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Experimental Study of the Performance-Improvement of the Abrasive Blasting Nozzle

연마가공 노즐의 성능개선을 위한 실험적 연구

  • Lee, Jung-Jae (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Hong, Cheon-Wha (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Song, Myoung-Joon (Department of Aerospace and Mechanical Engineering, Graduate School, Korea Aerospace University) ;
  • Kwak, Ji-Young (Department of Aerospace and Mechanical Engineering, Graduate School, Korea Aerospace University) ;
  • Lee, Yeol (School of Aerospace and Mechanical Engineering, Korea Aerospace University)
  • 이정재 (한국항공대학교 항공우주 및 기계공학부) ;
  • 홍천화 (한국항공대학교 항공우주 및 기계공학부) ;
  • 송명준 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 곽지영 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 이열 (한국항공대학교 항공우주 및 기계공학부)
  • Received : 2016.09.30
  • Accepted : 2017.01.05
  • Published : 2017.04.30

Abstract

An experimental study has been carried out to improve the performance of a commercial abrasive blasting nozzle, by simply redesigning the nozzle's inner contour. The analytical 1-D code, that can evaluate both the frictional effects on the nozzle inner wall and the sphericity effects of the particle, is utilized to calculate the dynamics of the particle inside the nozzle. The analytical results are compared to the experimental ones, that were obtained from images of the particle streaklines downstream from the nozzle exit. It is noted that the particle velocity at the redesigned nozzle exit increases as compared to the original commercial nozzle.

Keywords

References

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Cited by

  1. Flow Characteristics of Double-Venturi Abrasive Blasting Nozzle vol.17, pp.2, 2018, https://doi.org/10.14775/ksmpe.2018.17.2.008