2022
DOI: 10.1111/ijac.13996
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Creep properties of melt infiltrated SiC/SiC composites with Sylramic™‐iBN and Hi‐Nicalon™‐S fibers

Abstract: Isothermal tensile creep tests were conducted on 2D woven and laminated, 0/90 balanced melt infiltration (MI) SiC/SiC composites at stress levels from 48 to 138 MPa and temperatures to 1400 • C in air. Effects of fiber architecture and fiber types on creep properties, influence of accumulated creep strain on in-plane tensile properties, and the dominant constituent controlling the creep behavior and creep rupture properties of these composites were investigated. In addition, the creep parameters of both compos… Show more

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Cited by 7 publications
(7 citation statements)
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“…Near stoichiometric ratio SiC fiber reinforced SiC ceramic matrix composites have the characteristics of lightweight, oxidation resistance, and high‐temperature resistance, especially its long‐term use temperature up to 1350°C, which makes it an ideal material system for the hot end component of aeroengine with high thrust‐weight ratio and the thermal protection system of aircraft with high Mach number 1–11 . The interfacial layer is a bond connecting the reinforced phase fiber and the continuous phase matrix.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Near stoichiometric ratio SiC fiber reinforced SiC ceramic matrix composites have the characteristics of lightweight, oxidation resistance, and high‐temperature resistance, especially its long‐term use temperature up to 1350°C, which makes it an ideal material system for the hot end component of aeroengine with high thrust‐weight ratio and the thermal protection system of aircraft with high Mach number 1–11 . The interfacial layer is a bond connecting the reinforced phase fiber and the continuous phase matrix.…”
Section: Introductionmentioning
confidence: 99%
“…Near stoichiometric ratio SiC fiber reinforced SiC ceramic matrix composites have the characteristics of lightweight, oxidation resistance, and high-temperature resistance, especially its long-term use temperature up to 1350 • C, which makes it an ideal material system for the hot end component of aeroengine with high thrust-weight ratio and the thermal protection system of aircraft with high Mach number. [1][2][3][4][5][6][7][8][9][10][11] The interfacial layer is a bond connecting the reinforced phase fiber and the continuous phase matrix. Its principal function is to optimize the mechanical behavior of the ceramic matrix composite under external load by adjusting the bonding strength between the fiber and the matrix to realize the strengthening and toughening effect of the ceramic matrix composite.…”
Section: Introductionmentioning
confidence: 99%
“…To some extent, the technical level and engineering capability of SiC fibers' development have become decisive factors in determining the development of SiC/SiC composites. [4][5][6] The SiC ceramic matrix is one of the critical components of SiC/SiC composites, which has important significance for modulus, hardness and environmental stability. The ceramic matrix is subjected to thermal shock, load shock, and gasparticle impact before the fiber and interface, which causes the matrix crack initiation and expansion of matrix cracks in the initial failure stages of ceramic matrix composites.…”
Section: Introductionmentioning
confidence: 99%
“…Under the action of external loading, the fracture strain of the SiC fibers is greater than that of the SiC matrix, which is the prerequisite for the ceramic matrix composites to have excellent strain capacity and damage tolerance. To some extent, the technical level and engineering capability of SiC fibers’ development have become decisive factors in determining the development of SiC/SiC composites 4–6 . The SiC ceramic matrix is one of the critical components of SiC/SiC composites, which has important significance for modulus, hardness and environmental stability.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, SiC/SiC composites are ideal thermal structure materials for application in aerospace aircraft thermal protection systems, engine hot-end components, and nuclear energy. [1][2][3][4][5][6][7][8][9] Near stoichiometric SiC fiber is the ceramic fiber with the highest temperature resistance and excellent mechanical properties. SiC/SiC composites prepared with near stoichiometric SiC fibers as reinforcement phase can withstand long-term service at 1350 • C and short-term service at 1500 • C, which can meet the environmental requirements of hot-end components of aero-engines with a thrustto-weight ratio of 10 and 12-15 levels.…”
Section: Introductionmentioning
confidence: 99%