TY - GEN
T1 - Sensors for monitoring the processing of carbon-carbon composites
AU - Tittmann, Bernhard R.
AU - Yen, C. Eric
PY - 1995
Y1 - 1995
N2 - Carbon-carbon composite are used in many applications including aircraft disk brakes, space shuttle leading edges, rocket inlet nozzles and exit cones, and are currently being considered for future aircraft structural components, because of their mechanical stability under adverse temperature conditions. Unfortunately, the processing of carbon-carbon composites, especially the first carbonizations, has a relatively low yield, because of in-process interply failure leading to catastrophic delaminations. Considerable amount of man-power, equipment time and material are lost. Here we report on the progress in the development of sensors for monitoring these catastrophic events during the first carbonization. Specifically, acoustic emission sensors and gas sensors are singled out as the most promising ones for monitoring the evolution of micro and macro-structural changes during the first carbonization. Analysis of the high temperature waveguide was undertaken to determine the optimum waveguide geometry so that only a single mode is allowed to propagate in the waveguide.
AB - Carbon-carbon composite are used in many applications including aircraft disk brakes, space shuttle leading edges, rocket inlet nozzles and exit cones, and are currently being considered for future aircraft structural components, because of their mechanical stability under adverse temperature conditions. Unfortunately, the processing of carbon-carbon composites, especially the first carbonizations, has a relatively low yield, because of in-process interply failure leading to catastrophic delaminations. Considerable amount of man-power, equipment time and material are lost. Here we report on the progress in the development of sensors for monitoring these catastrophic events during the first carbonization. Specifically, acoustic emission sensors and gas sensors are singled out as the most promising ones for monitoring the evolution of micro and macro-structural changes during the first carbonization. Analysis of the high temperature waveguide was undertaken to determine the optimum waveguide geometry so that only a single mode is allowed to propagate in the waveguide.
UR - http://www.scopus.com/inward/record.url?scp=0029211099&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0029211099&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:0029211099
SN - 0819417939
T3 - Proceedings of SPIE - The International Society for Optical Engineering
SP - 180
EP - 191
BT - Proceedings of SPIE - The International Society for Optical Engineering
PB - Society of Photo-Optical Instrumentation Engineers
T2 - Smart Structures and Materials 1995: Smart Sensing, Processing, and Instrumentation
Y2 - 27 February 1995 through 1 March 1995
ER -