Study of the Temperature State of the T-100-130 Steam Turbine High-Pressure Cylinder by Experimental and Theoretical Methods

O. Y. Kurganova, I. Kudinov, T. Gavrilova
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Abstract

The results of experimental and theoretical studies of the T-100-130 steam turbine high-pressure cylinder (HPC) in the starting mode are considered. Based on the experimental data on the temperature of the outer surface of the metal wall of the shell, using the approximate analytical solution of the heat conduction problem for a two-layer turbine wall (thermal insulation - turbine body), the heat transfer coefficients on the inner surface of the wall (the vapor side) were found by solving the inverse heat conduction problem. The heat transfer coefficients obtained this way were used to determine the temperature condition of the turbine HPC by the wall thickness and thermal insulation in various sections of the body. Using the results of calculations of the turbine HPC body temperature condition by the finite element method, the temperature stresses in the longitudinal section of the body were found. Their analysis allows concluding that the magnitude of the temperature stresses does not exceed the tensile strength limit for a given material. In this case, the stresses arising from the vapor pressure forces and from the non-uniformity of the temperature distribution in the circumferential direction were not taken into account.
T-100-130汽轮机高压缸温度状态的实验与理论研究
考虑了T-100-130汽轮机高压缸在启动模式下的实验和理论研究结果。根据壳体金属壁面外表面温度的实验数据,利用双层涡轮壁面(绝热层-涡轮体)热传导问题的近似解析解,通过求解热传导逆问题,求出了壁面内表面(蒸汽侧)的换热系数。利用该方法得到的换热系数,通过涡轮体各截面的壁厚和绝热情况来确定涡轮HPC的温度状态。利用有限元法对涡轮高性能混凝土机体温度工况的计算结果,求出了机体纵断面的温度应力。他们的分析得出结论,温度应力的大小不超过给定材料的抗拉强度极限。在这种情况下,由于蒸汽压力和温度分布在圆周方向上的不均匀性而产生的应力没有被考虑在内。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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