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A Study of the Tip Clearance Effect to the Performance of an Axial-Type Fan

축류형 송풍기의 익단간극이 성능에 미치는 영향에 관한 연구

  • 조종현 (경상대학교 대학원) ;
  • 정양범 (세보금속주식회사 기술연구소) ;
  • 김영철 (한국기계연구원 회전체기계연구팀) ;
  • 조수용 (경상대학교 항공기부품기술연구센터(기계항공공학부))
  • Published : 2008.12.01

Abstract

Fan performances are obtained with various tip clearance gaps and stagger angles of the rotor. A tested fan is an axial-type fan of which the casing diameter is 806 mm. Two different rotors are applied to this test. One is designed on the basis of the free vortex method along the radial direction and the other is designed using the forced vortex method. The operating conditions are varied to the ultimate off-design point as well as the deign point. Overall efficiency, total pressure and input power are compared with the tip clearance gaps and different stagger angle. The experimental results show that changing of the stagger angle has minor influence to the performance when the same rotor is applied. When the tip clearance gap is less than 5% of the rotor span, the overall efficiency, total pressure loss and input power reduction are varied linearly with the variation of the tip clearance gaps. On the design point, the overall efficiency is decreased to the rate of 2.8-2.9 to the increasing of the tip clearance, but the changing rate of the overall efficiency is alleviated when the fan operates at off-design points. In particular, this rate is more quickly declined on a fan with the rotor designed using the forced vortex method. The result of the total pressure shows that the pressure reduction rate is a 0.08-0.1 according to the tip clearance, and additionally the input power reduction rate is a 0.045-0.065 at design point.

Keywords

References

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