• Journal of Advanced Marine Engineering and Technology
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• 제8권2호
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• pp.88-97
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• 1984

The combustion process and the performance of a diesel engine are considerably affected by the characteristics of fuel spray. It is known that the spray of swirl nozzle for diesel engine injector of small orifice ratio becomes soft spray that has no core, therefore its penetration, one of the characteristics of spray becomes werse inspite of its good dispersion. In this paper, the spray characteristics of variously designed swirl nozzle for diesel injector were investigated by the photographic method. The nozzles, used in this experiment, vary in the diameter of swirl chambers and orifice ratio. From the results of the study, the sprays of this type nozzle of optimum swirl chamber and orifice ratio show that penetration decreased slightly but dispersion and spray volume increased remarcably, compared with unswirled single hole nozzle of the same size. It was suggested as a reason for the results, that the spray of this type swirl nozzle is similar to hard spray, therefore the core of the spray sustains good penetration considerably.

• 대한기계학회논문집B
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• 제26권12호
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• pp.1655-1662
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• 2002

Recently, many researches have been performed to improve the performance of the combustion and emission in a D.I.Diesel engine. And many new techniques have been introduced and developed to reduce NO$_{x}$ and soot exhausted from diesel combustion. Some of these methods have the peculiar injection timing which is not used to traditional timing. To optimize these injection timing, characteristics of swirl flow and interaction of swirl with injection in the diesel engine should be investigated more carefully. Therefore, in this study, 2-zone energy method is adopted for the understanding of swirl flow in condition of moving piston, and then flame visualizations and image process are performed. From these studies, the characteristics of the swirl flow generated by SCV was investigated and the effect of swirl on injection timing was elucidated. As the results, velocity distribution caused by swirl flow increase the space utilization rate of flame plums. And flame plums of weak momentum are remained inside of combustion chamber by the swirl flow.w.

• 대한기계학회논문집B
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• 제26권3호
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• pp.458-464
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• 2002

Recently, many researches have been performed to improve performances of the combustion and emission in the D.I.Diesel engine. Especially reduction of the soot formation in tole combustion chamber is the essential to acquire the improvement of the emission performance. These emission of the diesel combustion is effected by the characteristics of air-fuel mixing. Thus, in this study, the distribution of soot in the diesel combustion is measured by LII(laser induced incandescence) and LIS(Laser induced scattering) method. From this experimental results, it is confirmed that the swirl flow intensified by SCV(swirl control valve) is effective on the reduction of soot in the combustion chamber.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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• pp.177-180
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• 2010

혼합비와 연소압에 따른 이중 와류 동축 분사기의 유량계수 변화를 살펴보았다. 연료 과농 조건에서 액체산소와 케로신을 이용하여 이중 와류 동축 분사기의 연소시험을 수행하였다. 두 종류의 분사기가 시험에 적용되었는데, 산화제 분무각 변화에 의한 추진제간 모멘텀 비 차이와 연료 노즐 직경 차이로 인한 유량계수 영향 특성이 파악되었다. 연료 와류실을 연료가 모두 채운 상태에서 연소가 이루어지는 경우 화염 구조의 변화가 없어 혼합비에 다른 유량계수 변화 또한 보이지 않는 것으로 파악하였다.

• 한국표면공학회지
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• 제36권1호
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• pp.69-73
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• 2003

The atmospheric pressure plasma is regarded as an effective method for surface treatments because it can reduce the period of process and doesn't need expensive vacuum apparatus. The performance of non-transferred plasma torches is significantly depended on jet flow characteristics out of the nozzle. In order to produce the high performance of a torch, the maximum discharge velocity near an annular gap in the torch should be maintained. Also, the compulsory swirl is being produced to gain the shape that can concentrate the plasma at the center of gas flow. In this work, the distribution of gas flow that goes out to atmosphere through a plenum chamber and nozzle is analyzed to evaluate the performance of atmospheric pressure plasma torch which can present the optimum design of the torch. Numerical analysis is carried out with various angles of an inlet flow velocity. Especially, three-dimensional model of the torch is investigated to estimate swirl effect. We also investigate the stabilization of plasma distribution. For analyzing the swirl in the plenum chamber and the flow distribution, FVM (finite volume method) and SIMPLE algorithm are used for solving the governing equations. The standard k-model is used for simulating the turbulence.

• 한국자동차공학회논문집
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• 제13권4호
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• pp.49-57
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• 2005

In this study, in-cylinder flow of the swirl chamber type diesel engine numerically simulated by VECTIS code. The flow fields during the intake and compression process were also investigated in detail. Numerical results revealed that the generation and distortion of the swirling, tumbling vortices and those influences on turbulence kinetic energy by shape of the jet passage, angle and area. It was also found that flow characteristics were affected by inflow velocity that depends on change of the jet passage shape. Swirl ratio was increased according to decrease of jet passage area, and was affected by piston motion according to increase of jet passage angle. Tumbling vortices had the similar in various cases, but tumble ratio was increased with the inflow velocity. The generation of turbulence kinetic energy was considerably influenced by complex effects of swirling and tumbling vortices.

• 산업기술연구
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• 제19권
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• pp.51-57
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• 1999

This research has an object to find out how the position of inlet valve influence swirling and tumbling of turbulence inside the combustion chamber of 4 valve engine. The computational analysis of three dimensional complicated turbulence flow in the cylinder is done by the KIVA-3V program to carry out this object. One use 6 valve positions with the bowl type of piston cavity. The swirl ration and the tumbling ratio of flow filed are evaluated quantitatively to find out how each valve position influence flow phenomena in the combustion chamber during the intake and compression processes.

• 한국추진공학회지
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• 제24권1호
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• pp.24-33
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• 2020

본 연구에서는 액체로켓엔진용 동축 와류형 분사기의 연소불안정 특성을 파악하기 위해 기체 추진제를 이용한 모델 연소실험을 수행하였다. 연소실 공진 주파수와 분사기 혼합조건의 영향을 알아보고자, 연소실 길이, 분사기, 리세스 길이, 추진제 혼합비를 변경하면서 연소실 압력섭동을 측정하였다. 실험 결과, 각 실험조건에 따른 압력섭동 변화를 확인하였으며 안정성 매핑을 통해 연소안정성을 평가하였다. 그리고 연소실 길이와 리세스 길이 변화에 따라 종방향 모드 및 켈빈-헬름홀츠 불안정이 발생함을 발견하였다.

• 한국농공학회지
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• 제17권4호
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• pp.3991-4000
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• 1975

It is the aim of this study to investigate the influence of the factors in the sprayer nozzle for the travelling distance and to get nozzle design data in relation to the nozz1e with and without swirl plate. The factors of sprayer nozzle are composed of the spraying pressure, the helical angle of swirl plate, the helical groove depth of swirl plate, the distance of vortex chamber the slope of nozz1e cap, the curvature of nozzle cap and the hole diameter of nozz1e cap. The travelling distance and the size of sprayed particle are experimeted indoors by the factorial arrange-ment according to the 5 each level of the above factors. The results of this stupy are summarized as follows; 1. In the nozzle with swirl p1ate there were remarkable significance among factors each other, while without swirl plate were no significance. 2. The helical angle and groove depth in the nozzle with swirl plate were the highest effective factors. The effect of helical angle was very remarked in the quadratic curve with minium value. 3. The correlation betweenthe travelling distance and the sprayed particle size was no high and under 250 micron in the case with swirl plate, and there was higher correlation in the case without swirl plate. 4. The new ideal development of the swirl plate using of the most effective helical angle and groove depth will probably show the possiblities to make effective travelling distance over 8 meters and more over and to make average particle diameter under 300 micron.

• 대한기계학회논문집B
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• 제41권2호
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• pp.97-107
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• 2017

본 논문은 반 쐐기형 연소실에서 포트형상에 따른 정상유동 특성을 비교한 연구의 두 번째로 유동 평가위치의 영향을 고찰한 것이다. 입자영상유속계로 반 쐐기형 연소실에 직선형 포트와 나선형 포트를 적용하여 측정위치를 헤드 밑면부터 하류로 보어의 1,75배 위치 즉 1.75B부터 6배 위치 즉, 6.00B까지 변경하면서 평면유속을 측정하였다. 속도분포 분석 결과 반 쐐기형 연소실을 채택하면 지붕형과 달리 동일 리프트에서 거시적 유속분포와 유선은 스월 거동 중심은 측정위치가 관계없이 거의 일정하다. 직선형 포트에서는 모든 측정위치에서 편심도는 충격식 스월 측정기에서 측정값 왜곡이 발생하는 범위에 들어오고, 나선형 포트에서도 리프트 4mm 이하에서는 모든 측정위치에서 편심의 영향을 무시할 수 없지만, 측정위치가 3.00B 이상이 되면 리프트 5mm 이상에서 편심도가 급격히 감소한다. ISM가정과의 속도분포 차이에 의해 직선형 포트의 리프트 4mm 이하 스월 중심 평가를 제외하고 모든 PIV 평가방법에서 ISM 평가 대비 상대적인 상쇄효과가 있다. 마지막으로 중심 설정과 축 방향 속도분포 가정은 스월 평가에 정성적 영향을 주지 않고, 구체적인 접선속도 분포형태에 따라 절댓값에만 영향을 준다.