは極めて少ない良好な結果であり、25年後でも機体は充分な強度および剛性を有していたことを証明した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The residual strength of three aged FA-200-180 light aircraft was tested in order to confirm the integrity of the aircrafts primary structures. These  aircraft have been used in training for about 25 years at the Civil Aviation College. The test results did not show any deterioration in aircraft primary structure compared with  the original prototype aircraft in the design limit load range. These aircraft maintained their strength without detrimental or permanent deformation up to the design limit load and, furthermore, without failing for more than three seconds at the ultimate load. Failures of each airframe occurred at 198％, 200％ and 199％ of the design limit load respectively. It was thus demonstrated that the primary structures of these aircraft have retained adequate structural integrity even after 25 years.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0750000","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-750","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構造研究部"},{"subitem_text_value":"航空宇宙技術研究所構造研究部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"外崎, 得雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上田, 哲彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SOTOZAKI, Tokuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"UEDA, Tetsuhiko","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":"2020-01-29"}],"displaytype":"detail","filename":"naltm0000750.pdf","filesize":[{"value":"3.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm0000750.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44232/files/naltm0000750.pdf"},"version_id":"4e574ad9-0f2c-4bf0-8833-8c1c2728188f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Aged Aircraft; Strength; Static test","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":"経年小型航空機の残存強度試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"経年小型航空機の残存強度試験"}]},"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":"44232","relation_version_is_last":true,"title":["経年小型航空機の残存強度試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:00:31.175570+00:00"}