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Non-Axisymmetric Shroud Profiled Endwall Optimization of an Embedded Stator and Experimental Investigation

机译:非轴对称护罩嵌入式定子的端壁优化和实验研究

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摘要

Turbomachinery has been widely used in the energy systems as an energy conversion device, such as gas turbine and aero-engine. The losses in the turbomachinery, especially in the multi-stage conditions, restrict the energy conversion efficiency and corresponding fuel economy. Previous studies show that non-axisymmetric endwall could be used to decrease the losses in compressors, but the real effects in the rig tests are usually inconsistent with the numerical simulation. In this paper, a shroud profiled endwall optimization method with the strategy of local loss as the objective function is proposed, aiming at reducing the tip loss of an embedded stator under the operating point. The traditional total loss coefficient and four local loss functions are studied to investigate how the objective functions influence the optimization results. Three optimized endwall geometries are tested in the embedded test platform. It showed that the strategy of loss coefficient above 90% span as the objective function was best at decreasing the stator loss in the tip region as well as the whole span. Under this strategy, the loss above 90% span was suppressed by 48.17% and the loss of the whole span decreased 9.27%, which proved the PEW optimization design method with the strategy of local loss as the objective function is potential.
机译:涡轮机已广泛用于能量系统中作为能量转换装置,例如燃气轮机和航空发动机。涡轮机械损失,特别是在多阶段条件下,限制了能量转换效率和相应的燃料经济性。以前的研究表明,非轴对称末端末端可用于降低压缩机中的损耗,但钻机测试中的实际效果通常与数值模拟不一致。在本文中,提出了一种作为目标函数作为目标函数的局部损失策略的护罩分布的端壁优化方法,旨在减少操作点下嵌入定子的尖端损耗。研究了传统的总损失系数和四个局部损失功能,研究了客观功能如何影响优化结果。在嵌入式测试平台中测试了三个优化的端壁几何形状。结果表明,由于目标函数的损耗系数以上损耗系数高于90%的策略,最好在降低尖端区域的定子损耗以及整个跨度时。在这一策略下,抑制了90%跨度的损失48.17%,整个跨度的损失减少了9.27%,这证明了局部损失策略的PEW优化设计方法,因为目标函数是潜力的。

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