近化学计量SiC纤维在模拟航空发动机环境中的湿氧化行为

IF 1.5 Q4 ELECTROCHEMISTRY International Journal of Corrosion Pub Date : 2018-08-01 DOI:10.1155/2018/4319354
Liangyu Li, K. Jian, Xianhe Mao, Yifei Wang
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引用次数: 0

摘要

前体衍生和接近化学计量的SiC纤维(KD-S)在1000–1500°C下暴露1 h在PH2O:O2:Ar=14:8:78的模拟航空发动机环境中 KPa,气体流量为200 ml/分钟。结果表明,氧化后的KD-S纤维被二氧化硅层覆盖。随着退火温度的升高,氧含量、二氧化硅晶粒尺寸和氧化层厚度增加,而抗拉强度降低。在模拟航空发动机环境下处理的KD-S纤维显示出比在干燥空气中退火的纤维更大的SiO2晶粒尺寸、更厚的二氧化硅层和更好的残余强度。蒸汽可以通过降低活性能来加速KD-S纤维的氧化。研究和讨论了水蒸气对KD-S SiC纤维氧化行为的影响。
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Wet Oxidation Behavior of Near-Stoichiometric SiC Fibres in the Simulated Aeroengine Circumstance
The precursor-derived and near-stoichiometric SiC fibres (KD-S) were exposed at 1000–1500°C for 1 h in the simulated aeroengine circumstance of PH2O:O2:Ar = 14:8:78 KPa with the gas rate of 200 ml/min. The results indicated that the oxidized KD-S fibres were covered by silica layer. The oxygen content, grain size of silica, and oxide layer thickness increased, whereas the tensile strength decreased with rising annealing temperature. KD-S fibres treated under simulated aeroengine circumstances showed larger SiO2 grain size, thicker silica layer, and better residual strength than those annealed in dry air. The steam could accelerate the oxidation on KD-S fibres by reducing the active energy. The influence of water vapour on the oxidation behavior of KD-S SiC fibres was investigated and discussed as well.
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来源期刊
CiteScore
5.70
自引率
0.00%
发文量
8
审稿时长
14 weeks
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