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A plastic stress intensity factor approach to turbine disk structural integrity assessment

机译:涡轮盘结构完整性评估的塑性应力强度因子方法

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摘要

This study based on a new fracture mechanics parameter is concerned with assessing the integrityof cracked steam turbine disk which operate under startup-shutdown cyclic loading conditions. Damageaccumulation and growth in service have occurred on the inner surface of slot fillet of key. In order todetermine elastic-plastic fracture mechanics parameters full-size stress-strain state analysis of turbine disk wasperformed for a quote-elliptical part-through cracks under considering loading conditions. As a resultdistributions of elastic and plastic stress intensity factors along crack front in slot fillet of key of turbine diskdepending on surface crack form are defined. An engineering approach to the prediction of carrying capacity ofcracked turbine disk which is sensitive to the loading history at maintenance is proposed. The predictions of therate of crack growth and residual lifetime of steam turbine disk are compared for elastic and elastic-plasticsolutions. It is shown that the previously proposed elastic crack growth models provide overestimate thelifetime with respect to the present one. An advantage to use the plastic stress intensity factor to characterizethe fracture resistance as the self-dependent unified parameter for a variety of turbine disk configurations ratherthan the magnitude of the elastic stress intensity factors alone is discussed.
机译:基于新的断裂力学参数,这项研究涉及评估的完整性裂化蒸汽涡轮盘的哪个启动关断循环载荷的条件下进行操作。损害积累和增长中的服务已经发生键的槽圆角的内表面上。为了确定弹塑性断裂力学参数涡轮盘的全尺寸的应力 - 应变状态的分析是的报价椭圆部分通过下考虑负载条件裂缝进行。其结果在涡轮盘的密钥的时隙圆角沿着裂纹前端的弹性和塑性应力强度因子分布取决于表面裂纹形式被定义。一期工程的方法来承载能力的预测建议在维修破裂的涡轮盘这是加载历史敏感。的预测裂纹生长和蒸汽涡轮盘的剩余寿命的速率用于弹性和弹性塑料进行比较解决方案。结果表明,先前提出的弹性裂纹生长模型提供高估寿命对于本之一。一个优点是使用塑料应力强度因子来表征抗断裂性作为用于各种涡轮盘而配置的自相关参数统一比弹性应力强度的大小单独因素进行了讨论。

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