• 한국자동차공학회논문집
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• 제15권3호
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• pp.54-62
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• 2007

The knock characteristics in an engine were investigated under homogeneous charge compression ignition (HCCI) operation. Liquefied petroleum gas (LPG)and gasoline were used as fuels and injected at the intake port using port fuel injection equipment. Di-methyl ether (DME) was used as an ignition promoter and was injected directly into the cylinder near compression top dead center (TDC). A commercial variable valve timing device was used to control the volumetric efficiency and the amount of internal residual gas. Different intake valve timingsand fuel injection amounts were tested to verify the knock characteristics of the HCCI engine. The ringing intensity (RI) was used to define the intensity of knock according to the operating conditions. The RI of the LPG HCCI engine was lower than that of the gasoline HCCI engine at every experimental condition. The indicated mean effective pressure (IMEP) dropped when the RI was over 0.5 MW/m2and the maximum combustion pressure was over 6.5MPa. There was no significant relationship between RI and fuel type. The RI can be predicted by the crank angle degree (CAD) at 50 CA. Carbon monoxide (CO) and hydrocarbon (HC) emissions were minimized at high RI conditions. The shortest burn duration under low RI was effective in achieving low HC and CO emissions.

• 센서학회지
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• 제8권2호
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• pp.163-170
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• 1999

각각 8개의 N과 P채널 EEPROM을 이용하여 광섬유 엔진 모니터용 압력센서를 위한 A/D 변환기를 설계하였다. EEPROM의 쓰기와 소거동작에서 요구되는 높은 프로그래밍 전압의 크기를 낮추기 위한 지역전계강화 효과가 소개된다. 프로그래밍 모드에서 EEPROM의 선형적 저장능력을 관찰하기 위해 MOSIS의 $1.2\;{\mu}m$ double-poly CMOS 공정을 이용하여 셀이 제작되었다. 그 결과 1.25V와 2V구간에서 10mV 미만의 오차 내에서 셀이 선형적으로 프로그램 되는 것을 보았다. 이러한 실험 결과를 이용하여 프로그램 가능한 A/B 변환기의 동작이 Hspice에서 시뮤레이션 되었으며, 그 결과 A/D 변환기가 $37\;{\mu}W$의 전력을 소모하고 동작주파수는 333MHz 정도인 것으로 관찰되었다.

• 대한환경공학회지
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• 제34권2호
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• pp.103-108
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• 2012

연소과정 중에 발생하는 질소산화물을 저감하는 기술인 MILD 연소로는 연소용 공기 및 연료로 고온의 배기가스가 유입되는 양에 따라 질소산화물 저감 특성이 많은 영향을 받는다. 일반적인 MILD 연소로는 연료와 연소용 공기는 수직 상향방향이고 배기가스는 수직하향 방향으로 흐르면서 배기가스가 유입되는데 이러한 형태보다 더욱 배기가스의 유입량을 증가시키기 위한 방법으로 동심원관형태의 MILD 연소로를 사용하고 있다. 본 연구에서는 바깥 원통의 배기가스 통로에서 안쪽 원통의 연소통로 사이에 연결관을 설치하고 배기가스를 유입하기 위한 공기노즐을 동심원관 형태로 설치하여 공기분사속도, 노즐 직경, 배기가스측 압력과 연소로측 압력 차이의 변화에 따른 유입량 특성을 수치해석을 통해 살펴봄으로써 MILD 연소로에서 더욱 적극적인 배기가스의 유입량 특성을 파악하는 것을 연구하였다. 공기노즐 분사속도의 증가에 따라 유입량은 속도의 제곱근에 비례하는 것을 알았고 배기가스 측과 연소로 측의 압력차의 크기에 선형적으로 감소하는 것을 관찰하였다. 공기노즐 출구 위치의 변화는 유입량 변화에 큰 영향이 없음을 알 수 있었다.

• 한국수소및신에너지학회논문집
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• 제24권6호
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• pp.573-579
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• 2013

Hydrogen engine with homogeneous charged compression ignition can achieve high efficiency by high compression ratio and rapid chemical reaction rates spatially. However, it needs to expansion of the operation range with over-all load conditions which is very narrow due to extremely high pressure rise rate. The adoption of the lean boosting in a HCCI $H_2$ engine is expected to be effective in expansion of operation range since minimum compression ratio for spontaneous ignition is decreased by low temperature combustion and increased surround in-cylinder pressure. In order to grasp its possibility by using lean boosting in the HCCI $H_2$ engine, compression ratio required for spontaneous ignition, expansion degree of the operation range and over-all engine performance are experimentally analyzed with the boosting pressure and supply energy. As the results, it is found that minimum compression ratio for spontaneous ignition is down to the compression ratio(${\varepsilon}$=19) of conventional diesel engine due to decreased self-ignition temperature, and operation range is extended to 170% in term of the equivalence ratio and 12 times in term of the supply energy than that of naturally aspirated type. Though indicated thermal efficiency is decreased by reduced compression ratio, it is over at least 46%.

• 한국추진공학회지
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• 제17권5호
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• pp.86-94
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• 2013

로켓의 연소불안정과 관련되어 분사기의 동특성을 연구하는 일은 중요하다. 와류형 분사기의 동특성에 대해서는 많은 연구가 이루어졌지만 충돌형 분사기의 동특성에 대해서는 알려진 바가 거의 없다. 따라서 본 연구에서는 충돌형 분사기의 동특성을 규명하기 위해 이에 관한 실험을 수행하였으며 동적거동을 생성시키기 위해 특별히 제작된 압력섭동기(mechanical pulsator)가 사용되었다. 가진주파수와 매니폴드 압력의 여러 조건 하에서 게인(gain)과 위상차(phase difference)를 분석하였고 주파수는 5, 10, 15 Hz의 낮은 영역에 맞춰졌다. 제트 속도를 결정하기 위한 방법에 대해 논의하였으며 실험과정 중에 나타난 특정현상이 클라이스트론(Klystron) 효과와 관련이 있는 것으로 판단되어 이에 대해 고려하였다.

• Journal of Electrical Engineering and Technology
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• 제9권5호
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• pp.1511-1519
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• 2014

The objective of this paper is to propose a modelling of a small compressed air energy storage system, which drives an induction generator based on a field-oriented control (FOC) principle for a renewable power generation. The proposed system is a hybrid technology of energy storage and electrification, which is developed to use as a small scale of renewable energy power plant. The energy will be transferred from the renewable energy resource to the compressed air energy by reciprocating air compressor to be stored in a pressurized vessel. The energy storage system uses a small compressed air energy storage system, developed as a small unit and installed above ground to avoid site limitation as same as the conventional CAES does. Therefore, it is suitable to be placed at any location. The system is operated in low pressure not more than 15 bar, so, it easy to available component in country and inexpensive. The power generation uses a variable speed induction generator (IG). The relationship of pressure and air flow of the compressed air, which varies continuously during the discharge of compressed air to drive the generator, is considered as a control command. As a result, the generator generates power in wide speed range. Unlike the conventional CAES that used gas turbine, this system does not have any combustion units. Thus, the system does not burn fuel and exhaust pollution. This paper expresses the modelling, thermodynamic analysis simulation and experiment to obtain the characteristic and performance of a new concept of a small compressed air energy storage power plant, which can be helpful in system designing of renewable energy electrification. The system was tested under a range of expansion pressure ratios in order to determine its characteristics and performance. The efficiency of expansion air of 49.34% is calculated, while the efficiency of generator of 60.85% is examined. The overall efficiency of system of approximately 30% is also investigated.

• Tribology and Lubricants
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• 제32권6호
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• pp.183-188
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• 2016

Engine oil plays an important role in the mechanical lubrication and cooling of a vehicle engine. Recently, engine development has focused on the adoption of gasoline direct injection (GDI) and turbocharging methodology to achieve high-power and high-speed performance. However, oil dilution is a problem for GDI engines. Oil dilution occurs owing to high-pressure fuel injection into the combustion chamber when the engine is cold. The chemical components of engine oil are currently developed to accommodate gasoline fuel; however, bio-alcohol mixtures have become a recent trend in fuel development. Bio-alcohol fuels are alternatives to fossil fuels that can reduce vehicle emissions levels and greenhouse gas pollution. Therefore, the chemical components of engine oil should be improved to accommodate bio-alcohol fuels. This study employs a 2.0 L turbo-gas direct injection (T-GDI) engine in an experiment that dilutes oil with fuel. The experiment utilizes a variety of fuels, including sub-octane gasoline fuel (E0) and a bio-alcohol fuel mixture (Ethanol E3~E7). The results show that the lowest amount of oil dilution occurs when using E3 fuel. Analyzing the diluted engine oil by measuring density and moisture with respect to kinematic viscosity shows that the lowest values of these parameters occur when testing E3 fuel. The reason is confirmed to influence the vapor pressure of the low concentration bio-alcohol-fuel mixture.

• 한국화재소방학회논문지
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• 제26권4호
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• pp.1-9
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• 2012

본 연구에서는 중소기업형의 밀가루 제조공정 및 각질제거용 기능성 비누를 생산하는 화장품 제조공정에서의 분진들을 채집하여 폭발 및 열적특성을 비교하기 위해 실험을 수행하였다. 폭발실험은 Hartman식 분진폭발장치를 이용하였고, 열적실험은 DSC 및 TGA를 이용하여 활석첨가시 농도의 변화에 따른 폭발압력 및 폭발하한계와 온도에 따른 무게감량과 흡열량을 측정하였다. 폭발실험결과 두 시료 모두 활석분진의 비율이 증가할수록 폭발하한농도가 증가하는 것을 볼 수 있었고, 폭발압력은 감소됨을 확인하였다. 그리고 DSC 실험결과 활석의 첨가량이 증가할수록 열유속은 감소하고 온도 또한 약간의 감소상태인 것으로 분석되었다. 또한 두 시료 모두 승온 속도가 증가 할수록 흡열개시온도가 낮은 온도부분으로 이동하고 있으며, 흡열량도 크게 증가하였다. 아울러 TGA 실험결과 활석의 양이 증가할수록 전체 무게감량이 줄어드는 것으로 나타났다. 향후 분진폭발메커니즘의 지속적 연구와 보완이 효과적인 분진폭발예방 대책수립에 기여할 것으로 기대된다.

• 한국추진공학회지
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• 제27권1호
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• pp.37-48
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• 2023

본 연구에서는 정상 상태 및 천이 상태에 따른 항공기용 터보팬 엔진의 성능해석 모델링을 수행하였다. 대상 엔진은 Pratt & Whitney 사의 F100-PW-229으로 선정하여 팬, 고압 압축기, 연소기, 고압터빈, 저압 터빈, Mixer, 수축-확산형 노즐 등의 구성품을 모델링하였다. 또한, 이차 유로를 통한 터빈에서의 냉각 효과를 적용하였다. Simulink를 이용하여 터보팬 엔진 성능해석 프로그램을 자체 개발함에 따라 해석의 자유도가 높으며, 엔진 제어기 설계에 활용이 용이한 구성의 성능해석 프로그램을 개발하였다. 개발된 성능해석 프로그램은 상용 프로그램인 GASTURB 해석 결과와의 비교를 통하여 검증하였다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 춘계학술대회논문집
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• pp.197-202
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• 2006

The low-altitude earth observation satellite is generally equipped with high performance camera as a main payload which is vulnerable to vibration environment. During the launch process of a satellite, the combustion and jet noise of launch vehicle produce severe acoustic environment and the acoustic loads induced may damage the critical equipments of the satellite including the camera. Therefore to predict and simulate the effect of the acoustic environment which the satellite has to sustain at the lift-off event is very important process to support the load-resistive design and test-qualification of components. Statistical Energy Analysis(SEA) has been widely used to estimate the vibro-acoustic responses of the structures and gives statistical but reliable results in the higher frequency region with less modeling efforts and calculation time than the standard FEA. In this study, SEA technique has been applied to a 3-Dimensional model of a low-altitude earth observation satellite to predict the acceleration responses on the structural components induced by the high level acoustic field in the launch vehicle fairing. In addition, the expected response on each critical component panel was calculated by the classical method in consideration of the mass loading and imposed sound pressure level, and then compared with SEA results.