Tensile creep behavior of 3-D woven Si-Ti-C-O fiber/SiC-based matrix composite with glass sealant |
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Authors: | T. Ogasawara T. Ishikawa N. Suzuki I. J. Davies M. Suzuki J. Gotoh T. Hirokawa |
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Affiliation: | (1) National Aerospace Laboratory (NAL), Mitaka, Tokyo, 181-0015, Japan;(2) National Aerospace Laboratory (NAL), Mitaka, Tokyo, 181-0015, Japan;(3) Kyoto Institute of Technology, Sankyo-Ku, Kyoto, 606-8585, Japan;(4) Ube Industries Ltd., Yamaguchi, 755-8633, Japan;(5) Kawasaki Heavy Industries Ltd., Gifu, 405-8710, Japan;(6) Shikibo Ltd., Shiga, 517-8577, Japan |
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Abstract: | The present work investigates the tensile creep behavior (deformation and rupture) at 1100–1300°C in air of a 3-D woven Si-Ti-C-O (Tyranno) fiber/SiC-based matrix composite with and without glass sealant. The composite contained Si-Ti-C-O fibers with an additional surface modification in order to improve interface properties. Although a significant decrease in tensile strength was observed in the unsealed composite beyond 1000°C in air (and attributed to oxidation of the fiber/matrix interface), the composite with glass sealant possessed excellent mechanical properties for short-term (<1 hr.) exposure in air. In this study, tensile creep testing was conducted at 1100–1300°C in air and the effect of glass sealant on medium- and long-term strength was investigated. In addition, chemical stability of the glass sealant was evaluated by X-ray diffraction analysis (XRD) and energy dispersive X-ray spectrometer (EDS). The creep rupture behavior of the composite with glass sealant under long-term exposure is suggested to depend on several factors including decomposition, evaporation, and crystallization of the glass sealant material, in addition to the applied stress. |
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