Damage growth monitoring for a bonding layer of the aircraft bonding structure

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 6171, Issue , 2006, Pages

  Ogisu, Toshimichi ^a   Shimanuki, Masakazu ^a   Yoneda, Hiroshi ^a   Okabe, Yoji ^b   Kuwahara, Junichiro ^b   Takeda, Nobuo ^b   Sakurai, Tateo ^c  

^a FUJI HEAVY INDUSTRIES LTD   (Japan)

^b UNIVERSITY OF TOKYO   (Japan)

^c R&D Institute of Metals and Composites for Future Industries   (Japan)

Author keywords

Aircraft structure; Bonding structure; Damage growth behavior; Damage monitoring; Elastic (lamb) wave detection; Small diameter FBG optical fiber sensor; Structural health monitoring

Indexed keywords

CONDITION MONITORING; CRACK INITIATION; DYNAMIC LOADS; ELASTIC WAVES; FIBER OPTIC SENSORS; INTELLIGENT STRUCTURES; OPTIMIZATION;

AIRCRAFT STRUCTURE; BONDING STRUCTURE; DAMAGE GROWTH BEHAVIOR; DAMAGE MONITORING; ELASTIC (LAMB) WAVE DETECTION; SMALL-DIAMETER FBG OPTICAL FIBER SENSOR; STRUCTURAL HEALTH MONITORING;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 33745915562     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.658555     Document Type: Conference Paper

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