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ADVANCED LINER COOLING NUMERICAL ANALYSIS FOR LOW EMISSION COMBUSTORS

机译:低排放燃烧器的高级内胆冷却数值分析

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The aim to reach very low emission limits has recently changed several aspects of combustor fluid dynamics. Among them, combustor cooling experienced significant design efforts to obtain good performances with unfavourable conditions. This paper deals with simplified 1D and complete 3D conjugate numerical simulations of effusion cooling configurations, performed in the first two years of the European research project INTELLECT DM. Geometries are derived from typical LPP combustor cooling configurations, which feature low coolant mass flow rate and high pressure losses (compared to typical blade cooling parameters). Results are obtained in terms of local distributions of effectiveness and discharge coefficient. Comparison among simulations allowed to derive useful indications on overall effectiveness behaviour. The configuration simulated in this paper represents a combustor liner with effusion cooling: the plate tested on the CNRS-LCD test rig of Poitiers is composed by two different patterns of effusion cooling. Furthermore, to be the most representative of a combustor chamber, an air flow bleed at the exit of the cold flow is introduced. On the investigated plate SNECMA performed 3D conjugate (coupling fluid/thermal) calculations using a 3D CFD code named N3S-Natur and ABAQUS, a well known 3D thermal code. The codes take into account the effusion cooling area as an homogenous wall described by a permeability, a discharge coefficient for the CFD code and a convective flow (h_(con), T_(con)) for the thermal one. That means that such simulations are not solving the flow inside each hole. The fluid code also enables to compare the experimental adiabatic effectiveness measurements on this plate, but the aim is before all the overall effectiveness. Conjugate calculations were also performed by means of a procedure employing 1D correlative fluid analysis and 2D metal conduction study. Finally, complete 3D CFD conjugated calculations has been carried out on the plate to verify the validity of assumptions and results obtained with simplified approaches previously exposed.
机译:达到极低排放限值的目标最近改变了燃烧室流体动力学的几个方面。其中,燃烧室冷却经历了巨大的设计努力,以在不利的条件下获得良好的性能。本文讨论了在欧洲研究项目INTELLECT DM的前两年中对积液冷却配置进行的简化1D和完整3D共轭数值模拟。几何形状源自典型的LPP燃烧器冷却配置,其特征在于低冷却液质量流量和高压力损失(与典型的叶片冷却参数相比)。根据有效性和排放系数的局部分布获得结果。模拟之间的比较可以得出有关整体有效性行为的有用指示。本文中模拟的配置代表具有喷射冷却的燃烧室衬套:在Poitiers的CNRS-LCD测试台上测试的板由两种不同的喷射冷却模式组成。此外,作为最有代表性的燃烧室,引入了在冷气流出口处排出的气流。在研究的板上,SNECMA使用名为N3S-Natur的3D CFD代码和ABAQUS(一种众所周知的3D热代码)执行了3D共轭(流体/热耦合)计算。规范考虑了渗流冷却区域,即均匀的壁,由渗透率,CFD规范的排放系数和热流的对流(h_(con),T_(con))描述。这意味着这种模拟无法解决每个孔内的流动问题。流体代码还可以比较此板上的绝热效果实验测量值,但目标是获得全部总体效果。共轭计算也通过采用一维相关流体分析和二维金属传导研究的程序进行。最后,已经在板上进行了完整的3D CFD共轭计算,以验证假设和使用先前公开的简化方法获得的结果的有效性。

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