预测工业燃气轮机EBC温度极限

B. Pint, P. Stack, K. Kane
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引用次数: 1

摘要

较高的涡轮进口温度可能需要使用陶瓷基复合材料(CMC),如SiC/ SiC,这需要环境屏障涂层(ebc)来保护它们免受水蒸气的有害影响。该项目的目标是确定用于陆基涡轮机的ebc的最大粘结涂层温度,其中最小涂层寿命为25,000小时。如果温度超过Si粘结涂层的熔点1414°C,则还需要评估没有粘结涂层的涂层。因此,目前有硅键涂层的Yb2Si2O7 EBCs和没有硅键涂层的下一代EBCs正在实验室测试中进行评估,在空气+90%H2O中循环1小时。在这项初步工作中,涂层沉积在CVD SiC板上。在1250°,1300°和1350°C下,通过测量暴露100-500小时后热生长二氧化硅的厚度来评估反应动力学。为了进行比较,未涂覆的SiC和Si样品在干燥和潮湿环境下的水垢生长速率分别作为最小值和最大值。基于临界尺度厚度失效标准,使用这些初始数据计算了两个EBC系统的估计最高温度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Predicting EBC Temperature Limits for Industrial Gas Turbines
Higher turbine inlet temperatures may require the use of ceramic matrix composites (CMC) such as SiC/SIC, which require environmental barrier coatings (EBCs) to protect them against the detrimental effect of water vapor. The goal of this project is to determine the maximum bond coating temperature for EBCs for land-based turbines, where the minimum coating lifetime is 25,000 h. If the temperature exceeds the 1414°C melting point of the Si bond coating, then coatings without a bond coating also need to be evaluated. Thus, current Yb2Si2O7 EBCs with a Si bond coating and next-generation EBCs without a Si bond coating are being evaluated in laboratory testing using 1-h cycles in air+90%H2O. For this initial work, coatings were deposited on CVD SiC coupons. Reaction kinetics at 1250°, 1300° and 1350°C have been evaluated by measuring the thickness of the thermally grown silica scale after 100–500 h exposures. For comparison, scale growth rates for uncoated SiC and Si specimens in dry and wet environments were included as minimum and maximum values, respectively. Based on a critical scale thickness failure criteria, estimated maximum temperatures were calculated for both EBC systems using this initial data.
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