Dynamic Properties of 3-D Reinforced C/SiC for the RS-2200 Linear Aerospike Engine
2008; Wiley; Linguagem: Inglês
10.1002/9780470294628.ch61
ISSN1940-6339
AutoresThomas Campbell, Joseph Ting, Peter Avitabile, James B. Min,
Tópico(s)Tribology and Wear Analysis
ResumoChapter 61 Dynamic Properties of 3-D Reinforced C/SiC for the RS-2200 Linear Aerospike Engine Thomas Campbell, Thomas Campbell Foster-Miller, Inc. 303 Bear Hill Rd Waltham, MA 02451Search for more papers by this authorJoseph Ting, Joseph Ting Foster-Miller, Inc. 303 Bear Hill Rd Waltham, MA 02451Search for more papers by this authorPeter Avitabile, Peter Avitabile University of Massachusetts Lowell One University Ave Lowell, MA 01854-2881Search for more papers by this authorJames Min, James Min NASA Glenn Research Center at Lewis Field Structural Dynamics and Mechanics Branch 21000 Brookpark Rd Cleveland, OH 44135Search for more papers by this author Thomas Campbell, Thomas Campbell Foster-Miller, Inc. 303 Bear Hill Rd Waltham, MA 02451Search for more papers by this authorJoseph Ting, Joseph Ting Foster-Miller, Inc. 303 Bear Hill Rd Waltham, MA 02451Search for more papers by this authorPeter Avitabile, Peter Avitabile University of Massachusetts Lowell One University Ave Lowell, MA 01854-2881Search for more papers by this authorJames Min, James Min NASA Glenn Research Center at Lewis Field Structural Dynamics and Mechanics Branch 21000 Brookpark Rd Cleveland, OH 44135Search for more papers by this author Book Editor(s):Todd Jessen, Todd JessenSearch for more papers by this authorErsan Ustundag, Ersan UstundagSearch for more papers by this author First published: 01 January 2000 https://doi.org/10.1002/9780470294628.ch61Citations: 3Book Series:Ceramic Engineering and Science Proceedings AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onFacebookTwitterLinked InRedditWechat Summary Ceramic matrix composite (CMC) materials such as C/SiC are an enabling technology for next-generation, high temperature air-breathing and rocket engines such as the RS-2200 Linear Aerospike engine. The goal of this research was to characterize the dynamic mechanical properties of C/SiC reinforced with 2-D and 3-D braid to support the design of the RS-2200. C/SiC samples were successfully produced using a pre-ceramic polymer infiltration and pyrolysis (PIP) process. 3-D braided reinforcement provides mechanical and process advantages over 2-D reinforcement. Dynamic and static mechanical properties were measured. Mechanical properties were found to be competitive with properties for parts produced with chemical vapor infiltration (CVI). Damping appeared to decrease with increasing frequency. Absolute damping at high frequencies was less than 0.2%. Results indicate that external damping treatments will be required for high-temperature, high speed turbomachinery applications. Citing Literature 24th Annual Conference on Composites, Advanced Ceramics, Materials, and Structures: A: Ceramic Engineering and Science Proceedings, Volume 21 RelatedInformation
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