Mechanical and vibration testing of carbon fiber composite material with embedded piezoelectric sensors

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 8341, Issue , 2012, Pages

  Duffy, Kirsten P ^a   Lerch, Bradley A ^b   Wilmoth, Nathan G ^b   Kray, Nicholas ^c   Gemeinhardt, Gregory ^c  

^a UNIVERSITY OF TOLEDO   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c GE AVIATION   (United States)

Author keywords

Aircraft engine blades; Damping; Piezoelectricity; Polymer matrix fiber composite; PZT 5A; Type II PZT

Indexed keywords

ACTIVE VIBRATION CONTROL SYSTEMS; CARBON FIBER COMPOSITE MATERIALS; COMPOSITE SPECIMENS; EMBEDDED PIEZOELECTRIC PATCH; FIBER COMPOSITE; FOUR-POINT BENDING; MATERIAL PROPERTY; PASSIVE DAMPING; PATCH TYPE; PIEZOCERAMIC MATERIALS; PIEZOELECTRIC ELEMENTS; PIEZOELECTRIC FIBER; PIEZOELECTRIC PATCH; PIEZOELECTRIC SENSORS; PZT; PZT-5A; SENSING PROPERTY; SHORT BEAM SHEAR; VIBRATION TESTING;

AIRCRAFT ENGINES; CARBON FIBERS; COMPOSITE MATERIALS; CRYSTALLOGRAPHY; DAMPING; DEBRIS; INTEGRATED CONTROL; INTERFACES (MATERIALS); PIEZOELECTRIC DEVICES; PIEZOELECTRIC MATERIALS; PIEZOELECTRICITY; VIBRATIONS (MECHANICAL);

STRENGTH OF MATERIALS;

AIR CRAFT; CARBON FIBERS; COMPOSITES; CONTROL SYSTEMS; CRYSTALLOGRAPHY; ENGINES; PIEZOELECTRICITY; POLYMERS; VIBRATION;

EID: 84861522860     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.916769     Document Type: Conference Paper

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