• Journal of Energy Engineering
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• v.15 no.4 s.48
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• pp.277-283
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• 2006

In this study, butane 100% was used as fuel to verify the real fuel effect such as vapor pressure variation due to temperature change. A MPI fuel injection system for V-6 engine, which has reverse 'L' type cross section to minimize the possibility of liquid phase injection, was composed and one bank was operated under sequential injection scheme. Flow rate were measured according to injection duration, interval, and pressure. Also occurring of liquid phase injection was monitored with varying vaporizer and fuel rail temperature. The result shows that basic characteristics of injection is a relatively difference between air and LPG injection. Under cold start condition, however, the occurrence of liquid injection becomes more severe as the pressure increases, and sufficiently high temperature both in vaporizer and fuel rail is very important to insure gaseous injection. In addition, the temperature of vaporizer plays more important role in keeping LPG vapor state and the reverse 'L' type cross section of the rail is available to prevent liquid injection.

• Aerospace Engineering and Technology
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• v.13 no.1
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• pp.96-107
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• 2014

Korea Aerospace Research Institute has a plan to launch experimental lunar orbiter in 2017, and lunar orbiter and lander in 2020. In the mission planning phase, LOI(Lunar Orbit Insertion) maneuver strategy should be designed using finite burn model because on-board propulsion system of lunar orbiter in finite burn type. LOI maneuver plan and amount of required ${\Delta}V$ using finite burn model depend on the spacecraft attitude at burn, a type of propellant, thrust level and burn timing. This paper describes the LOI maneuver of lunar orbiter of foreign space agency and then comes up with the LOI maneuver plan of Korean lunar orbiter. Adequate thrust level and burn duration of Korean lunar orbiter also present by performing simulation.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.7 no.4
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• pp.798-804
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• 2003

In this paper, We have designed an advanced circuits for controlling the Ink Nozzle of Printer Head We can fully increase the number of nozzle by reducing the number of Input/Output PADs using the proposed new circuit. The proposed circuit is tested with only 20 nozzles to evaluate functional test using FPGA sample chip. The new circuit architecture can be estimated. Full circuit for controlling 320 nozzles was designed and simulated from ASIC full custom methodology, then the circuit was fabricated by applying 3${\mu}{\textrm}{m}$ CMOS process design rule.

• Transactions of the Korean Society of Automotive Engineers
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• v.15 no.2
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• pp.35-40
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• 2007

The gaseous fuel injection (GFI) type in LPG fuel supply system has more advantage than the liquified fuel injection type from the viewpoint of durability and cost reduction. But in GFI system, to control pressure and temperature of gaseous fuel is needed to get precision fuel metering for the compressible characteristic of gaseous fuel. In this study, the effects of pressure and temperature on the fuel metering was simulated by commercial flow network analysis package, Flowmaster. And the fuel composition effects on the fuel metering were also studied to figure out the fuel metering characteristics.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1994.05a
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• pp.15-21
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• 1994

단계적 연료방식을 가지는 가스터빈 연소기의 해석을 위한 방법을 제안하였으며, 이를 바탕으로 연료배분방식에 따른 연소기의 연소 및 NOx 발생특성을 규명하였다. 연소기 해석모델은 연소기 내부를 선회기구역, 1차연소구역, 재순환구역, 2차연소구역 및 희석구역으로 나누어 각각의 반응구역을 혼합반응기, 플러그 유동반응기의 모델로서 근사하였다. 반응기내의 연소 및 NOx 생성반응은 천연가스 반응모델과 Zel'dovich 의 NOx 모델을 이용하여 예측하였다. 본 해석방법을 이용하여, 각 반응구역에 유입되는 연료량이 연소기내 연소특성, NOx 발생 특성 및 온도분포에 미치는 영향을 검토하였다. 또한, NOx 저감을 위해 증기분사를 사용하는 경우에 분사위치가 NOx 발생에 미치는 영향을 분석하여, 가스터빈 연소기설계에 필요한 기초자료를 제공하였다.

• Journal of the Korean Institute of Gas
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• v.24 no.1
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• pp.49-55
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• 2020

Experimental investigations were conducted to understand the multi-staged combustion characteristics of a swirl-stabilized double cone premixed burner nozzle used for industrial gas turbines for power generation. Multi-staged combustion is implemented by injecting the fuel through the existing manifold of the side slots as well as through the apex of the cone with two fuel injection angles which are slanted or axial. NOx and CO emissions, and wall temperature distributions were measured for various fuel distributions and operating conditions. Results show that NOx emissions are decreased when the fuel distribution to the apex is 3% of the total amount of fuel, which is due to more uniform fuel distribution inside the nozzle, hence less hot spots at the flame. NOx emissions are rather increased when the fuel distribution to the apex is 8% of the total amount of fuel for axial fuel injection by occurrence of flash back in premixing zone of burner.

• Journal of the Korean Institute of Gas
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• v.24 no.4
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• pp.25-31
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• 2020

Experimental investigations were conducted to examine the combustion characteristics of a swirl-stabilized double cone premixed burner nozzle used for industrial gas turbines for power generation. Several variants with different fuel injection patterns are tested to compare the combustion characteristics such as NOx and CO emissions, stability, and wall temperature distributions. Main results show that NOx emissions and stability are decreased either when the fuel hole diameter is decreased with the same number of fuel holes, or when the number of fuel holes is reduced with the same total area of fuel holes, both of which are due to a higher penetration of fuel into the air stream. Not only is NOx reduced but also stability is enhanced when the fuel hole diameter varies in an alternating manner with the same total area of fuel holes, showing that NOx reduction is due to a higher penetration of mean fuel injection path while stability enhancement is due to a lowered penetration of minimum fuel injection path.

• Transactions of the Korean Society of Automotive Engineers
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• v.4 no.6
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• pp.144-152
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• 1996

In the sequential MPI system with one injection for each cycle, engine performance is influenced by the mixture conditions. It can be said that engine performance is improved by being better identical mixture formation conditions for all cylinders. As the fuel injection timing to the intake port effects on the mixture formation conditions and the engine performance, injection timing must be better adjusted to engine requirements. Engine behavior was clearly different depending on the injection time during intake storke. Therefore it was studied that injection timing of fuel effects on the engine performance I. e. combustion stability, COV(imep), A/F excursion, CO,HC emission concentration and fuel consumption. It was found that late intake-synchronous injection was deteriorated the combustion characteristics and performance characteristics, while early intake-synchronous infection resulted in favorable engine behavior.

• 한국신재생에너지학회:학술대회논문집
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• 2009.06a
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• pp.687-690
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• 2009

본 연구에서는 가스 하이드레이트 형성과정에서 발생할 수 있는 유도지체시간을 줄이고 전체 가스 저장량과 반응 속도의 향상을 위하여 이류체 분사 방식을 이용하여 물분자의 액적을 최소화하는 실험을 통하여, 미세액적 분사에 따른 하이드레이트 형성 시간을 확인하였으며, 반응기 내부의 온도 변화를 확인하여 반응기 내부의 하이드레이트 형성 거동을 확인하고 이를 통하여 상용화를 위한 반응기 설계의 기초 자료로 활용하고자 하였다.

• Transactions of the Korean Society of Automotive Engineers
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• v.4 no.4
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• pp.46-57
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• 1996

The direct injection stratified charge(DISC) engine enhances the fuel tolerance and the antiknock tendency. This enhanc3d antiknock tendency allows use of a higher compression ratio which results in higher thermal efficiency. But its actual utilization is prevented by high emission combustion time and wall quenching will be the main causes of increasing unburned hydrocarbons in DISC system. In order to solve this problem, small aount of hydrogen was added to the charging air or injected fuel. The effects of hydrogen addition were examined experimentally by radial fuel injection using a pancake-type constant volume bomb. In case of the hydrogen addition to the charge of air, the combustion the amount of hydrogen. In case of the hydrogen addition to the fuel, the combustion pressure was significantly increased.