Erosion Evaluation of Gas-Turbine Grade CMC’s at Room and Elevated Temperatures

Amirhossein Eftekharian, R. P. Panakarajupally, G. Morscher, Dade Huang, F. Abdi, Sung R. Choi
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Abstract

The objective of this study is to predict ceramic matrix composites (CMCs) erosion behavior and Retained Strength (RS) under environmental conditions using an Integrated Computational Material Engineering (ICME) physics-based approach. The state-of-the-art erosion analysis using phenomenological algorithms and Finite Element Models (FEM) models follows a test duplication methodology and is not able to capture the physics of erosion. In this effort, two CMC systems are chosen for Erosion evaluation: (a) Oxide/Oxide N720/alumina; and (b) MI SiC/SiC. Experiments are conducted at room and elevated temperatures (RT/ ET). Erosion testing considers: (i) a high velocity oxygen fuel (HVOF) burner rig for ET, and (ii) a pressurized helium impact gun for RT. Erodent particles are chosen as alumina and garnet. Experimental observations show that the type of erodent materials affects CMC erosion degradation at ET. Alumina exhibits to be an effective erodent for maintaining a solid phase particle erosion, while Garnet, experiences some degree of melting. Erosion of the oxide/oxide composite is more severe for the same erodent, temperature, mass, and velocity conditions than the MI SiC/SiC composite for all conditions tested. In general, increasing erosion temperature results in increasing erosion rate for the same erodent mass/velocity condition. In conjunction with experiments, a computational Multi-Scale Progressive Failure Analysis (MS-PFA) is also used to predict erosion of the above-mentioned material systems at RT/ET. The MS-PFA augments FEM by a de-homogenized material modeling that includes micro-crack density, fiber/matrix, interphase, and degrades both fiber and matrix simultaneously during the erosion process. Erodent particles are modeled by Smooth Particle Hydrodynamic (SPH) elements. Erosion evolution in CMCs considering strain rate effect predicts a) spallation, b) mass-loss, and c) damages in fiber, matrix, and their interphase. ICME modeling is capable of predicting the erosion process and reproducing the test observation for the MI SiC/SiC at RT, where: a) erodent particles break up the layer of matrix covering fiber due to interlaminar shear (delamination); b) fiber is fractured because of brittle behavior; c) the process (erosion tunneling) continues till it gets to the next thick matrix layer that slows down the tunneling; and d) Erosion tunnel widens as exposed fiber layers are removed (eroded). Simulations are also performed for erosion of the oxide/oxide due to glass beads at RT and ET. Predictions show that erosion rate is lower at ET because voids in the CMC vanish and the glass beads are less effective at ET. Finally, prediction of retained strength of eroded CMC test specimens is predicted by MS-PFA.
燃气轮机级CMC在室温和高温下的腐蚀评价
本研究的目的是使用基于集成计算材料工程(ICME)物理的方法预测陶瓷基复合材料(cmc)在环境条件下的侵蚀行为和保留强度(RS)。使用现象学算法和有限元模型(FEM)模型的最先进的侵蚀分析遵循测试重复方法,无法捕获侵蚀的物理特性。在这项工作中,选择了两种CMC系统进行侵蚀评估:(a)氧化物/氧化物N720/氧化铝;(b) MI SiC/SiC。实验在室温和高温(RT/ ET)下进行。腐蚀测试考虑:(i)用于ET的高速氧燃料(HVOF)燃烧器装置,(ii)用于rt的加压氦冲击枪。腐蚀颗粒选择为氧化铝和石榴石。实验观察表明,侵蚀材料的类型影响CMC在ET下的侵蚀降解。氧化铝是一种有效的侵蚀剂,可以维持固相颗粒侵蚀,而石榴石则会经历一定程度的熔化。在相同的侵蚀、温度、质量和速度条件下,氧化物/氧化物复合材料的侵蚀比MI SiC/SiC复合材料更严重。一般来说,在相同的侵蚀质量/速度条件下,侵蚀温度的升高会导致侵蚀速率的增加。结合实验,还使用计算多尺度渐进失效分析(MS-PFA)来预测上述材料体系在RT/ET下的侵蚀。MS-PFA通过非均质化材料模型增强了FEM,该模型包括微裂纹密度、纤维/基体、界面相,并在侵蚀过程中同时降解纤维和基体。采用光滑颗粒流体力学(SPH)单元对侵蚀颗粒进行建模。考虑应变速率效应的cmc的侵蚀演化预测了a)剥落,b)质量损失和c)纤维、基体及其间相的损伤。ICME模型能够预测MI SiC/SiC在RT下的侵蚀过程并重现试验观测结果,其中:a)侵蚀颗粒由于层间剪切(分层)破坏了覆盖纤维的基体层;B)纤维因脆性而断裂;C)这个过程(侵蚀隧穿)一直持续到下一个较厚的基质层,这减慢了隧穿的速度;d)随着暴露的纤维层被移除(侵蚀),侵蚀隧道变宽。模拟了玻璃微珠在高温和高温下对氧化物/氧化物的侵蚀。预测表明,在高温下,侵蚀率较低,因为CMC中的空隙消失了,玻璃微珠在高温下的效果较差。最后,通过MS-PFA预测了侵蚀CMC试件的保留强度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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