Film Cooling Effectiveness Enhancement Using Multi-Longitudinal Vortex Generated by Alternating Elliptical Film Holes

K. Xiao, Juan He, Z. Feng
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Abstract

This paper proposed an alternating elliptical film hole for gas turbine blade to restrain kidney vortex and enhance film cooling effectiveness, based on the multi-longitudinal vortexes generated in alternating elliptical tube. The detailed flow structures in film hole delivering tube and out of the film hole, adiabatic film cooling effectiveness distributions as well as the total pressure loss coefficient were investigated. The delivering tube of alternating elliptical film hole consists of two straight sections and a transition section. In the straight sections, the cross section of the film hole is elliptical, and in the transition section, along flow direction, the major axis gradually shortened into the minor axis, and the minor axis gradually expanded to the major axis. But, the cross-section area of the film hole kept constant. Numerical simulations were performed by using 3D steady flow solver of Reynolds-averaged Navier-Stokes equations (RANS) with the SST k-ω turbulence model. To reveal the mechanism of kidney vortex suppression and film cooling effectiveness enhancement, the simulation results were compared with the cylindrical film hole set as the baseline at different mass flow ratios (MFR). Besides, the aerodynamic characteristics of these two kinds of film holes were also investigated. The results showed that obvious jet effect could be found in the cylindrical film hole, and the coolant mainly flowed along the upper wind wall, then interacted with the main flow, forming a strong kidney vortex after flowing out, which made the coolant to lift away from the wall surface and reduced the cooling effectiveness. The alternating elliptical film hole had a good inhibition impact on the jet effect in the hole due to the longitudinal vortices, which made the film adhere to the wall surface better after the coolant flowed out. The longitudinal vortices generated by alternating elliptical film hole have the opposite rotation direction to the vorticity of the kidney vortices, thus the kidney vortices were restrained to a certain extent. The height of kidney vortices is lower, and the size of kidney vortices is also smaller. As a result, the film cooling effectiveness of alternating elliptical film hole is distinctly higher than that of the cylindrical film hole, and the enhancement effect is more significant at higher mass flow ratio. In addition, the total pressure loss coefficient of alternating elliptical film hole is only slightly higher than the cylindrical film hole at the mass flow ratio of 1%, 2% and 3%, and is even lower at the mass flow ratio of 4%, thus inducing an excellent comprehensive performance.
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椭圆膜孔交替产生多纵向涡增强膜冷却效果
基于交变椭圆管内产生的多纵向涡,提出了一种用于燃气轮机叶片的交变椭圆膜孔来抑制肾涡,提高气膜冷却效率。研究了膜孔输送管内和膜孔外的流动结构、绝热膜冷却效率分布以及总压损失系数。交替椭圆膜孔输送管由两个直段和一个过渡段组成。在直线段,膜孔截面呈椭圆形,在过渡段,沿流动方向,长轴逐渐缩短为小轴,小轴逐渐扩大为长轴。但是,膜孔的横截面积保持不变。采用基于SST k-ω湍流模型的reynolds -average Navier-Stokes方程(RANS)三维定常求解器进行了数值模拟。为了揭示肾涡抑制和膜冷却效率提高的机理,以不同质量流量比(MFR)下圆柱形膜孔设置为基准,对模拟结果进行了比较。此外,还研究了这两种膜孔的气动特性。结果表明:柱状膜孔内存在明显的射流效应,冷却剂主要沿上风壁流动,然后与主流相互作用,流出后形成较强的肾涡,使冷却剂从壁面向上抬升,降低了冷却效果;由于纵向涡的存在,椭圆相间的膜孔对孔内的射流效果有很好的抑制作用,使得冷却剂流出后膜更好地附着在壁面上。交替椭圆膜孔产生的纵向涡与肾涡涡量的旋转方向相反,从而在一定程度上抑制了肾涡。肾形涡的高度较低,肾形涡的大小也较小。结果表明,椭圆型交替膜孔的膜冷却效果明显高于圆柱型交替膜孔,且在较大的质量流量比下,强化效果更为显著。此外,在质量流量比为1%、2%和3%时,交替椭圆膜孔的总压损失系数仅略高于圆柱膜孔,在质量流量比为4%时更低,从而产生了优异的综合性能。
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