SiC/SiC整体叶盘破裂转速分析与验证

Analysis and verification of the burst speed of ceramic matrix composite blisks

  • 摘要: 为了研究SiC/SiC整体叶盘承载能力,利用复合材料强度准则,在经典破裂转速分析方法中平均应力法和极限应力法的基础上,建立基于复合材料损伤机制的SiC/SiC整体叶盘破裂转速预测方法,对二维平纹布铺层的SiC/SiC整体叶盘试验件,开展破裂转速预测、试验验证,同时对破裂叶盘进行失效分析,探究整体叶盘起始失效位置影响因素。结果表明:平均应力法对破裂转速的预测结果误差较小,仅为0.02%,且预测的破裂起始位置和破裂模式与试验结果吻合;极限应力法对破裂转速的预测结果误差偏大,最大误差达到了10.71%,且预测的破裂起始位置和破裂模式不准确。涡轮叶盘起始失效位置与局部区域应力和缺陷体积及占比存在关联性。

     

    Abstract: To evaluate the load-bearing capacity of SiC/SiC integral turbine disks, a burst speed prediction approach grounded in the damage mechanisms of ceramic matrix composites was developed. The proposed method integrates composite strength criteria into the classical burst analysis framework, incorporating both the mean stress and ultimate stress methodologies. Based on a two-dimensional plain-woven SiC/SiC integral disk specimen, the burst speed was predicted and experimentally validated, followed by a failure analysis of the fractured disks to identify factors influencing the initiation of failure. The results demonstrate that the mean stress method yields highly accurate predictions, with a relative error of only 0.02%, and successfully reproduces both the initiation site and fracture morphology observed in experiments. In contrast, the ultimate stress method exhibits a considerably larger prediction deviation, with a maximum error of 10.71%, and fails to capture the actual initiation location and fracture pattern. Furthermore, the initiation site of the turbine disk failure is found to be closely correlated with local stress concentration, defect volume, and defect distribution ratio.

     

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