Static Strength Assessment of Turbine Blades in High-Capacity Power Units

IF 0.9 Q4 ENERGY & FUELS Thermal Engineering Pub Date : 2024-07-03 DOI:10.1134/s0040601524060016
A. N. Arkhipov, I. V. Puchkov, Yu. A. Ravikovich, O. V. Romanova, A. A. Ivanovskii
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Abstract

The article considers assessment methods and criteria of damage inflicted to turbine blades under the effect of static loads in carrying out 3D structural analyses of modern foreign and domestically produced high-capacity power units. Factors that should be considered in performing strength and lifetime analyses of the rotor blades of high-capacity turbines when subjected to short- and long-term static loading are pointed out. The article also describes 3D techniques for carrying out elastoplastic assessment of short-term static strength using a procedure for determining the limit rotation speed to blade fracture, airfoil residual displacements and strains, shank ultimate strength and displacement, root tearing-off, shear, flexural strength, etc. The article presents mutually complementary techniques for determining the bearing capacity as well as global and local long-term strength with using cumulative strain predictions by creep curves. Criteria used in different lifetime assessment methods are described, including those applied at different design stages and in using thermal protection coatings. Cases are considered in which creep strains are determined in the absence of data on creep curves by carrying out elastoplastic analyses by isochronous curves and lifetime analysis using the Larson–Miller curves. The need to take multiaxiality into account in estimating local creep in places of stress concentration is shown, and the applicability limits and criteria of such assessment that make it possible to increase the predicted lifetime by up to two times are described. Examples of tensile and compressive stress relaxation in estimating cumulative creep strain are given. Matters of creep interaction with other types of damage, including high-cycle and low-cycle (thermal cycling) fatigue, and various turbine loading kinds are considered.

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大容量发电机组涡轮叶片的静强度评估
摘要 本文探讨了在对现代国外和国内生产的大容量发电机组进行三维结构分析时,在静载荷作用下对涡轮叶片所造成损害的评估方法和标准。文章指出了在进行大容量涡轮机叶片在短期和长期静载荷作用下的强度和寿命分析时应考虑的因素。文章还介绍了使用确定叶片断裂极限转速、翼面残余位移和应变、柄部极限强度和位移、根部撕裂、剪切、弯曲强度等程序对短期静态强度进行弹性评估的三维技术。文章介绍了通过蠕变曲线预测累积应变来确定承载能力以及整体和局部长期强度的互补技术。文章介绍了不同寿命评估方法中使用的标准,包括在不同设计阶段和使用热保护涂层时使用的标准。还考虑了在没有蠕变曲线数据的情况下,通过等时曲线进行弹塑性分析和使用拉森-米勒曲线进行寿命分析来确定蠕变应变的情况。说明了在估算应力集中处的局部蠕变时需要考虑多轴性,并介绍了此类评估的适用范围和标准,这些评估使预测寿命最多可增加两倍。举例说明了在估算累积蠕变应变时拉伸和压缩应力松弛的情况。还考虑了蠕变与其他类型损伤的相互作用,包括高循环和低循环(热循环)疲劳,以及各种涡轮机加载类型。
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CiteScore
1.30
自引率
20.00%
发文量
94
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