• 대한기계학회논문집B
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• 제22권8호
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• pp.1101-1110
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• 1998

Computational investigation was conducted to examine the performance of a high pressure common-rail fuel injection system which is used to power a passenger car direct injection (Dl) diesel engine. The pipe flows were modeled by one dimensional wave equation and solved by implicit FDM Each volume of injector was considered as chambers with orifice nozzle in connections. These simulation results were compared with the experimental data of Ganser Hydromag. The comparison of needle life and rate of injection between simulation data and experimental data showed quite a good agreement Different shape of injection rate can be made by adjusting the size of inlet orifice and exit orifice in the piston chamber The pilot injection was accomplished by adjusting command signal.

• 한국자동차공학회논문집
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• 제4권2호
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• pp.147-157
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• 1996

Natural gas is gaining more attraction as a future fuel in particular both for environmental protection and energy conservation. In order to bring about more widespread use of gaseous engines, the technology capable of achieving output and efficiency performance equivalent to that of diesel engines needs to be developed. In the present paper, the requirements of the pilot torch from pre-chamber for ensuring ignition and promoting combustion are discussed by means of taking high-speed flame photography and system can run with leaner mixture of various fuels comparing to the electric plug ignition system cause the ignition delay period ignited with the torch and the combustion period are very short in spite of changing A/F of gaseous fuels in the main chamber. However, the suitable piston-cavity design for the use of lower-hydrocarbon fuels such as propane and butane must be discussed increasingly in the mear future.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2002년도 ICCAS
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• pp.66.2-66
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• 2002

In this study, a novel systematic design procedure by Genetic Algorithm of a two stage relief valve is proposed. First of all, a mathematical model describing the dynamics of a balanced piston type relief valve has been derived. Governing equations such as dynamic equations for the main spool and the pilot spool and flow equations for each orifice are established. The mathematical model is verified by comparing the results of simulation with that of experiments. Furthermore, influences of the parameters on the dynamic characteristics of a relief valve have been investigated by simulation of the proposed model. Major design parameters on the valve response are determin...

• 드라이브 ㆍ 컨트롤
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• 제14권4호
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• pp.17-22
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• 2017

In this study, the back-drivability of the single-rod and double-rod type EHAs (Electro-Hydrostatic Actuators) was compared by computer simulation and experiments. The back-drivability of EHAs exhibit non-linear behavior like their force tracking performance. In case of the double-rod type EHA, the back-drivability was mostly influenced by the bulk modulus of oil that changes with the working pressure due to entrapped air. The back-drivability of the single-rod type EHA was directly affected by the operation states of its pilot-operated check valves, while the asymmetrical piston geometry and the non-linear bulk modulus of oil also made the dynamic response in building up the cylinder pressure dependent on the operating conditions.

• 생명과학회지
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• 제16권3호
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• pp.534-539
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• 2006

크립토스포리디움은 염소내성이 매우 강해 일반적인 표준정수처리공정의 소독으로는 제거가 불가능하다. 따라서 본 연구에서는 오존 및 UV를 이용한 단위소독공정에서 DAPI/PI 및 in vitro excystation을 이용하여 크립토스포리디움 불활성화를 평가하였으며, 또한 오존을 이용한 고도산화처리 파일럿에서는 세포배양법을 이용하여 크립토스포리디움 불활성화를 평가하였다. 오존 소독연구는 50 mL 용량의 piston type batch reactor에서 용존오존을 자동적으로 측정해주는 flow injection analysis (FIA) 시스템을 이용하여 실험한 결과, 1 log 제거에 필요한 CT값은 $25^{\circ}C$에서 DAPI/PI 및 in vitro excystation에 의해 각각 약 1.8, 2.2 $mg/L{\cdot}min$으로 나타났으며, 2 log 제거에 필요한 CT값은 각각 약 3.2, 3.8 $mg/L{\cdot}min$으로 나타났다. 또한 $5^{\circ}C$에서 크립토스포리디움 1 log 제거에 필요한 CT값은 DAPI/PI 방법에 의해 약 9.1 $mg/L{\cdot}min$으로 나타났으며, 2 log제거에 필요한 CT값은 14.8 $mg/L{\cdot}min$로 나타나, 같은 소독효과를 나타내기 위해서 저온에서는 상온에서보다 요존 요구량이 약 $4{\sim}5$배 정도 증가하여야 함을 확인하였다. 40 L규모의 오존 반응조를 이용한 파일럿 실험에서는 정수처리공정상 모래여과를 거친 물에 살아있는 크립토스포리디움을 접종한 것을 시료로 하여 연속적으로 흐르게 한 다음, 오존량을 변화시키고 체류시간은 5분으로 고정하여 불활성화를 평가하였다. 실험결과, 8 $mg/L{\cdot}min$의 CT값에서 DAPI/PI 및 excystation과 같은 생사판별법을 이용하였을 경우에는 약 0.2 log정도의 불활성화를 나타내었으며, 세포감염시험법을 이용하였을 경우에는 약 1.2 log정도의 불활성화를 나타냈다. 오존에 의한 크립토스포리디움의 소독능 평가에 단위공정 및 파일럿 실험 모두 2가지 생사판별법(DAPI/PI와 excystation) 사이에는 큰 차이를 나타내지 않았으나, 생사판별법과 세포감염시험법 사이에는 현저한 차이를 나타내었는데, 이는 세포감염시험법으로 측정하는 sporozoite 및 merozoite로의 분화과정이 생사판별법이 근거한 세포벽의 구조와 기능 유지 보다 더 오존 소독에 더 민감함을 알 수 있었다. 파일럿 실험에서의 CT값이 piston batch reactor에서의 CT값 보다 낮게 나타난 것은 파일럿 실험에서 수작업으로 인한 용존 오존 측정이 정밀하지 못하여 IOD가 농도에 반영되지 않았고, 반응조 규모(50 mL vs 40 L) 및 형태(회분식 vs 연속식)의 차이에 기인하는 것으로 여겨진다. 한편, UV를 이용한 단위공정에서는 크립토스포리디움 1, 2 log 제거에 필요한 IT값은 $25^{\circ}C$에서 각각 DAPI/PI 방법에 의해 약 25, 50 $mWs/cm^2$로 나타났으며, $5^{\circ}C$에서의 크립토스포리디움 1, 2 log제거에 필요한 IT값은 약 40, 80 $mWs/cm^2$로 나타났다. 온도 $20^{\circ}C$ 감소 시 약 60% 정도의 IT값이 더 필요한데, 이것은 저온에서는 약한 자외선을 발산하는 저압저출력 UV 램프의 특성 때문인 것으로 사료되었다.

• 한국항공우주학회지
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• 제47권9호
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• pp.607-616
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• 2019

항공우주비행체 정적구조시험을 위한 과하중 방지를 위해 사용되는 하중제한밸브(LLV)의 파일럿 스테이지의 주요 구성품들에 대한 자유물체도 분석을 수행하였다. 이 분석을 통하여 유압작동기의 동일한 힘에서 일관성있게 포펫 개방되도록 하기 위해서는 파일럿스테이지에 있는 두 포펫의 직경비($(D_2)^{ten}/D_2)^{comp}$)가 작동기의 피스톤 면적비($A_{comp}/A_{ten}$)와 동일해야만 한다는 것을 보였다. 실험실에서 외산으로 수입하여 사용하고 있는 4개의 서로 다른 하중제한밸브의 포펫들 형상을 측정하고 대응되는 4개의 다른 용량을 갖는 유압작동기들의 피스톤 면적비들로부터 위의 분석결과가 타당함을 확인하였다. 두 개의 다른 파일럿스테이지로 수행한 "조절자 분해능시험들"의 결과들로부터 조절자 각 회전에서 얻은 Fi(포펫개방 순간의 작동기 힘)의 최대 표준편차는 각 평균값으로부터 0.3KN이고 표준편차를 각 평균값으로 나눈 무차원값으로 분석하면 최대편차는 3.7%이다. 이 결과로 부터 동일 포펫 직경비를 갖는 두 개의 파일럿스테이지들의 포펫은 각 조절자 회전에 대해 Fi/(평균 Fi) 값이 +/- 3.7% 범위에서 일관성 있게 개방되고 있음을 확인하였다. 위의 편차는 포펫 O-링의 마찰력으로부터 유발되는 것임을 보였다. 부가적으로 파일럿스테이지의 다른 주요부품인 포펫 스프링과 조절자의 주요설계인자들도 식별하였고 이들의 결정과정도 본 연구에서 보였다.

• 한국연소학회지
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• 제15권3호
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• pp.57-66
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• 2010

The purpose of this paper is to investigate the effects of fuel injection strategy and engine load on the structure and emissions characteristics of a DI diesel engine with 1.6L of piston displacement. In order to analyze the particulate matter (PM) and exhaust emissions characteristics in a direct injection diesel engine, the quantity of PM and exhaust emissions (including HC, CO and $NO_X$) were investigated under various injection strategies and engine loads. Two different injection strategies (one pilot/main injection and two pilots/main injection) was investigated under the various engine loads. A thermophoretic sampling method with a scanning electron microscope (SEM) were used to obtain the PM morphology (including primary particles, the size of the agglomerates, the number of agglomerates, the fractal dimension). The quantity of soot gradually increased with increasing engine load at both injection strategies. The primary particles in the PM agglomerates indicate that the average of the primary particle and radius of gyration increased as the engine load increased.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2002년도 추계학술대회 논문집
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• pp.501-506
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• 2002

In this study, a novel systematic design procedure by Genetic Algorithm of a two stage relief valve is proposed. First of all. a mathematical model describing the dynamics of a balanced piston type relief valve has been derived. Governing equations such as dynamic equations for the main spool and the pilot spool and flow equations for each orifice are established. The mathematical model is verified by comparing the results of simulation with that of experiments. Furthermore, influences of the parameters on the dynamic characteristics of a relief valve have been investigated by simulation of the proposed model. Major design parameters on the valve response are determined, which affect the system response significantly. And then, using the determined parameters, the optimization of the two stage relief valve by Genetic Algorithm, which is a random search algorithm can find the global optimum without converging local optimum, is performed. The optimal design process of a two stage relief valve is presented to determine the major design parameters. Fitness function reflects the changing pressure according to parameters. It is shown that the genetic algorithms satisfactorily optimized the major design parameters of the two stage relief valve.

• 드라이브 ㆍ 컨트롤
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• 제14권4호
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• pp.9-16
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• 2017

In this study, the force tracking performance of the single-rod and double-rod type EHAs (Electro-Hydrostatic Actuators) was compared by computer simulation and experiments. The force-controlled EHAs exhibit non-linear behavior that are significantly dependent on operation conditions. The investigation focused on localizing the parameters that provide significant rise to the non-linearity. For this, the single-rod and double-rod type EHAs were mathematically expressed to derive their linear models. In parallel, they were modeled by a commercial simulation program including non-linear properties based on experimental results. It was shown that the dependency of the bulk modulus of oil with entrapped air on working pressure dominated the non-linearity in force control performance in case of the double-rod type EHA. The force control of the single-rod type EHA was influenced by much more elements. Besides the asymmetrical piston geometry and the non-linear bulk modulus of oil, its pilot-operated check valves made it dependent not only on the magnitude of reference input but also on its direction.

• 한국정밀공학회지
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• 제21권4호
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• pp.109-119
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• 2004

Rapid prototyping (RP) technologies have been widely used to reduce the lead-time and development cost of new products. $VLM-_{ST}$ process has been developed to overcome the currently developed RP technologies such as a large building time, a high building cost, an additional post-processing and a large apparatus cost. $VLM-_{ST}$ process requires an additional human interaction due to the manual stacking and bonding. Hence, building time, building cost and the part quality are dependent on the skill of labor. A novel RP process, fully automated $VLM-_{ST}$ process ($VLM-_{ST}$), has been developed to improve building efficiency of the process and the human dependency of the part. The objective of this work is to propose a $VLM-_{ST}$ process and to develop an apparatus for implementation of the process. $VLM-_{ST}$ process and its apparatus have various technical novelties such as two step cutting using a rotating table, an automatic stacking method using two pilot holes and two reference shapes, a concept of automatic unit shape layer (AUSL), and an automatic bonding using the bonding roller and building magazine. In order to examine the efficiency and the applicability of the proposed process, various three-dimensional shapes, such as a piston, a human head shape and a human bust shape, were fabricated on the apparatus.