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Notch-Sensitivity of a Woven Oxide/Oxide Ceramic Matrix Composite

机译:编织氧化物/氧化物陶瓷基复合材料的缺口敏感性

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Oxide/oxide ceramic matrix composites (CMC) are currently being demonstrated in high-temperature aerospace applications. An oxide/oxide CMC under consideration by the U.S. Air Force is Nextel720/AS, which consists of an alumina-silica matrix (AS) reinforced with a woven Nextel720 fiber mat. The fracture behavior of notched Nextel720/AS at room and expected service temperatures is discussed in this paper. Specimens with semi-circular and narrow double-edge notches were tested under monotonic loading in laboratory air at 23 to 1200℃, and under sustained (creep) loading at 1100℃. The results show that Nextel720/AS is notch-insensitive at low temperatures (≤ 1000℃) and ≈22% notch-sensitive at higher temperatures (≥ 1100℃) under tensile loading. At 1100℃, the notch-sensitivity increased significantly under sustained loading.
机译:氧化物/氧化物陶瓷基复合材料(CMC)目前在高温航空航天应用中得到证明。美国空军正在考虑的氧化物/氧化物CMC是Nextel720 / AS,它由用编织Nextel720纤维毡增强的氧化铝-二氧化硅基质(AS)组成。本文讨论了带缺口的Nextel720 / AS在室温和预期使用温度下的断裂行为。在实验室空气中,在23至1200℃的单调载荷下,以及在1100℃的持续(蠕变)载荷下,对具有半圆形和窄双刃口缺口的样品进行了测试。结果表明,Nextel720 / AS在低温(≤1000℃)下对缺口不敏感,在高温(≥1100℃)下对缺口不敏感约≈22%。在1100℃下,持续载荷下的缺口敏感性显着提高。

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