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Parametric Study of Combustor Machined Ring Film-Cooling with TBC

机译:用TBC的燃烧室加工环膜冷却的参数研究

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Through the set up of a calculation model on film cooling in the primary zone of an annular combustor, a parametrical study was made on the relationship of film cooling effectiveness and wall temperature with configuration parameters such as cooling slot height and TBC thickness. Through parametrical study, it can be seen that with all the parameters kept the same and even the resulting effectiveness of the outer liner slightly greater due to a slightly higher blow ratio, the outer liner temperatures are considerably higher than the inner liner temperatures. The calculation shows, with cooling effectiveness, there are optimum values of coolant injection angle and film cooling slot height, while there is a monotonous tendency for the relationship of cooling effectiveness with other parameters such as tapered angle on nugget lip, starting edge angle at nugget-slot exit and lip thickness.The study demonstrates that the higher the TBC thickness, the lower the highest value of base metal temperatures, but when the TBC thickens, it becomes heavier, and the possibility of TBC spallation gets greater.
机译:通过在环形燃烧器的主区内的薄膜冷却中建立计算模型,对薄膜冷却效果和壁温的关系进行了参数研究,诸如冷却槽高度和TBC厚度的配置参数。通过参数研究,可以看出,由于吹吹比略高,外衬里温度远远高于外衬里的所有参数甚至导致的外衬里的效率甚至稍高。该计算表明,具有冷却效果,冷却剂注入角度和薄膜冷却槽高度有最佳值,而具有冷却效果与其他参数的关系的单调倾向,如块润滑尾,在纽扣环的开始边角-Slot出口和唇厚。研究表明,TBC厚度越高,基础金属温度的最高值越低,但是当TBC增厚时,它变得更重,并且TBC椎间体的可能性变得更大。

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