在不同的干氧大气中,具有薄间层的3D编织C/SiC的高温疲劳降解行为
Lexin Yang1, Dianwei He2, Chen Hu2
1State Key Laboratory of Clean and Efficient Turbomachinery Power Equipment, Deyang 618000, China.
Materials (Basel, Switzerland)
|October 16, 2024
概括
这项研究研究了3D编织的碳/碳化 (C/SiC) 复合材料的柔性强度,其中包含了溶性碳中间层. 在不同的温度,氧化和压力下,分析了高达1500°C的损伤机制.
科学领域:
- 材料科学 材料科学 材料科学
- 陶矩阵复合材料 陶矩阵复合材料
- 高温材料 高温材料
背景情况:
- 3D编织的C/SiC复合材料与溶性碳 (PyC) 介层是用于高温应用的先进材料.
- 了解它们在氧化和机械应力下的性能对于结构完整性至关重要.
研究的目的:
- 为了评估薄间层C/SiC (TI C/SiC) 复合材料的屈曲强度和损伤机制.
- 研究温度,氧化和应力对高达1500°C的材料行为的影响.
主要方法:
- 在循环负荷 (60 ± 20 MPa) 下在不同氧气部分压力和温度下对TI C/SiC复合材料的机械测试.
- 分析样本长度变化,骨折行为,残余屈曲强度和骨折形态.
主要成果:
- 材料长度的变化与PyC中间层 (正) 和C相 (负) 的损伤有关.
- 最大损伤发生在1300°C和17000Pa氧气部分压力下.
- 降低的温度/氧气缓解了正C相损伤;增加的参数促进了负C相损伤.
结论:
- C相的氧化主要是由向内氧气扩散驱动的.
- 较高的应力可以改变氧气扩散,扩大微裂并增加C相反应.
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