• 대한기계학회논문집B
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• 제20권6호
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• pp.1941-1947
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• 1996

Droplet size measurement technique was established for the sprayed viscous fluid by virtue of the installation of the sprayed-droplet size measurement system employing light scattering method. Atomization test results showed that the mean droplet size of the sprayed viscous fluid is decreased with the increase of the mass ratio of air to fuel and in case of the same air/fuel ratio, also with the increase of viscous fluid flow rate, and is increased with the distance from atomizer tip. Basic design data for the manufacture of external-mixing type, Y-Jet type, and internal-mixing type atomizers was acquired from the atomization tests.

• 한국분무공학회지
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• 제9권2호
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• pp.24-33
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• 2004

The effect of the working fluid flow conditions and nozzle geometry on the spray performance of a twin-fluid nozzle used in Selective Catalytic Reduction is investigated experimentally. The liquid pressure is varied in the range of 0.3atm to 1.5atm and the air pressure is varied from the 0.5atm to 3.0atm. relative position between liquid nozzle(internal nozzle) and air nozzle(external nozzle) tip changes front 1mm inside the air nozzle to 1mm outside the air nozzle. The orifice diameter of the air nozzle is varied with 5mm. 6mm and 7mm. Spray visualization is realized with CCD-Camera. SMD(Sauter Mean Diameter) and mean particle velocities are measured by PDPA(Phase Doppler Particle Analyzer) under various experimental conditions. The measuring point is 300mm away from the nozzle tip in the downstream spray. The experimental results are that spray angle is depended air flow rate because nozzle diameter, air pressure and nozzle tip relative positions are related air flow rate. SMD is depended air flow rate and water flow rate. Also, SMD is increased when water flow rate is bigger. SMD is decreased when Air flow rate is bigger.

• 연구논문집
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• 통권25호
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• pp.47-54
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• 1995

The atomizing characteristics in a spray injected from a twin fluid atomization nozzle have been investigated. The Sauter mean diameters as mean diameter are compared with wavelength calculated from the instability theory. The Sauter mean diameter are measured by the Fraunhofer diffraction theory using the Malvern particle sizer. The wavelength is calculated using the mean relative velocity instead of the exit relative velocity of nozzle. Also shadowgraphy technique is used to visualize atomization. This paper gives a possibility that the mean diameter can be predicted with the wavelength obtained by the simple instability theory.

• 한국화재소방학회논문지
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• 제33권3호
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• pp.37-43
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• 2019

본 연구에서는 2유체노즐을 이용하여 에탄올 풀화재(Ethanol pool fire) 소화 실험을 수행하였다. 화원 면적이 5.027 × 10^-3 ㎡와 1.131 × 10^-2 ㎡(연료팬 직경은 각각 80 mm와 120 mm)를 대상으로 하였고, 화재 소화 실험 시 2유체노즐로의 공급 유량의 경우 물은 156-483 g/min, 공기는 20-70 L/min 조건이었다. 화원 면적이 증가하면 열방출률도 증가하였고, 화원 면적이 5.027 × 10^-3 ㎡와 1.131 × 10^-2 ㎡일 때의 열방출률은 각각 1.01 kW와 5.51 kW로 측정되었다. 본 실험 영역에서 2가지 화원 면적 조건 모두, 물 공급 유량 조건과는 상관없이 공기 공급 유량이 40 L/min 이상의 조건에서 소화가 가능하였다. 소화 소요 시간 및 물 소모량의 경우 모든 물 공급 유량 조건에서 공기 공급 유량이 증가함에 따라 감소하는 경향이 관찰되었고, 공기 공급 유량이 비교적 많은 영역(예를 들면, 약 50 L/min 이상)에서 소화 소요 시간은 약 23 s, 물 소모량은 약 185 g 이내로 나타났다. 본 연구 결과와 단일유체노즐을 이용한 기존 연구 간 단위 열방출률 당 물 소모량 비교를 통하여, 2유체노즐이 단일유체노즐에 비해 더 적은 물 소모량으로 소화가 가능할 수 있음을 확인하였다.

• 한국화재소방학회논문지
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• 제32권3호
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• pp.35-41
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• 2018

본 연구에서는 2유체노즐을 이용하여 140 ml 헥산 풀화재(Pool fire)에 대한 소화 실험을 수행하였다. 해당 풀화재의 화원(직경 80 mm인 원형) 면적은 $0.005027m^2$이고, 열방출률은 2.81 kW로 측정되었다. 물 공급 유량은 156-483 g/min (~0.156-0.483 l/min), 기체(공기와 질소) 공급 유량은 30-70 l/min이었다. 본 실험조건에서 기체 공급 유량이 많은 경우에 성공적으로 소화가 가능하였다. 소화 가능 영역에서 기체 공급 유량이 적은 경우, 물 공급 유량이 많을 때 화재 소화 소요 시간이 길었고, 물 소모량은 많은 것으로 나타났다. 반면, 기체 공급 유량이 많은 경우, 물 공급유량에 따른 화재 소화 소요 시간 및 물 소모량은 상대적으로 큰 차이가 없는 것으로 나타났다. 한편, 본 실험조건에서 공급 기체의 종류는 소화 가능 여부, 소화 소요 시간, 물 소모량에 큰 영향을 미치지 않는 것으로 측정되었다. 마지막으로 본 실험결과와 단일유체노즐을 이용한 기존 실험결과를 이용하여, 2유체노즐과 단일유체노즐의 140 ml 헥산 풀화재 소화를 위한 물 소모량을 선행적으로 비교 및 검토하였다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제6권2호
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• pp.392-405
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• 2014

SSPA experiences a growing interest in twin skeg ships as one attractive green ship solution. The twin skeg concept is well proven with obvious advantages for the design of ships with full hull forms, restricted draft or highly loaded propellers. SSPA has conducted extensive hull optimizations studies of LNG ships of different size based on an extensive hull data base with over 7,000 models tested, including over 400 twin skeg hull forms. Main hull dimensions and different hull concepts such as twin skeg and single screw were of main interest in the studies. In the present paper, one twin skeg and one single screw 170 K LNG ship were designed for optimally selected main dimension parameters. The twin skeg hull was further optimized and evaluated using SHIPFLOW FRIENDSHIP design package by performing parameter variation in order to modify the shape and positions of the skegs. The finally optimized models were then built and tested in order to confirm the lower power demand of twin skeg designed compaed with the signle screw design. This paper is a full description of one of the design developments of a LNG twin skeg hull, from early dimensional parameter study, through design optimization phase towards the confirmation by model tests.

• Journal of Biosystems Engineering
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• 제25권1호
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• pp.11-18
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• 2000

In precision chemical application increment of biological efficacy with less chemical is the virtue. spraying rate and droplet size is closely related to biological efficacy. this study was performed to develope a spray-control-system that could control spraying rate and droplet size independently. Twin-fluid nozzles were selected and tested to certify if the nozzles were suitable for the objective of this study. Characteritics of the nozzles i.e., spraying rte and droplet size change u8nder the changes of spraying pressure and air pressure were statistically modeled. The model had I to 1 matching property between dependent variables and independent variables. Using the property and the model, inverse relationship could be determined between variables. A feedback spray control system was developed and tested with predetermined error of 5 % in pressure. The system showed 4 % error in spraying rate and 9 % error in droplets size. Performance of the system could be upgraded by fine tuning but, in practical sense keeping air pressure in the field sprayer was the bottle neck of commercialization of the spray system.

• 대한기계학회논문집
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• 제15권6호
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• pp.2147-2159
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• 1991

본 연구에서는 가장 다순한 내부혼합형 이류체분사노즐의 기류속도, 액체유량, 노즐직경 및 혼합길이, 기액접촉각을 변화시켜 평균입경(SMD), 분무각, 입도분포, 분 무분사량분포 등을 조사하여 노즐형상에 따른 분무특성의 변화를 자세히 밝혀, 분무특 성을 조절할 수 있는 이류체분사 노즐의 설계에 대한 기초적 자료를 제시하고자 한다.

• 한국분무공학회지
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• 제22권3호
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• pp.146-152
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• 2017

An experimental study was carried out to investigate the spray characteristics of non-circular effervescent twin-fluid nozzles. For this purpose, two types of non-circular nozzles (E1, E2) and circular nozzle (C) were used. Three types of aerorators with hole diameters of 1.2, 1.7 and 2.1 mm were used. Each aerorator has a total of 12 holes. It is defined by area ratio which is ratio of exit orifice area and aerator hole area. Experiments were carried out by controlling the amount of air flowing after fixing the flow rate of the liquid, and the nozzle internal pressure and SMD were measured, and the jet image was taken from the nozzles. The discharge coefficients of the three kinds of nozzles were compared with the used in plain orifice's equation and the Jedelsky's equation, and the Jedelsky's equation was found to be about 3 times larger. In addition, empirical formula based on ALR, which is the largest variable in Jedelsky's equation, was derived. The droplet sizes(SMD) were found to be smaller in the non-circular shape than in the circular shape, which is concluded to be caused by the difference of the discharge coefficients.

• 대한기계학회논문집B
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• 제21권8호
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• pp.1056-1067
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• 1997

Present study visualized flow pattern and investigated spray characteristics of twin-fluid atomization with converging-diverging nozzles. Particle sizes were measured by using the Malvern particle analyzer, and the radial size distributions were evaluated by using the tomographic transform technique. The results show that the SMD generally increases in the radial direction at a prescribed liquid flow rate and the increasing rate in the SMD becomes gradual as atomizing gas pressure increases. The SMD decreases as the liquid flow rate increases at a fixed GLR (gas/liquid mass ratio). The atomization performance of the protrusion-type nozzle turned out to be superior to that of the flush-type. However, in the case of the protrusion-type, flow separation occurs outside the liquid delivery tube when the pressure at the gas nozzle chamber is high enough, which may deteriorate the atomization performance.