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NUMERICAL SIMULATION OF ITD FLOWS IN THE PRESENCE OF HP BLADE AND LP VANE

机译:HP刀片和LP叶片存在ITD流量的数值模拟

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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.
机译:在连接高压涡轮机(HPT)和低压涡轮机(LPT)的中间涡轮管道(ITD)中的流动是高度复杂的,受上游HP涡轮机流动结构的影响。源自不同尺寸的管道的不均匀性也影响LPT流入条件,导致效率降低。本文的目标是详细了解ITDS内的流量物理和损失机制,以获得高效的ITD设计。进行了通过在HP刀片和LP叶片存在下通过ITDS流动的稳定和不稳定的数值模拟。探讨了上游HP刀片对ITDS内流场和损失特征的影响。描述了唤醒和次级流过整个配置的生成和传播,包括ITD中流量的快速傅里叶变换(FFT)分析。来自数值模拟的结果显示了从高端壁角管道中的叶片 - 支柱叶片流动相互作用导致的复杂流动图案,其不可从唯一的模拟中获得。此外,ITD对扭曲的流入具有很强的放大效果,并且具有上游唤醒和次级流动的流入沿着壳体在ITD出口沿壳体引入了高损耗区域。提出了详细的结果,并讨论了ITD内的流理物理和损失机制。

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