Fabrication of Al2O3 Based Ceramic Matrix Composite by Conventional Sintering and Sol-Gel Process

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Abstract:

Alumina (Al2O3) matrix composites reinforced with 10%, 20% and 40% of 10µm size aluminum particles were fabricated by two processes, namely cold pressing and sintering process and Sol-Gel process. Al2O3, Al, 5% volume fraction of cobalt was mixed together, compacted and then sintered at 400-500oC for 30 minutes to fabricate the CMC. In the Sol-Gel fabrication route the Al2O3, Al, Co were blended with water and aged for 2-3 days to remove all the moisture and to enable oxidation of Al reinforcement. The mixture was cold pressed and sintered at 400-500oC to produce the CMC. The composition analysis of the CMC carried out by EDAX clearly showed that Al2O3 particles were formed by oxidation of Al reinforced in the matrix, effectively forming Al2O3/Al2O3 particulate reinforced ceramic matrix composite. The nature of the bonding at the interface was characterized using Scanning Electron Microscopy (SEM). The amount of porosity was determined using image analyzer based on ASTM B 276 standard. The average micro hardness of the samples was measured. The optimum volume fraction of aluminum for better interface bonding and reduced porosity was determined using the results obtained.

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Advanced Materials Research (Volumes 335-336)

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856-860

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September 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] Hiroshi Kaya: The application of ceramic-matrix composites to the automotive ceramic gas turbine. Composites Science and Technology, volume 59 (1999), pages 861-872.

DOI: 10.1016/s0266-3538(99)00016-0

Google Scholar

[2] Herbell TP, Eckel AJ: Ceramic matrix composites for rocket engine turbine applications. Journal of Engineering for Gas Turbines and Power, Volume 115, Issue 1. ASME paper No 92-GT-394.

DOI: 10.1115/1.2906687

Google Scholar

[3] Hisaichi Ohnabe, Shoju Masaki, Masakazu Onozuka, Kaoru Miyahara, Tadashi Sasa: Potential application of ceramic matrix composites to aero-engine components. Composites: Part A 30 (1999), pages 489–496.

DOI: 10.1016/s1359-835x(98)00139-0

Google Scholar

[4] H. Böhrk, U. Beyermann: Secure tightening of a CMC fastener for the heat shield of re-entry vehicles. Composite Structures. Volume 92, Issue 1, January 2010, Pages 107-112.

DOI: 10.1016/j.compstruct.2009.07.002

Google Scholar

[5] S.R. Pembertona, E.K. Oberga, J. Deana, D. Tsarouchasb, A.E. Markakib, L. Marstonc and T.W. Clyne: The fracture energy of metal fibre reinforced ceramic composites (MFCs). Composites Science and Technology, Volume 71, Issue 3, 7 February 2011, Pages 266-275.

DOI: 10.1016/j.compscitech.2010.10.011

Google Scholar

[6] L.P. Huang, J. Li: Properties of cobalt-reinforced Al2O3–TiC ceramic matrix composite made via a new processing route. Composites Part A: Applied Science and Manufacturing Volume 30, Issue 5, May 1999, Pages 615-618.

DOI: 10.1016/s1359-835x(98)00178-x

Google Scholar

[7] T. Sekino and K. Niihara: Microstructural characteristics and mechanical properties for Al2O3/metal nanocomposities. Nanostructured Materials Volume 6, Issues 5-8, 1995, Pages 663-666. Proceedings of the Second International Conference on Nanostructured Materials

DOI: 10.1016/0965-9773(95)00145-x

Google Scholar