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Louver Slot Cooling and Full-Coverage Film Cooling With a Combination Internal Coolant Supply

机译:百叶窗槽冷却和全覆盖薄膜冷却,带有组合内部冷却剂供应

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摘要

Within the present investigation; a louver slot is employed upstream of an array full-coverage film cooling holes. Cooling air is supplied using a combination arrangement; with cross-flow and impingement together. The louver consists of a row of film cooling holes; contained within a specially designed device that concentrates and directs the coolant from a slot; so that it then advects as a layer downstream along the test surface. This louver-supplied coolant is then supplemented by coolant which emerges from different rows of downstream film cooling holes. The same coolant supply passage is employed for the louver row of holes; as well as for the film cooling holes; such that different louver and film cooling mass flowrates are set by different hole diameters for the two different types of cooling holes. The results are different from data provided by past investigations; because of the use and arrangement of the louver slot; and because of the unique coolant supply configurations. The experimental results are given for mainstream Reynolds numbers from 107;000 to 114;000. Full-coverage blowing ratios are constant with stream-wise location along the test surface and range from 3.68 to 5.70. Corresponding louver slot blowing ratios then range from 1.72 to 2.65. Provided are heat transfer coefficient and adi-abatic effectiveness distributions; which are measured along the mainstream side of the test plate. Both types of data show less variation with streamwise development location; relative to results obtained without a louver employed; when examined at the same approximate effective blowing ratio; mainstream Reynolds number; cross-flow Reynolds number; and impingement jet Reynolds number. When compared at the same effective blowing ratio or the same impingement jet Reynolds number; spanwise-averaged heat transfer coefficients are consistently lower; especially for the downstream regions of the test plate; when the louver is utilized. With the same type of comparisons; the presence of the louver slot results in significantly higher values of adiabatic film cooling effectiveness (spanwise-averaged); particularly at and near the upstream portions of the test plate. With such characteristics; dramatic increases in thermal protection are provided by the presence of the louver slot; the magnitudes of which vary with the experimental condition and test surface location.
机译:在目前的调查中;百叶窗槽在阵列全覆盖膜冷却孔的上游采用。使用组合装置提供冷却空气;用交叉流动和冲击在一起。百叶窗由一排薄膜冷却孔组成;包含在专门设计的装置内,从槽中专注并引导冷却剂;这样它就会推进沿着测试表面下游的层。然后通过从不同行的下游薄膜冷却孔中出来的冷却剂来补充这种百叶窗供应的冷却剂。相同的冷却剂供应通道用于百叶窗孔;以及薄膜冷却孔;这样的不同的百叶窗和薄膜冷却质量流量由不同类型的冷却孔的不同孔直径设定。结果与过去调查提供的数据不同;由于百叶窗槽的使用和布置;并且由于唯一的冷却剂供应配置。将实验结果为107; 000至114; 000的主流雷诺数。全覆盖吹率呈沿着测试表面的流式位置,范围为3.68至5.70。相应的百叶窗槽吹量比率从1.72到2.65。提供的是传热系数和ADI-避免效果分布;沿着测试板的主流侧测量。两种类型的数据显示得更少的变化,流动开发位置;相对于没有百叶窗获得的结果;当以相同的近似有效吹出比例检查时;主流雷诺数;横流雷诺数;和冲击喷射雷诺数。在相同的有效吹吹比或相同的冲击喷射雷诺数相比时;翼展平均传热系数始终更低;特别是对于测试板的下游区域;当百叶窗被使用时。具有相同类型的比较;百叶窗槽的存在导致绝热膜冷却效果的显着较高值(跨越平均);特别是在测试板的上游部分附近。具有这样的特点;通过Louver槽的存在提供了热保护的剧烈增加;其大小随着实验条件和测试表面位置而变化。

著录项

  • 来源
    《Journal of turbomachinery》 |2021年第3期|031004.1-031004.10|共10页
  • 作者单位

    Propulsion Research Center Department of Mechanical and Aerospace Engineering 5000 Technology Drive Olin B King Technology Hall University of Alabama in Huntsville Huntsville AL 35899;

    Propulsion Research Center Department of Mechanical and Aerospace Engineering 5000 Technology Drive Olin B. King Technology Hall University of Alabama in Huntsville Huntsville AL 35899;

    Propulsion Research Center Department of Mechanical and Aerospace Engineering 5000 Technology Drive Olin B. King Technology Hall S236 University of Alabama in Huntsville Huntsville AL 35899;

    Propulsion Research Center Department of Mechanical and Aerospace Engineering 5000 Technology Drive Olin B. King Technology Hall S236 University of Alabama in Huntsville Huntsville AL 35899;

    Propulsion Research Center Department of Mechanical and Aerospace Engineering 5000 Technology Drive Olin B King Technology Hall S236 University of Alabama in Huntsville Huntsville AL 35899;

    Propulsion Research Center Department of Mechanical and Aerospace Engineering 5000 Technology Drive Olin B. King Technology Hall S236 University of Alabama in Huntsville Huntsville AL 35899;

    Combustion Engineering Solar Turbines Incorporated 2200 Pacific Highway Mail Zone E-4 San Diego CA 92186-5376;

    Combustion Engineering Solar Turbines Incorporated 2200 Pacific Highway Mail Zone E-4 San Diego CA 92186-5376;

    Combustion Engineering Solar Turbines Incorporated 2200 Pacific Highway Mail Zone E-4 San Diego CA 92186-5376;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    heat transfer; louver slot cooling; film cooling; effusion cooling; combustor liner; thermal protection; impingement jets; cross flow cooling;

    机译:传播热量;百叶窗槽冷却;薄膜冷却;流水冷却;燃烧器衬里;热保护;冲击喷射器;交叉流冷却;

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