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Development of Elements for the Modernized Flow Path of a T-100-12.8 Steam Turbine by the Methods of Computational Aerodynamics

机译:用计算空气动力学方法开发T-100-12.8汽轮机现代化流道要素

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摘要

The results of gasdynamic development of the flow path elements in modernization of the high-pressure cylinder of a T-100-12.8 turbine using reaction blading are presented. The numerical simulation of viscous turbulent flows of the compressible working medium is carried out using the SINF program. This enabled determination of efficient shapes of the elements being developed. We find a shape for the meridional contours of the control stage chamber that guarantees minimum energy losses and a reasonable radial flow nonunifor-mity. The use of a tear-shaped profile is substantiated in the second-stage nozzle vanes when the incident flow angles are small. Check calculations are carried out verifying that the choice of the shape of the flow-path elements is optimal.
机译:给出了使用反应叶片对T-100-12.8涡轮机高压缸进行现代化改造时流路元件的气体动力学结果。使用SINF程序对可压缩工作介质的粘性湍流进行了数值模拟。这使得能够确定所开发元素的有效形状。我们找到了控制级腔室子午线轮廓的形状,该形状可确保最小的能量损失和合理的径向流量不均匀性。当入射流角较小时,在第二级喷嘴叶片中证实使用了泪状轮廓。进行检查计算,以验证对流路元件形状的选择是否最佳。

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