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タイトル
和文:二段階電気抵抗変化法による複合材製旅客機の短時間衝撃損傷検査 
英文:Quick impact-damage inspection for composite aircraft by the 2-stage ERCM 
著者
和文: 鈴木良郎, 轟章, 水谷義弘.  
英文: Yoshirou Suzuki, AKIRA TODOROKI, yoshihiro mizutani.  
言語 English 
掲載誌/書名
和文: 
英文:Proceedings of the 2012 M&M Symposium for Young Researchers 
巻, 号, ページ         pp. 81-89
出版年月 2012年9月13日 
出版者
和文: 
英文: 
会議名称
和文:M&M若手シンポジウム2012 Hakodate (日本機械学会 材料力学部門) 
英文: 
開催地
和文: 
英文: 
公式リンク http://www.jsme.or.jp/conference/mmdconf12-2/
 
アブストラクト Impact loads initiate damages of several forms such as an indentation, fiber breakage, matrix cracking, and delamination cracking in carbon fiber reinforced polymer (CFRP). In this study, rapid diagnosis, which can finish inspecting the whole aircraft structure within an hour during refueling, was developed for composite aircraft. The proposed method consists of two electrical resistance change methods (ERCMs); the first target for detection is indentation in the whole structure, and the second one is delamination cracking. After an indentation is detected in the first stage, you only have to inspect limited area around the indentation for delamination inspection. Therefore, you can make use of an indentation as a marker of impact damage and can save inspection time and money even if large CFRP components are inspected. In the first for indentation detection, indentation increases fiber–fiber contact at the interlaminar interface and electrical conductivity. Consequently, electrical current applied to the material will concentrate around the indentation, and lead to selective and intense resistive heating. This temperature increase can be observed by thermography or detected as a change in electrical resistance caused by the temperature difference. In the second stage, delamination around an indentation can be detected without sampling the data from intact structures using statistical treatment. Moreover false diagnoses from changes in electrical resistance caused by damage to the electrical contacts at the electrodes can be prevented.

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