• 제목/요약/키워드: 선회 분무식 노즐

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Urea-SCR시스템 액막형 선회분사기의 분사압력변화에 따른 무특성에 관한 연구 (Effect of injection pressure on the atomization characteristics of a liquid sheet-type swirl injector for Urea-SCR system)

  • 김덕진;양동욱;이지근
    • Journal of Advanced Marine Engineering and Technology
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    • 제37권5호
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    • pp.510-519
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    • 2013
  • Urea-SCR시스템에 적용하기 위한 액막형 선회분사기의 분사압력변화에 따른 분무특성이 실험적으로 조사되었다. 실험에 사용된 노즐은 형상비 3.1을 갖는 단공 압력식 액막형 선회노즐이며, 노즐선단에 분사되는 유체에 선회류를 형성하기 위한 선회기가 설치되어 있다. 노즐의 분사량 조절은 PWM(pulse width modulation)기법에 의해 제어되었다. 분무의 발달과정은 2차원 PIV에 의해 가시화되었으며, 분무각 변화가 조사되었다. 분무액적의 속도 및 크기는 2차원 PDPA에 의해 상온 대기압 조건에서 측정되었다. 분무구조는 분사압력에 큰 영향을 받으며, SMD는 분사압력 증가에 따라 감소하며 선행연구자의 반실험적 결과와 유사한 경향을 보임을 알 수 있었다.

저 NOx2단 선회 분무식 노즐 개발 및 실기적용 연구 (A Study for Development and Application of a Low NOx 2-staged Swirl Atomizer)

  • 송시홍;김혁필;안상택;이익형
    • 대한기계학회논문집B
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    • 제25권12호
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    • pp.1793-1801
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    • 2001
  • A study of low NOx atomizer was carried out to reduce nitrogen oxides(NOx) in a liquid fuel burner flame. The basic concept of NOx reduction in this atomizer is the fuel 2-staging combustion which is generated by a single atomizer forming two different stoichiometric flames. Two orifices swirl atomizer was selected and modified to realize this concept, and it was tested to obtain the design process of low NOx atomizer. These experiments were achieved to find out the relationship between the injection pressures and the flow rate, spray angle and drop size of swirl atomizer as well as to confirm the NOx reduction concept in real plant(power boiler). In comparison between experimental and theoretical results, the correct discharge coefficient and spray angle were obtained. In real burning test, NOx reduction rate was reached to above 27% of the case using conventional swirl atomizer.

경사노즐 선회분사기의 가솔린 분무 특성 (The Gasoline Spray Characteristics of Tapered Nozzle for a Swirl Injector)

  • 문석수;최재준;배충식
    • 한국분무공학회지
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    • 제12권1호
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    • pp.11-17
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    • 2007
  • The swirl spray for direct-injection spark-ignition (DISI) engines was investigated using a nozzle whose exit surface shape was cut with a certain tapered angle. The reason for the change in spray's characteristics at various tapered angles was explained by the data correlating the taper and flow angles. The spray tended to shift its characteristics from the symmetric to asymmetric when the tapered angle was increased; furthermore, the spray penetration and spray cone angle were also increased. When the tapered angle was greater than the $90^{\circ}$ minus flow angle, an opened hollow cone spray was formed because of the fuel impingement against the tapered surface area of the nozzle exit. This behavior indicates that the reduction in the air pressure difference between the inner and outer spray of the spray can be achieved. This behavior also promises the potential use of the tapered nozzle for the case where the independence of the spray performance from atmospheric pressure and fuel temperature is desired.

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경사노즐 선회분사기의 가솔린 미립화 및 분무 내부 압력 분포 (The Gasoline Atomization Characteristics and Static Pressure Distribution of Tapered Nozzle Swirl Spray)

  • 문석수;최재준;배충식
    • 대한기계학회논문집B
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    • 제31권3호
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    • pp.283-291
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    • 2007
  • The static pressure distribution, atomization characteristics and velocity distribution of tapered nozzle swirl spray is analyzed and then compared with original swirl spray. The static pressure distribution inside the swirl spray is measured using a piezoresistive pressure transducer. Phase Doppler anemometry (PDA) is applied to measure and analyze the droplet size and velocity distribution of tapered nozzle and original swirl spray. The static pressure inside the spray shows the lower value compared to the atmospheric pressure and this pressure drop is getting attenuated as the taper angle is increased. The droplet size of tapered nozzle spray shows similar value compared to the original swirl spray at the horizontal mainstream while it shows increased value at vertical mainstream. The deteriorated atomization characteristics of tapered nozzle spray is improved by applying high fuel temperature injection without causing the spray collapse. The velocity results show that the larger portion of fuel is positioned with higher injection velocity, and the smaller portion of fuel is positioned with lower injection velocity with causing spatially non-uniform mixture distribution.