Recent advances in composite fuselage demonstration program for damage and health monitoring in Japan

Structural Control and Health Monitoring

Volumn 12, Issue 3-4, 2005, Pages 245-255

  Takeda, N ^a   Tajima, N ^b   Sakurai, T ^b   Kishi, T ^c  

^a UNIVERSITY OF TOKYO   (Japan)

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

^c NATIONAL INSTITUTE FOR MATERIALS SCIENCE   (Japan)

Author keywords

Composite structures; Damage detection; Damage suppression; Optical fiber sensors; Structural health monitoring

Indexed keywords

ACTUATORS; COMPOSITE STRUCTURES; FUSELAGES; HEALTH CARE; MONITORING; OPTICAL FIBERS; SENSORS; STRUCTURAL ANALYSIS;

DAMAGE DETECTION; DAMAGE SUPPRESSION; OPTICAL FIBER SENSORS; STRUCTURAL HEALTH MONITORING;

INTELLIGENT MATERIALS;

EID: 27144550752     PISSN: 15452255     EISSN: None     Source Type: Journal    
DOI: 10.1002/stc.68     Document Type: Conference Paper

References (10)

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3. Takeda N, Niizuma H, Ogihara S, Kobayashi A. Application of micro-line/grid methods to temperature-dependent microscopic deformation and damage in CFRP laminates. Experimental Mechanics 1997; 37(2): 182-187.
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6. Satori K, Ikeda Y, Kurosawa Y, Hongo A, Takeda N. Development of small-diameter optical fiber sensors for damage detection in composite laminates. SPIE Proceedings 2000; 3986:104-111.
7. Mizutani T, Okabe Y, Takeda N. Crack identification in CFRP laminates using small-diameter FBG sensors. SPIE Proceedings 2002; 4694:330-340.
8. Takeda S, Okabe Y, Takeda N. Detection of delamination in composite laminates using small-diameter FBG sensors. SPIE Proceedings 2002; 4694:138-148.
9. Tsutsui H, Sanda T, Okabe Y, Takeda N. Real-time detection of impact load on composite laminates with embedded small-diameter optical fiber. SPIE Proceedings 2000; 3986:112-120.
10. Park JB, Okabe T, Takeda N, Curtin WA. Electromechanical modeling of unidirectional CFRP composites under tensile loading condition. Composites 2002; 33A:265-275.