• Journal of the Korea Academia-Industrial cooperation Society
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• v.16 no.3
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• pp.1677-1683
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• 2015

To cope with exhaust gas regulation, Diesel engine applied to electronic control system. As it accurately regulated the injected fuel mass and the fuel efficiency and the output are increased but the noise and the vibration are decreased. In order to keep the performance of Electronic Diesel Control System, it is important to accurately control the fuel pressure. However, when the regulator of fuel pressure is not controlled properly, the failure phenomenons(starting failure, staring delay, accelerated failure, engine mismatch et al.) occur because the fuel pressure is not stabilize. In this study, effects on a fuel pressure, engine rotating speed according to the control rate of fuel-pressure regulator are investigated in order to analyzed the performance variation with failure of fuel-pressure regulator. As a result, when the control rate of a fuel-pressure regulator is 4%~6% lower than that of standard condition, the variation of engine's rpm and return fuel flow is increased, and the abnormal condition was occurred. Besides, it is possible to diagnose the failures on fuel-pressure regulator under these conditions.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05b
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• pp.921-926
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• 1998

CANFLEX 연료봉 다발의 3000 시간 내구성 시험 기간 동안 속도센서를 사용하여 압력관 내부에 장전된 연료봉 다발의 진동을 측정하였다. 압력관 내부에 장전된 연료봉의 진동측정은 고온, 고압, 그리고 공간적 제약 때문에 가속도계나 스트레인 게이지 같은 접촉센서로는 측정할 수 없다. 비접촉 센서를 사용하면 이러한 난점을 해결하고 압력관 내부에 장전된 연료봉 다발의 진동을 측정할 수 있다. 속도센서는 비접촉 센서로서 가우스(gauss)의 크기를 감지하여 전압을 출력하는 센서이지만, 측정거리, 주파수, 그리고 속도와 가우스가 비선형이기 때문에 교정을 한 후에 사용하여야 한다. 본 본문에는 속도센서의 교정방법과 압력관 내부에 고온, 고압의 유체가 흐를 때 발생하는 연료봉 다발의 진동특성을 구하였다.

• Journal of Energy Engineering
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• v.4 no.3
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• pp.354-363
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• 1995

차세대 연료전지인 용융탄산염 연료전지의 운전조건을 확립하기 위하여 운전변수와 단위전지 성능과의 관계를 살표보았다. 용융탄산염 연료전지에 산화제로 공기를 사용하는 경우 양극가스에 질소가 포함된다. 그리고 연료전지의 작동압력을 높이면 출력을 크게 할 수 있다. 그리하여 본 연구에서는 에너지 및 물질수지를 이용하여 양극가스내 질소 조성과 작동압력 변화에 따른 전지내의 온도분포 및 성능변화를 구하였다. 본 연구팀이 이미 발표한 용융탄산염 단위 연료전지의 전류밀도의 온도분포를 구하기 위한 수치모사가 이용되었다. 가스흐름의 형태는 십자류를 선택하였다. 양극가스내 질소의 영향은 냉각효과로 나타났다. 작동압력이 증가할수록 전지의 성능은 증가하였고, 기전력[mV]변화 대 압력[atm]의 상용대수값의 변화(즉, ΔV 대 Δ(log))의 1차함수 그래프 기울기는 79.9로 문헌상의 실험치와 유사하게 나타났다.

• Journal of the korean Society of Automotive Engineers
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• v.11 no.2
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• pp.34-40
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• 1989

본 연구에서는 유화연료 액적의 연소시에 나타나는 일반적인 연소특성과 이에 미치는 압력의 영향에 대하여 실험적인 방법으로 연구를 수행하였다. 고압용기내에서 유화연료의 단일 액적을 연소시키면서 그 연소과정을 고속으로 촬영하여 분석하는 한편, 연소과정중의 액적 내부의 온도변화를 측정하였다. 고압 용기내의 압력은 대기압으로부터 10atm까지, 연료에 대한 물의 혼합비는 체적비로 0-20%까지 변화시키면서, 유화연료 액적의 연소특성에 미치는 물의 함량과 압력변화의 영향을 분석하였다.

• Journal of Advanced Marine Engineering and Technology
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• v.40 no.4
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• pp.295-300
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• 2016

This paper presents a numerical analysis of the delivery pressure wave in a 210-kW/cyl fuel injection pump (P. Corporation, Changwon-si, Korea) for medium-speed diesel engines using Ansys Fluent R15.0. Results obtained from experiment and from numerical analysis of the fuel delivery pressure wave were compared and found to be similar, thereby confirming the reliability of the numerical analysis of the delivery pressure wave in the fuel injection pump.

• Journal of Advanced Marine Engineering and Technology
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• v.39 no.9
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• pp.911-917
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• 2015

The objective of this work focuses on the analysis of injection rate and macroscopic spray behavior characteristics with injection pressures as well as combustion and exhaust emission characteristics with injection timing and injection pressure by using a common rail single-cylinder diesel engine. The injection rate was measured by applying the Bosch method, and macroscopic spray behavior characteristics were analyzed with a constant-volume vessel and a high-speed camera. In addition, combustion and emission characteristics were analyzed in a common-rail single-cylinder diesel engine with precise control of fuel injection timing and pressure. For injection pressures of 30MPa and 50MPa, the injection rate was higher at 50 MPa, and the spray development (penetration) was also higher in the same elapsed time. The peak in-cylinder pressure and rate of heat release showed a tendency to decline as injection timing was delayed, and the peak in-cylinder pressure and rate of heat release were slightly higher for higher injection pressures. Higher injection pressures also reduced the mean effective pressure, while the indicated mean effective pressure and torque increased as injection timing was delayed to TDC. Nitrogen oxides had a peak level at injection timings of $BTDC20^{\circ}$(30MPa) and $BTDC15^{\circ}$(50MPa); carbon monoxide emissions were reduced by delaying injection timing from $BTDC30^{\circ}$.

• Journal of the Korean Society of Propulsion Engineers
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• v.4 no.2
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• pp.39-45
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• 2000

A Thruster valve operates to supply fuel into thruster chamber. Very quick on-off operation of thruster valve results in unsteady flow of fuel in the propellant supplying system. Then fuel kinetic force, elastic material of propellant line, compressibility of fuel cause the flow field to pulsate. The pressure oscillation arising from resonance would damage the weak part of the thruster valve and other propellant supplying equipment. Pressure drop and fuel flowrate through propellant suppling system were measured, and pressure oscillation were triggered at the thruster valve inlet.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.469-473
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• 2010

In this study, combustion tests using liquefying fuels with fast regression rate were performed. The chamber pressure oscillation was analyzed and hazards of combustion instabilities were examined. In case of Liquefying fuel with fast regression rate, the amplitude of chamber pressure oscillation was increased compared to the polymeric fuels. However, the critical combustion instability can hardly occur in liquefying fuel. This is because the rapid change of inner chamber diameter limits the amplification of chamber pressure oscillation. The chamber pressure oscillation due to the large increase of fuel production and the vortex shedding in pre-chamber violently occurs during combustion using single-port axial injector.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.145-148
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• 2009

Combustion tests of a fuel-rich gas generator had been conducted using the assembly of a powerpack. A gas generator is prone to longitudinal modes of combustion instabilities in a powerpack due to the increase of a characteristic length. It has been observed that the orifice inserted at the exit of the gas generator suppresses a longitudinal combustion instability. The intensities of pressure fluctuations in the manifolds and the chamber increase quadratically with a chamber pressure. Pressure fluctuations in the fuel manifold reveal two-fold strength greater than those in the oxygen manifold and the chamber. Frequency analysis indicates nonlinear characteristics inherent in the pressure fluctuations in the fuel manifold.

• Proceedings of the KAIS Fall Conference
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• 2010.05b
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• pp.988-991
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• 2010

본 연구는 직접 연료분사 가솔린 엔진에 장착되는 고압연료 인젝터의 연료공급 특성에 대한 것으로, 두 종류 GDI 인젝터의 분무가시화 실험을 수행하였고, 분무특성을 분석하였다. 가시화 실험을 통하여 인젝터 끝단 분사 초단부근 연료거동을 확인하였고, 인젝터의 특성인 도달거리와 관통력을 확인하였으며, 분위기 압력의 변화에 따른 분무특성을 고려하여 실험을 수행하였다. 두 인젝터 모두 분위기 압력이 증가함에 따라 도달거리와 분사각이 감소하였다. B type의 인젝터 보다 A type의 인젝터가 분위기 압력에 민감한 것으로 나타났다. 본 연구를 통하여 분위기 압력의 변화에 따른 분무거동의 변화를 확인 하였으며 직접 분사인젝터의 엔진적용을 위한 기초 분무 데이터를 확보하였다.