首页> 外文会议>International Symposium on Jet Propulsion and Power Engineering >FLOW AND HEAT TRANSFER CHARACTERISTICS OF TWO EFFUSED COOLING MODELS: TRANSPIRATION COOLING AND FULL COVERAGE FILM COOLING
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FLOW AND HEAT TRANSFER CHARACTERISTICS OF TWO EFFUSED COOLING MODELS: TRANSPIRATION COOLING AND FULL COVERAGE FILM COOLING

机译:两个活化冷却模型的流动和传热特性:蒸发冷却和完全覆盖膜冷却

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Though both discrete hole and slot film cooling has been proved to be effective cooling methods, strong demand for further improvement of turbine blade cooling exists with the increase of turbine inlet temperature of modern gas turbine. Transpiration cooling, by replacing the cooled surface with porous wall, could be a satisfied choice for next generation high temperature gas turbine for its larger and evenly distributed cooling effectiveness. Full coverage film cooling has been severing as the main external cooling method of G class gas turbine. But the implementation of transpiration cooling in gas turbine blade cooling requires elaborated research. Numerical simulation was conducted to make a comparison of cooling effectiveness between two effused cooling models: porous plate model and inclined-multi holes model with the same coolant mass flow rate. For the porous plate model, the flow resistance for porous plate was simulated with the packed bed formula, and the porosity studied was 0.33. For the inclined-multi holes model, the geometry consisted of 10 rows of cylindrical round holes in staggered arrangement, which were angled at 20 degree. The study covered 4 blowing ratio of M=0.5, 1.0, 1.5, 2.0, and the coolant-to-mainstream density ratio was equal to 2. The influence of Reynolds number within the coolant duct was considered by covering the case of Rec=3000. The 3 dimension geometric models were meshed with a structured, multi-block grid containing about 1 million elements for inclined-multi holes model and 0.3 million elements for porous plate model. The steady state Reynolds- averaged Navier-Stokes equations with turbulence closure of RNG k-ε turbulence model were solved with the aid of FLUENT.Based on the laterally averaged cooling effectiveness over the investigated plate, the two effused cooling models studied in this paper were much higher comparing with the traditional slot film cooling. Detailed flow and heat transfer characteristics of the two effused cooling models were compared.
机译:虽然已经证明了离散孔和槽膜冷却都是有效的冷却方法,但随着现代燃气轮机的涡轮机入口温度的增加,对涡轮机叶片冷却的进一步改善的强劲需求存在。通过用多孔壁替换冷却表面来冷却,可以是下一代高温燃气涡轮机的最佳选择,用于其较大且均匀分布的冷却效果。全覆盖薄膜冷却已被切断为G类燃气轮机的主要外部冷却方法。但是在燃气轮机叶片冷却中的蒸腾冷却的实施需要阐述的研究。进行了数值模拟以进行两个活化冷却模型之间的冷却效果:多孔板模型和具有相同冷却剂质量流速的倾斜多孔模型。对于多孔板模型,用填充床配方模拟多孔板的流动阻力,研究的孔隙率为0.33。对于倾斜多孔模型,几何形状由10行的圆柱形圆孔组成,以交错的布置,其在20度上成角度。研究覆盖了4个吹气比为m = 0.5,1.0,1.5,2.0,冷却剂 - 主流密度比等于2.通过覆盖Rec = 3000的情况,考虑了冷却剂管道内的雷诺数的影响。用结构化的多块网格啮合3尺寸几何型号,其含有约100万个元素的用于倾斜多孔模型和0.3亿个多孔板模型的元件。通过流利的借助于流利的稳定状态雷诺平均湍流闭合RNG k-ε湍流模型的循环方程。基于所研究的横向平均冷却效果,在本文中研究的两个活化冷却模型与传统的槽膜冷却比较得多。比较了两个活化冷却模型的详细流动和传热特性。

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