Damage growth detection of aircraft bonding structure under cyclic loading using FBG/PZT hybrid sensor system

Proceedings of the 3rd European Workshop - Structural Health Monitoring 2006

Volumn , Issue , 2006, Pages 220-227

  Ogisu, T ^a   Shimanuki, M ^b   Yoneda, H ^b   Okabe, Y ^b   Takeda, N ^b   Sakurai, T ^b  

^a FUJI HEAVY INDUSTRIES LTD   (Japan)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT SKIN; BONDING LAYERS; BONDING STRUCTURE; CYCLIC LOADINGS; DAMAGE GROWTH; DAMAGE GROWTH BEHAVIOR; DAMAGE INDEX; DAMAGE INITIATION; DAMAGE MONITORING; DETECTION CAPABILITY; EMBEDDED SENSORS; EMBEDDING METHOD; MONITORING SYSTEM; MUTUAL CORRELATIONS; PIEZO ELEMENTS; SKIN STRUCTURE; SMALL-DIAMETER FBG OPTICAL FIBER SENSORS; STRUCTURAL ELEMENTS; WAVE FORMS;

AIRCRAFT DETECTION; CHEMICAL SENSORS; COMPOSITE STRUCTURES; CYCLIC LOADS; LOADING; MONITORING; SIGNAL PROCESSING; STRUCTURAL ANALYSIS;

DAMAGE DETECTION;

EID: 34547424796     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

1. http://www.newairplane.com/ja-JP/Exas/TwchnolugySpotlight/composite.htm, visitedon Feb/2005."
2. th International Workshop on Structural Health Monitoring 2005, Stanford University, pp. 17-25, 2005.
3. th International Workshop on Structural Health Monitoring 2005, Stanford University, pp. 770-779, 2005.