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Influence of Tip Clearance on Performance of a Contra-Rotating Fan 被引量:6

Influence of Tip Clearance on Performance of a Contra-Rotating Fan
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摘要 Influences of tip clearance on the tip flow and associated loss mechanism in a contra-rotating axial flow fan hasbeen studied in the paper, based on three dimensional numerical results. The results with different tip clearanceare compared in terms of stage efficiency, relative total pressure loss coefficient, flow angle. It is found that theefficiency of the contra-rotating fan changes almost linearly with increment of the tip clearance, however, efficiencyof the rear rotor is observed to decrease more dramatically than that of the forward rotor given same tipclearance variation. The analysis on the flow structure indicates that the tip region flow field is qualitatively similarin both rotors. However, with the same clearance value, the leakage flow in the rear rotor is effected by a tipleakage vortex of greater intensity caused by relative loading levels and the inter rotor interaction.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2009年第3期207-214,共8页 热科学学报(英文版)
关键词 contra-rotating fan tip clearance PERFORMANCE tip leakage flow 间隙 旋转 总压损失系数 风扇 性能 流动结构 轴流风机 数值结果
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参考文献7

  • 1Sharma P B, Dekoya A. A.: A Review of Recent Kesearcn on Contra-Rotating Axial Flow Compressor Stage, ASME, 96-GT-254, (1996).
  • 2Roy B, Agrawal L A.: Casing Boundary Layer Control by Recess Vaned Casing for a Twin-Rotor Contra-Rotating Axial Flow Fan Unit, ASME, 94-GT-478, (1994).
  • 3Wisler, D. C.: Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing, ASME, J. Eng, Gas Turbines and Power, vol.107, pp. 354-363, (1985).
  • 4Inoue M, Kuroumaru M, Fukuhara M.: Behavior of Tip Leakage Flow behind an Axial Compressor Rotor, ASME, 85-GT-62, (1985).
  • 5Kang, S., Hirsch, C.: Experimental Study on the Three- Dimensional Flow within a Compressor Cascade with Tip Clearance: Part I -Velocity and Pressure Fields, ASME, J. Turbomachinery, vol. 115, pp. 435-443, (1993).
  • 6Kang, S., Hirsch, C.: Experimental Study on the Three- Dimensional Flow within a Compressor Cascade with Tip Clearance: Part II-the Tip Leakage Vortex, ASME, J. Turbomachinery, vol. 115, pp. 444-452, (1993).
  • 7Chang, Z. Z.: Axial Flow Fans Design Technology, China, Mechanical Industry Press, Beijing, (2005) in Chinese.

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