Integrated Influence Mechanism of Typical Parameters on Sealing Effectiveness of Rim Seal

被引:0
|
作者
Dong W.-L. [1 ]
Wang S.-F. [1 ]
Xia Z.-L. [1 ]
机构
[1] Ministry of Industry and Information Technology, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing
来源
关键词
Fetter effect; Ingestion; Inner ring; Rim seal;
D O I
10.13675/j.cnki.tjjs.180442
中图分类号
学科分类号
摘要
In order to have a good understanding of the integrated influence mechanism of the typical parameters on sealing effectiveness of rim seal, the internal relationship between the ingestion form and the vortex structure in sealing gap was studied and revealed by numerical method. On this basis, an inner ring rim seal was designed. The results show that not only increasing rotation speed but also increasing mainstream mass flow will lead to the reduction of the sealing efficiency, but the role of the two is to fetter each other. Compared with conventional orifice model, the inner ring rim seal utilize fetter effect to widen the work condition range of the high sealing efficiency by restricting the recirculation vortex in the sealing gap. Thus the sealing effectiveness was improved. © 2019, Editorial Department of Journal of Propulsion Technology. All right reserved.
引用
收藏
页码:1293 / 1299
页数:6
相关论文
共 17 条
  • [1] Bohn D., Decker A., Ma H., Et al., Influence of Sealing Air Mass Flow on the Velocity Distribution in and Inside the Rim Seal of the Upstream Cavity of a 1.5-Stage Turbine
  • [2] Dittmann M., Dullenkopf K., Wittig S., Discharge Coefficients of Rotating Short Orifices with Radiused and Chamfered Inlets, Journal of Engineering for Gas Turbines & Power, 126, 4, pp. 803-808, (2004)
  • [3] Bricaud C., Richter B., Dullenkopf K., Et al., Stereo PIV Measurements in an Enclosed Rotor-Stator System with Pre-Swirled Cooling Air, Experiments in Fluids, 39, 2, pp. 202-212, (2005)
  • [4] Bohn D.E., Decker A., Ohlendorf N., Et al., Experimental Investigations of the Influence of Sealing Air Mass Flow on the Adiabatic Wall Temperature Distribution on the Surface of the Rotor Blisk in a 1.5 Stage Turbine
  • [5] Da S., Andreini F., Turbine Stator Well CFD Studies: Effects of Coolant Supply Geometry on Cavity Sealing Performance
  • [6] Jeffrey A.D., Antonio G.V., Andreas B., Et al., Heat Transfer in Turbine Hub Cavities Adjacent to the Main Gas Path
  • [7] Eastwood D., Coren D.D., Long C.A., Et al., Experimental Investigation of Turbine Stator Well Rim Seal, Re-Ingestion and Interstage Seal Flows Using Gas Concentration Techniques and Displacement Measurements
  • [8] Idris A., Pullen K., Barnes D., An Investigation into the Flow Within Inclined Rotating Orifices and the Influence of Incidence Angle on the Discharge Coefficient, Journal of Power & Energy, 218, 1, pp. 55-68, (2004)
  • [9] Owen J.M., Prediction of Ingestion through Turbine Rim Seals, Part 1: Rotationally-Induced Ingress, Journal of Turbomachinery, 131, 3, pp. 1083-1093, (2009)
  • [10] Owen J.M., Prediction of Ingestion Through Turbine Rim Seals, Part 2: Externally Induced and Combined Ingress, Journal of Turbomachinery, 133, 2, pp. 1983-1995, (2011)