• Title/Summary/Keyword: 기관동력학

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Effects of Intake Gas Mixture Cooling on Enhancement of The Maximum Brake Power in a 2.4 L Hydrogen Spark-ignition Engine (수소 내연기관의 흡기 냉각 방법에 따른 최고 출력 향상에 관한 연구)

  • Kim, Yongrae;Park, Cheolwoong;Oh, Sechul;Choi, Young;Lee, Jeongwoo
    • Journal of the Korean Institute of Gas
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    • v.25 no.5
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    • pp.11-18
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    • 2021
  • Since hydrogen has the lower minimum ignition energy than that of gasoline, hydrogen could be also appropriate for the IC engine systems. However, due to the low ignition energy, there might be a 'back-fire' and 'pre-ignition' problems with hydrogen SI(Spark-ignition) combustion. In this research, cooling effects of intake gas mixture on the improvement of the maximum power output were evaluated in a 2.4 L SI engine. There were two ways to cool intake gas mixtures. The first one was cooling intake fresh air by adjusting inter-cooler system after turbocharger. The other one was cooling hydrogen fuel before supplying by using heat ex-changer. Cooling hydrogen was performed under natural aspired condition. The result showed that cooling fresh air from 40 ℃ to 20~30 ℃ improved the maximum brake power up to 6.5~8.6 % and cooling hydrogen fuel as -6 ℃ enhanced the maximum brake power likewise.

A Comparative Study on Engine Performance and Exhaust Emission Characteristics of Response Power 150HP & 240HP Turbocharged Marine Diesel Engine (대응출력 150마력 및 240마력 터보차저 선박용 디젤기관의 동력성능 및 배출특성 비교에 관한 연구)

  • Kim, Tae-Hyun;Lee, Chi-Woo
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.12 no.1
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    • pp.43-51
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    • 2013
  • This is a thesis about the experiment of comparison characteristic of power and exhaust gas in the same condition between diesel engine that is equipped turbocharger different from response power to increase effectiveness of the engine which is recently used in a lot of industry which requires high power. Resulting of the experiment with natural aspiration diesel engine and turbocharger diesel engine, difference in low speed is not significant, but in high speed, effectiveness of turbocharger diesel engine is much higher than the other one. In other hand, in exhaust gas experiment, turbocharger model exhausts more $NO_X$ and $O_2$, but it doesn't significantly affect the result when it comes with decreasing of $CO_2$ and effectiveness of increased power characteristic. As a result, the turbocharger diesel engine is economically effective comparing with the natural aspiration diesel engine.

A Study on Engine Performance and Exhaust Emission Characteristics of Response Power 150HP Turbocharged Diesel engine (대응출력 150마력 터보차저 디젤기관의 동력성능 및 배출특성에 관한 연구)

  • Kim, Tae-Hyun;Lee, Chi-Woo
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.11 no.6
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    • pp.100-106
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    • 2012
  • This is a thesis about the experiment of comparison characteristic of power and exhaust gas in the same condition between diesel engine that is equipped turbocharger to increase effectiveness of the engine which is recently used in a lot of industry which requires high power. Resulting of the experiment with natural aspiration diesel engine and turbocharger diesel engine, difference in low speed is not significant, but in high speed, effectiveness of turbocharger diesel engine is much higher than the other one. In other hand, in exhaust gas experiment, turbocharger model exhausts more NOX and $O_2$, but it doesn't significantly affect the result when it comes with decreasing of $CO_2$ and effectiveness of increased power characteristic. As a result, the turbocharger diesel engine is economically effective comparing with the natural aspiration diesel engine.

Basic Experiment of P8250 Educational Engine Performance (P8250 학습용 엔진성능의 기초 실험)

  • Lim, Chang-Su;Choi, Jun-Seop;Wang, So-Rang
    • 대한공업교육학회지
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    • v.33 no.2
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    • pp.218-231
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    • 2008
  • The purpose of this study was made for the pre-teacher of university to enhance understanding for the concept of engine performance and to provide information regarding engine performance in the institute of teacher educator. This study was carried out through engine performance experiment with The Cussons Engine Test Bed P8250, internal combustion engine, in order to analyze data quantitatively, and apply and verify factors of controlling engine performance. The main results of this study are as follows: First, power and brake horsepower increased linearly, and torque over the mid-speed as engine rps(revolution per second) decreased. Second, the change of torque and specific fuel consumption were able to be verified and the concept of engine performance was able to be understood. Third, the experimental values of brake horsepower and torque on engine performance showed the same tendency as theoretical values. Fourth, air/fuel ratio increased proportionally as engine speed increased.

Movable Nozzle Performance Analysis by Using ADAMS (ADAMS를 이용한 가동 노즐 성능 평가 기법)

  • Kim, Joung-Keun;Jang, Hong-Been
    • Journal of the Korean Society of Propulsion Engineers
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    • v.13 no.4
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    • pp.30-35
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    • 2009
  • Effective-pivot effects on the thrust vector control performance of the flexible seal nozzle to be used to control the flight direction of missile were investigated by computer simulation. $2^3$-Design of experiment technique was applied and ADMAS was used for the surrogate technique. As a result, radial pivot position had more influence upon the nozzle actuating performance than axial pivot position. Connecting method of actuator was also important factor in determining effective-pivot effects on the thrust vector control performance of the flexible seal nozzle.

Analysis on the two-dimensional ablation phenomenon at nozzle throat with graphite (그라파이트 노즐목의 2차원 삭마현상 해석)

  • 윤덕진;강윤구
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1998.04a
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    • pp.35-35
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    • 1998
  • 고체 로켓 추진기관의 노즐을 개발하기 위해서는 주어진 체계 제한 조건내에서 기본적인 가스의 동력학, 내탄도에 의한 형상 설계, 재료 개발 및 적용 기술, 열전달 계산에 의한 열설계 및 해석 등이 종합적으로 적용되며 수많은 반복과정을 거쳐야 한다. 특히 최근에는 알루미늄 함유량을 증가시켜 연소가스의 온도가 300$0^{\circ}C$ 이상이 되는 고성능 추진제가 일반적으로 적용되고 있으므로 고온에 의한 열적문제가 심각하게 대두되고 있으며 이에 견디는 신뢰도가 높은 노즐 설계개발이 요구되고 있다. 노즐목을 노즐내에서 열부하가 가장 심한 곳으로 노즐목 확대에 의한 추력 손실을 최소화하기 위해 내삭마성이 강한 재료를 선정하여야 하며, 그래파이트는 이러한 조건을 만족시키는 소재의 하나로 많이 적용되고 있다.

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A Design of Expert System for Reconstruction of Automobile Collision Accidents (자동차 사고 재구성 전문가 시스템의 설계)

  • 김현경
    • Journal of Intelligence and Information Systems
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    • v.4 no.2
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    • pp.35-44
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    • 1998
  • 자동차 사고 재구성이란 사고 상황으로부터 가능한 모든 정보를 수집, 분석하여 사고 거동 및 원인을 규명하는 작업을 의미한다. 본 논문에서는 자동차 사고 재구성에 직접 적용이 가능하도록 개발된 범용성의 정성적 충돌 전문가 시스템의 Prototype을 소개한다. 이 시스템은 충돌 전 물체의 운동 방향과 공간에서의 정보가 주어졌을 때, 충돌로 인한 물체의 순간적인 운동을 정성적으로 예측한다. 분야 모델은 정성적 충돌 이론과 정성적 계산을 제공하는 정성적 수학의 지식 베이스로 구성된다. 충돌로 인한 물체의 운동을 해석하는 데 있어, 충돌 전 물체의 운동 방향과 충돌시의 기하학적 배치사이의 상호 작용을 분석하는 것이 그 핵심을 이루고 있다. 본 논문에서는 그 상호 작용을 밝혀 내어 정성적 표현 방식에 의거하여 해석하는 충돌 이론을 소개하였다. 추론 기관을 설계하는데 있어서는 동력학 정보뿐만 아니라 공간 정보를 추론하기 위한 기법이 제시되었다.

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전기철도차량 전력변환장치 성능시험 기술

  • Kim, Myeong-Ryong;Ryu, Jun-Hyeong
    • KIPE Magazine
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    • v.14 no.5
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    • pp.36-41
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    • 2009
  • 전기철도차량에는 대용량 추진제어 컨버터/인버터부터 소용량 스위칭 모드 전원장치에 이르기까지 철도차량의 운행에 필요한 각종 동력 및 전력을 공급하기 위한 여러 가지 형태의 전력변환장치가 사용되고 있다. 그 중 가장 대표적인 전력변환장치가 추진제어인버터와 보조전원장치이다. 전기철도차량의 성능평가는 전력변환장치의 성능평가라 할 수 있을 정도로 많은 비중을 전력변환장치가 차지하고 있다. 한국철도기술연구원은 국토해양부로부터 지정받은 성능시험기관으로서 국내 도시철도 및 철도차량의 성능평가를 수행하고 있다. 성능시험은 차량의 제작공정에 따라 부품시험, 구성품시험, 완성차시험, 예비주행 및 본선시운전의 각 단계별로 실시하고 그 시험기준으로 도시철도차량의 성능시험에관한기준 및 철도차량성능시험 시행지침이 적용된다. 성능시험기준을 근간으로 추진제어인버터와 보조전원장치의 성능시험 대한 시험항목과 시험방법에 대하여 소개한다.

A Study on the Improvement of New Growth Engine Fund Management Ways by PEF Vehicle (사모투자펀드 기구를 이용한 신성장동력투자펀드 운용방식의 개선에 관한 연구)

  • Chung, Ki-Yun;Lee, Cheol-Gyu
    • Journal of Korea Technology Innovation Society
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    • v.13 no.3
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    • pp.538-557
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    • 2010
  • Korean Government has supplied small-medium enterprises with various technology financing programs such as R&D grant." loans, equities, guarantees since 1980's. The purpose of this study is to render policy suggestions for policy makers by analysing problems with regard to regulations. The suggestions of this study are such as the following. First, the current three months of the fund formation period should be extended within six months for general partners to have enough time to raise funds in the current tough capital market situation. Second, the government's non priority loss devotion system should keep going to prevent general partner's moral hazard. Third, in order to fulfill the policy purpose that is to create globally well-known companies, the government investment ratio should scale up from the current 20% to 30% of the total fund size in that the stable capital supply for core technology commercialization, industrialization and globalization of companies is achieved. Finally, general partners of the New Growth Engine Fund should showoff their investment abilities to the potential investors such as institutional investors by accumulating all track records and know-hows that prove their specialities and implementing action plans to achieve the best result of their investment. This study provides general considerations of the selection procedure, the government investment ratio, the government priority loss devotion system and so on when formating the public funds.

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Design and Output Characteristic Analysis of Electro-Mechanical Ignition Safety Device (전기-기계식 점화안전장치 설계 및 출력 특성 해석)

  • Jang, Seung-Gyo;Lee, Hyo-Nam;Oh, Jong-Yun;Oh, Seok-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.12
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    • pp.1166-1173
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    • 2011
  • Electro-Mechanical Ignition Safety Device(EMISD) for solid rocket motor is designed and manufactured. The EMISD utilizes a true rotary solenoid for arming mechanism and an electric squib(initiator) for generating ignition energy. In order to prove the ignition capability of the EMISD, 10-cc Closed Bomb Test(CBT) is performed, which measures the pressure built by high temperature and high pressure gas generated by operating EMISD. The pressure built in the free volume of 10-cc closed bomb and the opening time of the ignition gas outlet are calculated using one dimensional gas dynamic model which is composed of the ideal gas equation and mass-energy conservation equation. Comparing the test result with model prediction, it is realized that the pressure built in the free volume of closed bomb due to the firing of EMISD, has the efficiency ratio of about 34%.