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Probabilistic Analysis of a SiC/SiC Ceramic Matrix Composite Turbine Vane

机译:SiC / SiC陶瓷基复合材料涡轮叶片的概率分析

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摘要

To demonstrate the advanced composite materials technology under development within the Ultra-Efficient Engine Technology (UEET) Program, it was planned to fabricate, test, and analyze a turbine vane made entirely of silicon carbide-fiber-reinforced silicon carbide matrix composite (SiC/SiC CMC) material. The objective was to utilize a five-harness satin weave melt-infiltrated (MI) SiC/SiC composite material developed under this program to design and fabricate a stator vane that can endure 1000 hours of engine service conditions. The vane was designed such that the expected maximum stresses were kept within the proportional limit strength of the material. Any violation of this design requirement was considered as the failure. This report presents results of a probabilistic analysis and reliability assessment of the vane. Probability of failure to meet the design requirements was computed. In the analysis, material properties, strength, and pressure loading were considered as random variables. The pressure loads were considered normally distributed with a nominal variation. A temperature profile on the vane was obtained by performing a computational fluid dynamics (CFD) analysis and was assumed to be deterministic. The results suggest that for the current vane design, the chance of not meeting design requirements is about 1.6 percent.
机译:为了展示超高效发动机技术(UEET)计划中正在开发的先进复合材料技术,计划制造,测试和分析完全由碳化硅纤维增强的碳化硅基复合材料(SiC / SiC CMC)材料。目的是利用在此程序下开发的五线缎纹编织熔渗(MI)SiC / SiC复合材料来设计和制造可承受1000小时发动机工作条件的定子叶片。叶片的设计应使预期的最大应力保持在材料的比例极限强度之内。任何违反此设计要求的行为均视为失败。该报告提供了叶片的概率分析和可靠性评估的结果。计算出不满足设计要求的概率。在分析中,材料特性,强度和压力载荷被视为随机变量。压力负荷被认为是具有名义变化的正态分布。叶片上的温度曲线是通过执行计算流体动力学(CFD)分析获得的,并被认为是确定性的。结果表明,对于当前的叶片设计,不满足设计要求的机会约为1.6%。

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