• 한국자동차공학회논문집
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• 제11권1호
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• pp.32-41
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• 2003

For the countermeasure of expected higher thermal load in miller cycle engine, coolant flows in the cylinder head of base engine with several coolant flow methods and drilled hole passages were measured by using PIV technique. And the cooling effect was evaluated by measurements of wall temperatures according to each coolant flow method. It was found that the series flow system was most suitable among the discussed 3 types of coolant flow methods since it had the best cooling effect in cylinder head by the fastest coolant flow velocity It was also found that for drilled water passage to decrease the large thermal load in exhaust valve bridge, nozzle type is more effective compared with round type of water passage, and its size has to be determined according to the coolant flow pattern and velocity in each cylinder.

• 한국자동차공학회논문집
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• 제10권6호
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• pp.1-10
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• 2002

As the preliminary stage for the countermeasure of thermal loading in miller cycle engine, coolant flows in the cylinder head of base engine including exhaust valve bridge were visualized and analyzed by using PIV technique. It was found that low coolant velocity regions were around exhaust valve bridge, around which stagnation of the coolant flow was observed due to the complex geometry configuration of water jacket. And velocity variation between each cylinder was remarkable. For the countermeasure of these, it is necessary to enhance coolant flow around exhaust valve bridge and to improve the deviation of coolant flow between each cylinder.

• Journal of Advanced Marine Engineering and Technology
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• 제36권4호
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• pp.423-429
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• 2012

밀러 사이클은 저배기 및 고효율 달성으로 Tier II 규제뿐만 아니라 $CO_2$ 저감을 동시에 달성할 수 있는 기술로 알려져 있다. 그러나 이를 위해서는 충분한 흡입공기량이 확보되어야 하며 흡기계통은 공기저항을 최소화할 수 있는 형상으로 개선되어야 한다. 본 연구에서 흡기계통 설계 및 사이클 해석에 활용하기 위한 기초 자료 확보를 위해 흡기밸브의 유량계수를 측정하였다. 유량계수 측정에는 정상유동장치를 이용하였다. 중속 박용기관에 사용되는 포핏 밸브를 대상으로 실험을 수행한 결과, 흡기밸브 유량계수는 밸브양정의 증가에 따라 약 0.62까지 지속적으로 증가하는 경향이며 행정/보어 비와는 무관한 흡기밸브 고유의 특성이 있음을 확인하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제39권6호
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• pp.626-632
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• 2015

국제해사기구(IMO)에서는 선박으로부터의 대기오염방지를 위한 규제와 여기에 더하여 지구온난화의 방지를 위한 규제가 이미 시행되고 있거나 또는 논의 중에 있다. 따라서 고효율 친환경에 대한 요구들을 동시에 만족시킬 수 있는 대책이 요구된다. 디젤엔진에 있어서 밀러 사이클의 채택이 NOx 저감과 열효율향상을 동시에 꾀할 수 있는 방법으로 많은 관심을 받고 있다. 그러나 이 방법은 높은 급기압력이 요구되며 그 대책의 하나로 2단과급에 의한 방법이 주목을 받고 있다. 2단 과급시스템을 이용하면 고과급의 효과는 물론 여기에 바이패스기술과 밀러사이클을 이용하면 특정 부하영역에서의 성능향상 등 더욱 다양한 성능개선을 이룩할 수 있다. 그러나 2단 과급시스템의 디젤기관은 그만큼 구조가 복잡하게 되어 과급기 최적 매칭 등 시스템의 최적설계가 매우 복잡하고 어렵게 된다. 따라서 설계초기단계에서 이러한 다양한 방법들의 개선효과를 정량적으로 확인하고 또한 최적조건을 검토할 필요가 있다. 본 연구에서는 과급 시스템의 최적 설계를 위한 시뮬레이션 프로그램을 개발하였으며, 개발 된 프로그램의 신뢰성을 확인하고 이 프로그램의 활용방법에 관하여 고찰한 결과를 보고한다.

• Journal of Advanced Marine Engineering and Technology
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• 제36권2호
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• pp.230-237
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• 2012

최근 엔진 메이커들은 원유가 인상 및 대기환경 규제에 대응하기 위하여 디젤엔진의 대안으로서 가스엔진 개발에 대한 관심이 증가되고 있다. 이에 STX는 22HLX 디젤엔진을 기초로 한 1.6MW급 가스엔진을 개발하였다. 예연소실 방식의 개발된 가스엔진은 엔진속도가 1000rpm에서 제동평균유효압력이 21bar이고 질소산화물 배출량이 50ppm(공기 중 산소함유 15% 기준)의 우수한 성능을 가진다. 특히 열효율 45%의 우수한 연료 경제성을 가지며 이산화탄소 배출량은 디젤엔진의 약 75%수준으로 온실가스 저감에도 효과적이다.

• Fashion, Industry and Education
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• 제14권2호
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• pp.47-59
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• 2016

This research is concerned with comparing fluctuation in the Korean and the US economies in order to ascertain the degree to which the former is influenced by changes in the latter. The aim of this research is to explore business cycles, to examine consumer expenditure in Korea and the US, and to discover the relationships between business fluctuation indexes and overall expenditure. Statistical data from the national statistics of Korea and the US during period from 1990 to 2015 were used. The instrument included a measure of GDP, unemployment rates, GDP deflator rate (inflation rates), and household income and expenditure. For the average annual household expenditures, food, apparel and transportation expenditure data were compared across the two countries. Data were collected separately from different (though comparable) sources and were analyzed using relatively straight forward statistical techniques. It was found that Korean and the US consumers' income and expenditure were greatly affected by economic fluctuations. Total expenditure and the expenditures for food and transportation were much influenced by business fluctuation in the US, whereas, the expenditures for apparel were much influenced by business fluctuation in Korea.

• 대한원격탐사학회지
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• 제1권1호
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• pp.63-87
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• 1985

Considerable experience has been reported on the use of spectral data to measure the canopy biomass of dryland grain crops and the use of these estimates to forecast subsequent grain yield. These basic procedures were retested to assess the use of the general process to forecasting grain yield for paddy rice. The use of the ratio of a multiband radiometer simulation of Thematic Mapper band 4(.76 to .90 .mu.m) divided by band 3 (.63 to .69 .mu.m) was tested to estimate the canopy biomass of paddy rice as a function of the stage of development of the rice. The correlation was found to be greatest (R = .94) at panicle differentiation about midway through the development cycle of the rice canopy. The use of this ratio of two spectral bands as a surrogate for canopy biomass was then tested for its correlation against final grain yield. These spectral estimates of canopy biomass produced the highest correlations with final grain yield (R = .87) when measured at the canopy development stages of panicle differentiation and heading. The impact of varying the amounts of supplemental nitrogen on the use of spectral measuremants of canopy biomass to estimate grain yield was also determined. The effect of the development of a significant amount of weed biomass in the rice canopy was also clearly detected.

• 한국응용과학기술학회지
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• 제36권4호
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• pp.1427-1433
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• 2019

본 연구에서는 합성가스의 에너지화를 위한 가스엔진 성능 평가를 수행하였다. 회전수 1800 rpm 조건에서 공기과잉률이 1, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6 증가에 따른 엔진출력(kW_m)과 열효율(%)을 평가한 결과, 공기과잉률 λ 1.4에서 엔진출력 34 kW_m를 나타냈으며, 공기과잉률이 증가할수록 엔진 열효율은 전반적으로 감소하는 경향을 보였다. 엔진출력 34 kW_m 조건에서 공기과잉률이 1, 1.1, 1.2, 1.3, 1.4 증가시 열효율이 34.2%, 36.9%, 37.2%, 37.4%, 38.1%로 증가하였고, 발전출력을 통한 종합효율은 발전출력 30 kWe 부하조건에서 38.7 kg/h의 연료를 소모하여 32.1%의 발전효율과 냉각수와 배기가스에서의 열회수를 통해 57.3 kW의 폐열을 회수하여 53.8%의 열을 회수하여 총 85.8%의 종합효율을 보이는 것으로 나타났다.

• 한국해양공학회지
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• 제3권2호
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• pp.125-137
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• 1989

To check technical improvement in the soundness and strength of 12% Cr steel rotor, a 25 tons of rotor with 65 tons of ingot was made in real size and was cut to pieces to take test samples, and the various mechanical tests such as impact, tensile, creep, and fatigue were carried out. The strengths are compared with those of 1% Cr-Mo-V rotor of same size. Microstructures of the samples are examined and reviewed. The results can be summarized as follows. 1) Fracture appearance transition temperatures are 80.deg. C at the center part and 60.deg. C near surface of 12% Cr rotor, and 8.deg. C near surface of 1% Cr-Mo-V rotor. 2) Comparative rapid softening occurs at higher temperatures above 600.deg. C for 12% Cr steel and 550.deg. C for 1% Cr-Mo-V steel in tension tests. 3) Fatigue crack propagation rate of 12% Cr steel is almost same as that of 1% Cr-Mo-V steel at the same corresponding surface part of the rotors. The crack growth rate of center part of 12% Cr rotor is faster than near surface part of the rotor, and the crack growth rate at the load condition of R=0.04 is slower than that of the load condition of R=0.5 for both 12% Cr steel and 1% Cr-Mo-V steel. 4) Crack growth rate of radial direction near surface of 12% Cr rotor is faster than that of transverse direction at the same part because of the difference in residual stresses. 5) Both creep and fatigue strengths of 12% Cr steel are superior to those of 1% Cr-Mo-V steel and the difference is thought the effect of climb and glide controlled creep by solid solution of alloying elements and dispersion of carbides.

• 한국해양공학회지
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• 제3권2호
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• pp.625-625
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• 1989

To check technical improvement in the soundness and strength of 12% Cr steel rotor, a 25 tons of rotor with 65 tons of ingot was made in real size and was cut to pieces to take test samples, and the various mechanical tests such as impact, tensile, creep, and fatigue were carried out. The strengths are compared with those of 1% Cr-Mo-V rotor of same size. Microstructures of the samples are examined and reviewed. The results can be summarized as follows. 1) Fracture appearance transition temperatures are 80.deg. C at the center part and 60.deg. C near surface of 12% Cr rotor, and 8.deg. C near surface of 1% Cr-Mo-V rotor. 2) Comparative rapid softening occurs at higher temperatures above 600.deg. C for 12% Cr steel and 550.deg. C for 1% Cr-Mo-V steel in tension tests. 3) Fatigue crack propagation rate of 12% Cr steel is almost same as that of 1% Cr-Mo-V steel at the same corresponding surface part of the rotors. The crack growth rate of center part of 12% Cr rotor is faster than near surface part of the rotor, and the crack growth rate at the load condition of R=0.04 is slower than that of the load condition of R=0.5 for both 12% Cr steel and 1% Cr-Mo-V steel. 4) Crack growth rate of radial direction near surface of 12% Cr rotor is faster than that of transverse direction at the same part because of the difference in residual stresses. 5) Both creep and fatigue strengths of 12% Cr steel are superior to those of 1% Cr-Mo-V steel and the difference is thought the effect of climb and glide controlled creep by solid solution of alloying elements and dispersion of carbides.