首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >INTRODUCING A NEW TEST RIG FOR FILM COOLING MEASUREMENTS WITH REALISTIC HOLE INFLOW CONDITIONS
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INTRODUCING A NEW TEST RIG FOR FILM COOLING MEASUREMENTS WITH REALISTIC HOLE INFLOW CONDITIONS

机译:引入一种新的试验台,用于具有真实孔渗入条件的薄膜冷却测量

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Further improvements in film cooling require an in-depth understanding of the influencing parameters. Therefore, a new test rig has been designed and commissioned for the assessment of novel film cooling holes under realistic conditions. The test rig is designed for generic film cooling studies. External hot gas flow as well as internal coolant passage flow are simulated by two individual flow channels connected to each other by the cooling holes. Based on a similarity analysis, the geometry of the test rig is scaled up by a factor of about 20. It furthermore offers the possibility to conduct experiments at high density ratios and realistic approach flow conditions at both cooling hole exit and inlet. The operational range of the new test rig is presented and compared to real engine conditions. It is shown that the important parameters are met and the transferability of the results is ensured. Special effort is put onto the uniformity of the approaching hot gas flow, which will be demonstrated by temperature and velocity profiles. A first measurement of the heat transfer coefficient without film cooling is used to demonstrate the quality of the measurement principle.
机译:薄膜冷却的进一步改进需要对影响参数有深入的了解。因此,已经设计并调试了一种新的测试设备,用于在实际条件下评估新型薄膜冷却孔。该试验台专为通用薄膜冷却研究而设计。外部热气流和内部冷却剂通道流是通过两个单独的流道模拟的,两个流道通过冷却孔相互连接。根据相似性分析,试验台的几何尺寸将扩大约20倍。它还提供了在冷却孔出口和入口处以高密度比和实际进水条件进行实验的可能性。介绍了新测试台的运行范围,并将其与实际发动机条件进行了比较。结果表明,满足了重要参数并确保了结果的可传递性。将特别努力处理接近的热气流的均匀性,这将通过温度和速度曲线来证明。在没有薄膜冷却的情况下对传热系数的首次测量用于证明测量原理的质量。

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