• Journal of ILASS-Korea
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• v.20 no.2
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• pp.70-75
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• 2015

Swirl flow in the gun type burner has an impact on the stabilization of the flame, improvement of the combustion efficiency. The swirl flow is created by the spinner which is inside the airtube that guide the combustion air. Gun type burner has generally the inner devices composed electronic spark plug, injection nozzle, combustion device adaptor, and spinner. These inner components change the air flow behavior passing through airtube. So, this study conducted the measurement using by hot-wire anemometer and analyzed effect of the swirl number of spinner on the exhaust air of gun type burner. Turbulence characteristics come up in this study was mean velocity, turbulence intensity, kinetic energy, shear stress and flattness factor of the air flow with the change of the distance of axial direction and tangential direction from the exit of the airtube.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 1999.12a
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• pp.201-210
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• 1999

• Transactions of the Korean Society of Mechanical Engineers B
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• v.27 no.11
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• pp.1579-1586
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• 2003

A gun-type burne. fur a LPG(Liquified Petroleum Gas) boiler was utilized for hydrogen combustion. The study was performed to obtain fundamental data prior to the design of a very low NO$\_$x/, hydrogen-fueled burner. First, numerical simulations were performed to predict mixing characteristics between air and fuel flows, and temperature distributions, etc. Experimental study was then performed to find out flame lengths, temperature distributions, and NO$\_$x/ concentrations. The results showed that a gun-type burner for a LPG boiler can be successfully used for hydrogen combustion without any major retrofitting. The hydrogen flame was very stable and 75 ppm of NO$\_$x/ in average was observed for the conditions considered in this study. Hydrogen combustion could be therefore a solution to avoid the problem of green-house gas(CO$_2$) if hydrogen becomes cost-effective.

• Journal of ILASS-Korea
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• v.20 no.2
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• pp.76-81
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• 2015

Swirl flow has an impact on the stabilization of the flame by the recirculation flow, improvement of the combustion efficiency. The swirl flow in the gun type burner is created by the spinner which is inside the airtube that guide the combustion air. Burner has generally the combustion device composed electronic spark plug, injection nozzle, combustion device adaptor, and spinner. These inner components change the air flow behavior passing through airtube. So, this study analyzed exhaust flow characteristics of the gun type burner according to the ratio of airtube diameter. Turbulence characteristics by the spinner was mean velocity, turbulence intensity, kinetic energy, shear stress and flattness factor of the air flow of axial direction and tangential direction from the exit of the airtube.

• Proceedings of the Korean Society for Bio-Environment Control Conference
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• 1999.04a
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• pp.9-14
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• 1999

1. LPG 온풍기는 용량 16$\times$$10^4$ ㎉ 건타입가스버너, 연소부 및 열교환부, 6개의 50kgLPG탱크와 자동절체기, 가스메타, 배관으로 구성하였다. LPG 온풍기의 이론연소효율은 91%, $CO_2$ 배출량은 11.74%, CO배출량은 0ppm, 과잉공기비는 1.16, 배기가스온도는 253$^{\circ}C$, 온풍온도는 8$0^{\circ}C$로서 우수한 성능으로 나타났다. 2. LPG온풍기에서 배출되는 배기가스중의 $CO_2$ 를 온실로 공급하기 위하여 $CO_2$ 공급기를 제작하여 배출가스연도에 부착하였다. $CO_2$ 공급기는 흡입형 시로코팬(1200㎥/h)과 차단문으로 이루어졌다. 1-2W형 300평 온실내의 $CO_2$ 농도를 1000ppm으로 올리기 위해서는 $CO_2$ 공급기를 약 1시간 정도 운전시켜야 할 것으로 판단되었다. 3. LPG온풍기와 경유온풍기의 경제성 비교분석에 의하면 현 시점의 경유 가격 242원, LP가스 가격 435원을 기준으로 연간소요비용은 각각 5,392,430원, 5,299,917원으로 경유온풍기가 10만원 정도 경제적이지만 탄산가스 시용비용, 탄산가스 공급으로 인한 작물의 수량증대 및 고품질 생산물을 고려한다면 LPG온풍기 사용이 더 경제적이라 사료된다.

• Journal of Biosystems Engineering
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• v.24 no.2
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• pp.107-114
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• 1999

To find the best combustion conditions in the heavy oil burner kinetic viscosity of heavy oil A, B and C at different temperature range, from 40 to 140$^{\circ}C$, and the droplet sizes of the heavy oils at different temperature and pump pressure were measured. And, combustion characteristics were investigated under the different conditions : two different heavy oil and three different oil temperature. At temperature of 70, 100, 130$^{\circ}C$ the kinetic viscosity of heavy oil A and B are 7.9, 5.7, 4.3 and 30.4, 13.7, 7.9cSt, respectively. The greatest and smallest viscosity were 7,455 cSt at C oil on 27$^{\circ}C$ and 4.26cSt at A oil on 140$^{\circ}C$. The magnitude of viscosity difference between at 100$^{\circ}C$ and 140$^{\circ}C$ under 6 cSt in cases of A and B oil, but more than 30cST on C oil. Of the droplet sizes, the biggest and smallest droplet size in A oil were 98$\mu\textrm{m}$ at oil temperature of 130$^{\circ}C$(4.3cSt), pump pressure of 1.57MPa and 72$\mu\textrm{m}$ at 70$^{\circ}C$(7.9cSt), 2.35MPa, respectively. It appeared that as spraying pressure increased the droplet size decreased, however, no distinct differences were found in the effects of kinetic viscosity on the droplet sizes of the test range. The best combustion performance was observed when droplet size, spraying pressure and oil temperature were 73$\mu\textrm{m}$, 2.35MPa and 70$^{\circ}C$ producing CO2 of 13.1%, CO of 13ppm and flue gas temperature of 250$^{\circ}C$ in A oil combustion For B oil, it was100$^{\circ}C$, 2.35MPa, 52$\mu\textrm{m}$, producing CO2 of 10ppm and flue gas temperature of 260$^{\circ}C$. In general, it appeared that better combustion results were observed in the smaller droplets produced burner condition.