{"created":"2023-06-20T15:07:27.784516+00:00","id":36835,"links":{},"metadata":{"_buckets":{"deposit":"2c3eaa97-e353-4510-8a83-cf7ec64b4dda"},"_deposit":{"created_by":1,"id":"36835","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36835"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036835","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["425110","425111","425108","425116","425114","425105","425107","425115","425106","425109","425117","425113","425118","425112"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"信頼性にもとづく耐損傷構造の検査スケジュール"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"146","bibliographicPageStart":"135","bibliographicVolumeNumber":"31","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空機の耐損傷胴体構造を解析し、Bayesの信頼性解析の有用性を実証した。数値計算例の結果は、検査中に多数の亀裂データが得られなくても、この解析は不確定パラメータの推定により適当な非定期的検査スケジュールを生成することを立証した。実際の場合のように一連の航空機を検査すると、多数の亀裂と破損の可能性が見出され、Bayesの解析をさらに実用的なものとしている。構造要素における疲れ亀裂の開始と伝搬および最終的な破損からなる破損プロセスの生成を評価した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The damage tolerant fuselage structure of an aircraft was analyzed, and the usefulness of the Bayesian reliability analysis was demonstrated. The results of the numerical examples verified that this analysis could generate appropriate nonperiodic inspection schedules with estimation of uncertain parameters even if a large number of crack data could not be collected during inspections. If a fleet of aircraft can be inspected as in the actual case, a large number of cracks and possibly failures will be found, and it makes the Bayesian analysis more practical. The generation of the failure process consisting of fatigue crack initiation and propagation, and final failure in the structure element was evaluated.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000440012","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-31","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 機体部"},{"subitem_text_value":"航空宇宙技術研究所 機体部"},{"subitem_text_value":"航空宇宙技術研究所 機体部"},{"subitem_text_value":"富士重工業 航空宇宙技術本部"},{"subitem_text_value":"富士重工業 航空宇宙技術本部"},{"subitem_text_value":"富士重工業 航空宇宙技術本部"},{"subitem_text_value":"富士重工業 航空宇宙技術本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries, Ltd Aerospace Division"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries, Ltd Aerospace Division"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries, Ltd Aerospace Division"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries, Ltd Aerospace Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"朝田, 洋雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 誠一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"少路, 宏和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"戸井, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤原, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大八木, 隆春"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高木, 淳二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Asada, Hiroo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Seiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shoji, Hirokazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Toi, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujiwara, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oyagi, Takaharu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takaki, Junji","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0031012.pdf","filesize":[{"value":"868.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0031012.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36835/files/nalsp0031012.pdf"},"version_id":"d72e8755-299e-4a84-b14d-6b16d3e84cfb"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"耐損傷構造","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機胴体","subitem_subject_scheme":"Other"},{"subitem_subject":"Bayesの信頼性解析","subitem_subject_scheme":"Other"},{"subitem_subject":"検査スケジュール","subitem_subject_scheme":"Other"},{"subitem_subject":"亀裂伝搬","subitem_subject_scheme":"Other"},{"subitem_subject":"破損プロセス","subitem_subject_scheme":"Other"},{"subitem_subject":"構造要素","subitem_subject_scheme":"Other"},{"subitem_subject":"疲れ亀裂","subitem_subject_scheme":"Other"},{"subitem_subject":"damage tolerant structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft fuselage","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Bayesian reliability analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inspection schedule","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"crack propagation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"failure process","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structure element","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fatigue crack","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Reliability-based inspection schedule for damage-tolerant structures","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Reliability-based inspection schedule for damage-tolerant structures","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36835","relation_version_is_last":true,"title":["Reliability-based inspection schedule for damage-tolerant structures"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:49:29.061386+00:00"}