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Rapid Prototyping of Continuous Fiber Reinforced Ceramic Matrix CompositesFor ceramics to be used as structural components in high temperature applications, their fracture toughness is improved by embedding continuous ceramic fibers. Ceramic matrix composite (CMC) materials allow increasing the overall operating temperature, raising the temperature safety margins, avoiding the need for cooling, and improving the damping capacity, while reducing the weight at the same time. They also need to be reliable and available in large quantities as well. In this paper, an innovative rapid prototyping technique to fabricate continuous fiber reinforced ceramic matrix composites is described. The process is simple, robust and will be widely applicable to a number of high temperature material systems. This technique was originally developed at the University of Delaware Center for Composite Materials (UD-CCM) for rapid fabrication of polymer matrix composites by a technique called automated tow placement or ATP. The results of mechanical properties and microstructural characterization are presented, together with examples of complex shapes and parts. It is believed that the process will be able to create complex shaped parts at an order of magnitude lower cost than current chemical vapor infiltration (CVI) and polymer impregnation and pyrolysis (PIP) processes.
Document ID
20030062265
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Vaidyanathan, R.
(Advanced Ceramics Research, Inc. Tucson, AZ, United States)
Green, C.
(Advanced Ceramics Research, Inc. Tucson, AZ, United States)
Phillips, T.
(Advanced Ceramics Research, Inc. Tucson, AZ, United States)
Cipriani, R.
(Advanced Ceramics Research, Inc. Tucson, AZ, United States)
Yarlagadda, S.
(Delaware Univ. Newark, DE, United States)
Gillespie, J. W., Jr.
(Delaware Univ. Newark, DE, United States)
Effinger, M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Cooper, K. C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Composite Materials
Meeting Information
Meeting: SAMPE 2003 Symposium/Exhibition
Location: Long Beach, CA
Country: United States
Start Date: May 11, 2003
End Date: May 15, 2003
Sponsors: Society for the Advancement of Materials and Process Engineering
Funding Number(s)
CONTRACT_GRANT: NAS8-00192
Distribution Limits
Public
Copyright
Public Use Permitted.
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