Turbine Nozzle Insert Clogging With Seeded Medium Size Particles

Hongzhou Xu, Kevin Liu, M. Fox
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Abstract

Gas turbine nozzle cooling often uses inserts to intentionally distribute cool air through impingement holes to hot spots, especially at leading edge regions of stage-1 nozzles. Owing to the variations of engine operation environment, inlet air filtration systems, upstream component surface coating layers, and oil/air sealing material choices, solid particles could enter the engine from outside or be generated inside from rotor rubbing, seal debris, peeled off coating layers or rusty surfaces, etc. These particles and their agglomerates can be carried by airflow to enter nozzle inserts and clog impingement holes, which may reduce cooling air significantly, resulting in severe engine failures. To reduce the risk of insert clogging, particle separation devices and filtration mesh screens have been implemented in front of nozzle inlets to prevent larger particles from entering. Therefore, designing appropriate nozzle insert hole sizes becomes very critical to let smaller particles pass through and exhaust from the nozzle exit. This experimental study focuses on finding a correlation between the impingement hole sizes of a nozzle insert and their clogged areas caused by seeded fine and medium size particles of Fe2O3 under specific pressure ratios. A nozzle insert was first chosen, and a single row of cylindrical impingement holes was machined at the leading edge of the insert. Measurements were conducted in a pressurized vessel at Reynolds numbers from 7,000 to 62,000 and pressure ratios from 1.01 to 1.10. Results indicate that insert clogging is a strong function of the hole size, particle size, and pressure ratio. The tested particles showed a bimodal distribution of fine and medium sizes, and the medium size particles played a major role in clogging holes. A clogging diagram with 3 zones (fully clogged zone, partially clogged zone, and no clogging zone) is generated from the test data, which can provide important design criteria for sizing the insert leading edge impingement holes to reduce the risk of clogging.
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涡轮喷嘴插入物被播种的中等大小颗粒堵塞
燃气轮机喷管冷却通常使用插片有意地通过冲击孔将冷气分配到热点,特别是在一级喷管的前缘区域。由于发动机运行环境、进气过滤系统、上游部件表面涂层、油气密封材料选择的不同,固体颗粒可能从外部进入发动机,也可能由转子摩擦、密封件碎屑、涂层脱落或生锈表面等在发动机内部产生。这些颗粒及其结块可被气流携带进入喷嘴镶件并堵塞撞击孔,这可能会显著减少冷却空气,导致严重的发动机故障。为了降低喷嘴堵塞的风险,在喷嘴入口前安装了颗粒分离装置和过滤网,以防止更大的颗粒进入。因此,设计合适的喷嘴插入孔尺寸变得非常关键,以使较小的颗粒通过并从喷嘴出口排出。本实验研究的重点是在特定压力比下,寻找喷嘴插入物的撞击孔尺寸与颗粒中、细颗粒Fe2O3造成的堵塞面积之间的关系。首先选择喷嘴插入件,在插入件的前缘加工单排圆柱撞击孔。测量在一个压力容器中进行,雷诺数从7000到62000,压力比从1.01到1.10。结果表明,钻头堵塞与井眼尺寸、颗粒尺寸和压力比密切相关。试验颗粒呈细粒和中粒双峰分布,中粒对孔洞堵塞起主要作用。根据试验数据,生成了3个区域(完全堵塞区、部分堵塞区和未堵塞区)的堵塞图,为确定刀片前缘撞击孔的尺寸提供了重要的设计依据,以降低堵塞风险。
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