Feasibility studies on active damage detection for CFRP aircraft bonding structures

Advanced Composite Materials: The Official Journal of the Japan Society of Composite Materials

Volumn 15, Issue 2, 2006, Pages 153-173

  Ogisu, Toshimichi ^a   Shimanuki, Masakazu ^a   Kiyoshima, Satoshi ^a   Okabe, Yoji ^b   Takeda, Nobuo ^b  

^a FUJI HEAVY INDUSTRIES LTD   (Japan)

^b UNIVERSITY OF TOKYO   (Japan)

Author keywords

Aircraft structure; Damage detection; Damage monitoring system; Elastic wave; Piezo transducer (PZT) actuator FBG sensor; Structural health management; Structural integrity

Indexed keywords

ACTUATORS; COMPOSITE MATERIALS; COSTS; ELASTIC WAVES; JOINTS (STRUCTURAL COMPONENTS); OPTICAL FIBERS; PIEZOELECTRIC DEVICES; SAFETY FACTOR; SENSORS;

AIRCRAFT STRUCTURES; DAMAGE DETECTION; DAMAGE MONITORING SYSTEM; PIEZO TRANSDUCER (PZT) ACTUATOR/FBG SENSOR; STRUCTURAL HEALTH MANAGEMENT; STRUCTURAL INTEGRITY;

CARBON FIBER REINFORCED PLASTICS;

EID: 33747132471     PISSN: 09243046     EISSN: None     Source Type: Journal    
DOI: 10.1163/156855106777873923     Document Type: Article

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