首页> 外文会议>International Symposium on Jet Propulsion and Power Engineering >NUMERICAL INVESTIGATION OF THE EFFFECTIVENESS OF EFFUSION COOLING FOR PLANE MULTI-LAYER SYSTEMS WITH DIFFERENT BASE-MATERIALS
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NUMERICAL INVESTIGATION OF THE EFFFECTIVENESS OF EFFUSION COOLING FOR PLANE MULTI-LAYER SYSTEMS WITH DIFFERENT BASE-MATERIALS

机译:不同基底材料的平面多层系统渗流冷却效果的数值研究

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Within Collaborative Research Center (SFB) 561 "Thermally Highly Loaded, Porous and Cooled Multi-Layer Systems for Combined Cycle Power Plants" at RWTH Aachen University an effusion-cooled multi-layer plate configuration is investigated numerically by application of a 3-D in-house fluid flow and heat transfer solver, CHTflow. The geometrical setup and the fluid flow conditions derive from modem gas turbine combustion chambers and bladings.Within the SFB two different multi-layer systems have been investigated: one system consisting of substrate made of CMSX-4 (a single-crystal super-alloy), an MCrAlY-bondoat and a ZrO2 thermal barrier coating and one system consisting of a NiAl-alloy and a graded bondcoat/TBC. The grading will increase the life-span of the TBC as it can compensate the different thermal expansion coefficients of the different materials better. The main focus in this study is on the different substrate materials, though: the thermal conductivity of the NiAl is considerably higher than that of CMSX-4, which leads to different temperature profiles in the components.The numerical grid for the simulations contains the coolant supply (plenum), the solid body for the conjugate calculations and the main flow area on the plate. The effusion-cooling is realized by finest drilled shaped holes with a diameter of 0.2 mm.The investigations concentrated on a cooling hole geometry with a laterally-widened fan-shaped outlet, contoured throughout and one without lateral widening that is only shaped in the top 0.25 of the system. Two blowing ratios M=0.28 and M=0.48 were investigated, both for a hot gas Maeh number of 0.25. The results for the lower blowing ratio and the fully contoured hole will be discussed here as well as those of the higher blowing ratio and the non-laterally widened hole. These represent two characteristic cases.The in-house code CHTflow is used for these calculations.CHTflow is a conjugate code, which yields information on the temperature distribution in the solid body. This enables a detailed discussion of the effects of a change in materials.
机译:在亚琛工业大学(RWTH Aachen University)合作研究中心(SFB)561“联合循环发电厂的热高负荷,多孔和冷却的多层系统”中,通过应用3D技术对渗出冷却的多层板结构进行了数值研究。内部流体流动和热传递求解器CHTflow。几何设置和流体流动条件来自现代燃气轮机的燃烧室和叶片。在SFB中,研究了两种不同的多层系统:一种由CMSX-4(单晶超合金)制成的基底组成的系统,MCrAlY-bondoat和ZrO2隔热涂层,以及一个由NiAl合金和渐变粘结层/ TBC组成的系统。分级将增加TBC的寿命,因为它可以更好地补偿不同材料的不同热膨胀系数。但是,本研究的主要重点是不同的基材材料:NiAl的热导率明显高于CMSX-4的热导率,这导致组件中的温度曲线不同。模拟的数字网格包含冷却液供给(增压),用于共轭计算的固体和板上的主流动面积。积液冷却是通过直径为0.2 mm的最细的钻孔实现的,研究集中在冷却孔的几何形状上,该几何形状具有侧向扩展的扇形出口,整个出口轮廓化,并且没有横向扩展,仅在顶部成形系统的0.25。研究了两种吹气比M = 0.28和M = 0.48,两者的热气Maeh数均为0.25。此处将讨论较低吹气比和全轮廓孔的结果,以及较高吹气比和非横向扩孔的结果。这代表了两种典型情况。内部代码CHTflow用于这些计算.CHTflow是共轭代码,可得出有关固体中温度分布的信息。这样就可以详细讨论材料变更的影响。

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