高压叶片和低压叶片存在时过渡段流动的数值模拟

Jie Gao, Xuezheng Liu, Weiyan Xiao, Weiliang Fu, F. Meng, G. Yue, Q. Zheng
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引用次数: 0

摘要

受上游高压涡轮流动结构的影响,连接高压涡轮和低压涡轮的中间涡轮风道内的流动非常复杂。不同尺寸支板的导管产生的不均匀性也会影响LPT流入条件,导致效率降低。本文的目的是为高效过渡段设计提供对过渡段内流动物理和损失机制的详细了解。对高压叶片和低压叶片存在时过渡段的定常和非定常流动进行了数值模拟。探讨了上游高压叶片对过渡段内流场和损失特性的影响。描述了整个结构中尾流和二次流的产生和传播,包括过渡段流动的快速傅里叶变换(FFT)分析。数值模拟结果表明,在高端壁角风管中,叶片-支杆-叶片流动相互作用导致了复杂的流动模式,这是仅通过过渡段模拟无法获得的。过渡段对畸变流有较强的放大作用,上游尾迹和二次流的流入在过渡段出口处沿机匣形成了较大的损失区。对过渡段内的流动物理和损失机制进行了详细的分析和讨论。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Numerical Simulation of ITD Flows in the Presence of HP Blade and LP Vane
Flows in an intermediate turbine duct (ITD) connecting high-pressure turbines (HPT) and low-pressure turbines (LPT) are highly complex, influenced by the upstream HP turbine flow structures. Non-uniformities originating from the duct with struts of different sizes also affect the LPT inflow conditions, resulting in reduced efficiency. The goal of this paper is to provide detailed understanding of the flow physics and loss mechanisms within the ITDs for highly efficient ITD designs. Steady and unsteady numerical simulations of flows through the ITDs in the presence of HP blade and LP vane were conducted. Effects of upstream HP blade on flow fields and loss characteristics within the ITDs are explored. The generation and propagation of wake and secondary flows through the whole configuration is described, including the fast Fourier transformation (FFT) analyses of the flow in the ITD. Results from the numerical simulations show complex flow patterns resulted from blade-strut-vane flow interactions in a high-endwall-angle duct, which are not obtainable from ITD-only simulations. Moreover, the ITD has a strong amplifying effect on the distorted inflow, and the inflow with the upstream wake and secondary flows introduces a high loss area along the casing at ITD exit. Detailed results are presented and discussed for the flow physics and loss mechanisms within the ITD.
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