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PARAMETRIC EXPERIMENTAL AND NUMERICAL STUDY OF LP DIFFUSER AND EXHAUST HOODS

机译:LP扩散器和排烟罩的参数实验和数值研究

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The design of an effective diffuser for a given last stage blade of an LP turbine is known to be highly dependent on the size and shape of the exhaust hood in which it is located. For retrofit steam turbines in particular, where a new last stage blade and diffuser are fitted into an existing exhaust hood, the shapes and sizes of the exhaust box have been seen to vary significantly from one contract to the next. An experimental parametric study of diffuser lips and exhaust hood configurations has been run on a model test turbine rig at GE Power to investigate the impact of various geometric parameters on the performance of the diffusers. Improved testing and post-processing methodologies means the diffuser performance has been obtained for a greater number of geometric configurations than was previously typically possible. The results of these experiments are compared with numerical calculations and confirm the accuracy of the standard in-house diffuser design tools. Key geometric parameters are identified from the test data and used to generate improved diffuser design guidelines.
机译:已知用于LP涡轮的给定的末级叶片的有效扩散器的设计高度取决于其所位于的排气罩的尺寸和形状。特别是对于改造后的汽轮机,在现有排气罩中安装了新的末级叶片和扩散器的情况下,排气箱的形状和尺寸从一次收缩到另一次收缩都有很大不同。在GE Power的模型测试涡轮机上进行了扩散器唇缘和排气罩配置的实验参数研究,以研究各种几何参数对扩散器性能的影响。改进的测试和后处理方法论意味着,与以前通常可能获得的数量相比,采用更多数量的几何构型可以获得扩压器性能。将这些实验的结果与数值计算进行比较,并确认了标准室内扩散器设计工具的准确性。从测试数据中识别出关键的几何参数,并将其用于生成改进的扩压器设计指南。

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