• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.309-315
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• 2006

Effects of injector or design on combustion characteristics of full-scale gas generators were studied. Three full-scale gas generators, which have same total mass flow rate but mass flow rate per injector is different depending on their designs, were manufactured. Thirteen, nineteen and thirty seven injectors, which have internal-mixing and double-swirl characteristics, are distributed in injector heads, respectively. The results showed that special pressure fluctuations in the gas generators with 13 and 19 injectors didn't appear around longitudinal resonant frequency, but small longitudinal-mode instability appeared in the gas generator with 37 injectors. As the number of injectors installed in injector heads increased, temperature distribution in combustion chambers showed small deviations, but the damage of LOx posts increased.

• Journal of the Korean Institute of Gas
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• v.20 no.2
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• pp.58-65
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• 2016

Hydraulic analysis of the natural gas transmission pipeline is to determine whether adequate flow can be sustained throughout the design life of pipeline under all expected flow conditions. Many factors have to be considered in the hydraulic design of long-distance pipelines, including the nature, volume, temperature and pressure of fluid to be transported, the length and elevation of pipeline and the environment of terrain traversed. This study reviewed the available gas operation data provided by pipeline construction project in the arctic area and discussed the gas properties such as viscosity and compressibility factor that influence gas flow through a pipeline. Pipeline inside diameter was calculated using several flow equations and pipeline wall thickness was calculated from Barlow's equation applying a safety factor and including the yield strength of the pipe material. The AGA flow equation was used to calculate the pressure drop due to friction, gas temperature and pipeline elevation along the pipeline. The hydraulic design in this study was compared with the report of Alaska Pipeline Project.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.05a
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• pp.258-261
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• 2003

The optimal design and combustion analysis of the gas generator for Liquid Rocket Engine (LRE) were performed. A fuel-rich gas generator in open cycle turbopump system was designed for 101on1 in thrust with RP-1/LOx combination. The optimal design was done for maximizing specific impulse of main combustion chamber with constraints of combustion temperature and power matching in turbopump system. Results of optimal design show the dimension of length, diameter, and contraction ratio of gas generator. The configuration of the gas generator and the condition for performance which can maximize the objective function were determined and found to meet the design constraints. Also, the combustion analysis was conducted to evaluate the performance of designed chamber and injector of gas generator. And the effect of the turbulence ring was investigated on the mixing enhancement in the chamber.

• Journal of the Korean Ceramic Society
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• v.38 no.12
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• pp.1180-1186
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• 2001

W $O_3$-Sn $O_2$thin film sensors with approximately 1${\mu}{\textrm}{m}$ in thickness were fabricated by using a high-vacuum resistance-heating evaporator, were annealed at 50$0^{\circ}C$ for 4 hours in air, and then their crystallinities and surface microstructures were analyzed. As results of gas-sensing characteristics to oxidizing gas, N $O_2$, and reducing gas, CO, of 100 ppm, the highest gas sensitivities (S= $R_{gas}$/ $R_{air}$) were the W $O_3$thin-film sensor measured at 25$0^{\circ}C$ for N $O_2$(S≒1000) and the Sn $O_2$thin-film sensor measured at 15$0^{\circ}C$ to 25$0^{\circ}C$ range for CO (S≒0.25), respectively.ely.

• Clean Technology
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• v.18 no.4
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• pp.360-365
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• 2012

With rapid increase in municipal solid waste (MSW) due to the rising economy, solid waste gasification emerges as one of the promising technologies. Separation of the carbon monoxide (CO) and hydrogen ($H_2$) from syngas obtained by gasification of MSW was studied using the polyamide composite membrane. The separation characteristics of the CO and $H_2$ were studied at different gas flow rates and stage cuts. The permeability of CO and $H_2$ along with the selectivity of $H_2$ with respect to CO was obtained. Furthermore, the Arrhenius plots were obtained to estimate the activation energies of CO and $H_2$ permeabilites.

• Clean Technology
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• v.19 no.3
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• pp.226-232
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• 2013

A 5 kg/hr scale integral dual fluidized-bed gasifier for producing medium heating value syngas from biomass or combustible wastes was manufactured. The effect of operating variables including gasification temperature, rate of feeding, and weight ratio of steam/feed on the behavior of the gasifier was investigated. The contents of $H_2$ and CO in syngas, flow rate of feeding, cold gas efficiency increased with the increased gasification temperature or rate of feeding, but decreased with the increased weight ratio of steam/feed within the experimental range. With wood powder as the feed, the concentrations of $H_2$ and CO in the syngas were as high as 41% and 32%, and the cold gas efficiency and lower heating value of the syngas were as high as 70.1% and $3,428kcal/Nm^3$. With food wastes as the feed, the concentrations of $H_2$ and CO in the syngas were as high as 37% and 23.9%, and the cold gas efficiency and lower heating value of the syngas were as high as 66.7% and $3,670kcal/Nm^3$.

• Journal of the Korean Institute of Gas
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• v.22 no.1
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• pp.1-8
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• 2018

FCV is installed with a automatic valve attached in an high pressure cylinder to control the hydrogen flow. The supply of hydrogen from the cylinder into the fuel cell stack is controlled via the on/off operation of a solenoid attached to the automatic valve. The solenoid needs to provide the necessary attraction force even at any saturation temperature caused by drive of the vehicle. In this study, the simplified prediction equations for the saturation temperature are suggested. The finite element analysis was performed by steady state technique, according to the boundary condition in order to predict the saturation temperature and attraction force. Finally, the saturation temperature was validated through comparison between the analysis results and measurement results. From the results, the measured saturation temperature $5.9^{\circ}C$ lower with respect to the analysis results. And the error of attraction force ranged from 1.0 to 2.1 N at testing conditions.

• Journal of the Korean Society of Propulsion Engineers
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• v.18 no.1
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• pp.26-32
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• 2014

In this study, DC (Direct current) type steam plasma igniter is developed for effective ignition of high-energy density metal aluminum and gas temperature is measured by emission spectrum of OH radical. Because of the ultra-high gas temperature, the DC plasma jet is measured by Boltzmann plot method which is the non-contact optical technique and spectrum comparison-analysis. And both methods were applied to experiment after accurate verification. As a result, we could identify that plasma jet temperature is 2900 K ~ 5800 K in the 30 mm range from the nozzle tip.

• Journal of Power System Engineering
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• v.11 no.2
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• pp.12-19
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• 2007

현재, 육지에서 필요한 천연 가스 (NG)의 얻기 위한 방법으로 공기 가열식 기화기의 사용이 증가하고 있다. 특히, 파이프라인에 의해 도달될 수 없는 거리가 멀리 떨어진 소외된 지역까지 보낼 수 있기 때문에 소형 위성기지의 역할은 대단히 중요하다고 할 수 있다. 소형 위성기지의 LNG는 인수기지에서 탱크로리를 이용하여 배달되고 그 후에 위성기지에서 기화과정을 통하여 각 수요처로 보내어진다. 공기 가열식 기화기는 LNG 인수기지 외의 소형 위성기지 단위에서 최근 많이 개발되고 사용되고 있는 기화기의 종류 중 하나라고 할 수 있다1). 효율적인 공기 가열식 기화기를 개발하기 위하여, 핀이 없는 경우와 핀이 8개이고 핀의 길이가 55 mm인 공기 가열식 기화기를 사용하여 실험을 진행하였고 그리고 나서 두 가지 유형의 기화기를 비교하였다. 실험조건은 기화기의 길이 변화와 여러 가지 주위 조건(온도, 습도, 풍속)을 변화하였다. 실험에 적용된 주위 온도는 각 계절별 온도와 동일한 온도를 적용하였다. 본 실험에서 나타내고자 한 공기가열식 기화기의 주요 특성은 각 계절별 조건에 따른 입구 측과 출구 측의 온도차를 비교하는 것이다. 액화천연가스(LNG)를 가지고 실험을 하는 것은 위험성이 있어 특성이 비슷하면서 안전한 $LN_2$를 사용하여 실험을 진행하여 핀을 가지는 기화기가 핀이 없는 기화기보다는 좋다는 결과를 확인할 수 있었다.

• Journal of the Korean Society of Propulsion Engineers
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• v.3 no.4
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• pp.51-57
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• 1999

Temperature and velocity controlling of air at inlet position of Ramjet combustor is important under Ramjet engine grounding-test condition since temperature of inlet air increases due to compression process by supersonic flow at inlet position of Ramjet combustor. In this study, Vitiated Air Heater methodology was used to control temperature of air that is inducted into Ramjet combustor. Temperature and velocity of air at Vitiated air heater exit, which is inducted into Ramjet combustor, were measured to evaluate Vitiated air heater system developed in this study. It is shown that temperature and velocity of inducted air can be well controlled using Vitiated air heater system developed in this study, and we could make a Vitiated Air which is almost same with real air.