Impact monitoring of the aircraft composite structure using FBG sensor/PZT actuator hybrid sensor system

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 6527, Issue , 2007, Pages

  Nakamura, Noritsugu ^a   Ogisu, Toshimichi ^a   Yoneda, Hiroshi ^a   Okabe, Yoji ^b   Takeda, Nobuo ^b   Sakurai, Tateo ^c  

^a FUJI HEAVY INDUSTRIES LTD   (Japan)

^b UNIVERSITY OF TOKYO   (Japan)

^c NONE

Author keywords

Aircraft structure; Impact damage monitoring; Small diameter FBG optical fiber sensor; Structural health monitoring

Indexed keywords

ACTUATORS; AIRCRAFT MANUFACTURE; FIBER BRAGG GRATINGS; IMPACT TESTING; OPTICAL SENSORS; STRUCTURAL HEALTH MONITORING;

AIRCRAFT STRUCTURE; IMPACT DAMAGE MONITORING; SMALL-DIAMETER FBG OPTICAL FIBER SENSORS;

COMPOSITE STRUCTURES;

EID: 35549007171     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.715584     Document Type: Conference Paper

References (9)

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