• Title/Summary/Keyword: 재순환 챔버 노즐

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Effect of Internal Flow inside Recirculation Chamber Nozzle for Automative Head Lamp on Cleaning Spray (자동차 헤드램프 세척용 재순환 챔버 노즐의 내부유동이 분무장에 미치는 영향)

  • Shin, J.H.;Lee, I.C.;Kang, Y.S.;Kim, J.H.;Koo, J.S.;Koo, J.Y.
    • Journal of ILASS-Korea
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    • v.16 no.2
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    • pp.90-96
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    • 2011
  • Atomized liquid jets from the washing nozzle which configured with recirculation chamber for cleaning hot-zone area are accelerated and impinged on the head lamp surface. Cleaning efficiency of head lamp can be increased with injecting washing fluids into the hot-zone area. Experimental and numerical studies with various design parameters were executed to reveal the relations between internal geometry and internal flow in the washing nozzle. Spray structures were fitted with each of the head lamp surfaces and spray nozzles were optimized to the spray pattern. The recirculation chamber induces a recirculation flow and can be decreased the pressures perturbation inside the chamber. Orifice determines the mass flow rate. When the diameter of orifice is excessively large, it showed an unstable spray pattern. As a nozzle exit angle increases, density distributions are separated with two section. Also, as a protrusion length of nozzle exit increases, spray patterns are spread into a large area and density distributions showed unstable trend.

The Influence of the Supply Chamber Configuration on Under-Expanded Swirling Jets (노즐 챔버 형상이 부족팽창 스월제트 유동에 미치는 영향에 관한 연구)

  • Kim, Jung-Bae;Lee, Kwon-Hee;Setoguchi, Toshiaki;Kim, Heuy-Dong
    • Proceedings of the KSME Conference
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    • 2003.11a
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    • pp.586-591
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    • 2003
  • The present study addresses experimental results to investigate the effect of the jet supply chamber configuration on the sonic/supersonic swirling jets, as the case study. The experiment is carried out using the convergent nozzle with a various different chamber configurations upstream the nozzle throat, which is composed of four tangential inlet holes for the swirling flows. The jet pressure ratio is varied between 3.0 and 7.0. The sonic/supersonic swirling jet flows are specified by the pitot impact and static pressure measurements and visualized using the Shadowgraph method. The results show that the major structures of the sonic/supersonic swirling jet are strongly influenced by the jet supply chamber.

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