• Title/Summary/Keyword: 엔진 시동

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A Numerical Study on Urea Melting Phenomena with Coolant and Electric Heaters (냉각수 및 전기히터를 이용한 우레아 해동 특성에 관한 수치적 연구)

  • Lee, Seung-Yeop;Kim, Man-Young;Park, Yun-Beom;Lee, Gyo-Woo;Kang, Hee-Young;Baek, Byung-Joon
    • Proceedings of the KAIS Fall Conference
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    • 2011.12b
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    • pp.402-405
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    • 2011
  • 디젤엔진에서 발생되는 PM과 $NO_X$는 강화되는 배기규제의 주요 저감대상으로서 이의 저감을 위한 다양한 후처리장치가 개발되고 있다. 이중 Urea-SCR은 $NO_X$의 전환율이 높고 연비에 미치는 영향이 작기 때문에 $NO_X$저감을 위한 최선의 장치로 인식되고 있다. 하지만, 우레아 수용액의 물성치 특성으로 인하여 동절기 $-20^{\circ}C$이하로 내려가는 지역에서 동결되는 문제점을 해결해야한다. 따라서 이러한 우레아 저장탱크에 해동 시스템을 적용하여 시동초기 우레아를 적정 시간내에 안정적으로 공급가능한 기술의 확보가 필요하다. 본 연구에서는 요소수 저장탱크 내부에 냉각수 순환 가열방식(CH)과 전기 가열방식(EH)을 이용하여 동결된 요소수의 해동현상에 대한 3차원 비정상상태 수치 해석을 수행하였다. 이를 통하여 해동 과정 중 나타난 액상분율, 온도영역 그리고 자연대류를 분석하여 각 가열 방식에 대한 해동특성을 비교하였으며 순수 갈륨 융해 실험 결과값과 수치 해석 결과값를 통하여 수치 해석 방법을 검증하였다. 결론적으로 1,000ml의 우레아 수용액이 확보되기까지의 시간은 CH의 경우, 275s, 그리고 EH의 경우, 230s임을 알 수 있었다.

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Design and Performance Evaluation of Integrated Exhaust Manifold (일체형 배기다기관 설계 및 성능 평가)

  • Oh, Jin-Ho;Ryu, Jeong-Soo;Kim, Jae-Hyun;Choi, Han-Ho
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.34 no.7
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    • pp.905-910
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    • 2010
  • Exhaust manifolds are the first structures to be developed by hydroforming; mass production of exhaust manifolds by this method will be possible soon. This is obviously related with tight emission regulation induced by environmental problems commonly for both domestic and worldwide and standards, thus evoking its solution for domestic automakers. Compared to conventional cast products, thin-gauge tubular hydroformed exhaust manifold have superior features; for example, in the hydroformed exhaust manifold, gas decomposition during the cold-start period of the engine is reduced by lowering the heat sink, and manufacturing process is simplified since less welding is involved. The aim of this study is to develop a hydroformed exhaust manifold; the study deals with the components, the hydroforming process, and tool design of the manifolds. The performance of the exhaust system is evaluated by performing flow analysis, heat-transfer analysis, heat-stress analysis, and fatigue analysis by using a computer.

Opening Characteristics of a Main Oxidizer Shut-off Valve at Different Valve Inlet Pressures (밸브 입구 압력 변화에 따른 연소기 산화제 개폐밸브 열림 특성)

  • Hong, Moongeun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.10
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    • pp.801-807
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    • 2020
  • Opening characteristics of a main oxidizer shut-off valve at different valve inlet pressures have been experimentally investigated. The pilot pressure at the moment of the valve opening increases linearly with increasing the valve inlet pressure and the increased pilot pressure reduces the valve travel time. As the pilot pressure increases at the moment of valve opening, the time to start opening the valve is delayed resulting in increasing the valve opening time. With the increment of the valve inlet pressure, the valve opening time is mainly determined by the time required for the pilot pressure to start opening the valve. Therefore the design of a pilot gas supply system can readily control the valve inlet pressure at the valve opening as well as the amount of oxidizer supplied to a combustion chamber during the engine startup.

An Experimental Study on the Performance and Characteristics of Emission for an S.I. Engine with Methanol-Reformulated Fuel (메탄올 개질 연료를 이용한 S.I. 엔진의 성능 및 배기 배출물 특성에 관한 연구)

  • Jang, Yeong-Jun;Choe, Seung-Hwan;Ha, Cheol-Ho;Jeon, Chung-Hwan
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.9
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    • pp.1193-1200
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    • 2001
  • There are many regulation test methods to be related with engine emissions such as CVS-75, D-13, ECE-15 modes and so on. Most of these modes are consisted of lots of transient conditions that have rapid acceleration, deceleration and cranking modes. In this experimental research, the engine characteristics of cranking, accelerating and power output in a S.I. engine were studied to compare with neat gasoline and alternative fuels of M30 (methanol 30%, aromatic series 32%, non-aromatic 38%) and M50 (methanol 50%, aromatic 30%, non-aromatic 20%) for performance and exhaust emissions. The results show that reformulated methanol fuels are better emissions reduction of 15.7% over than that of neat gasoline fuel especially in HC and CO emissions at cranking mode. And the accelerating performances coincide with the results of distillation curve. CO concentration for M50 fuel is varied in a just little for the condition of slow acceleration. At wide-open throttle condition, brake specific energy consumption of reformulated fuels is increased and thermal efficiency is some what lower than that of gasoline fuel.

Starting of Farming Diesel Engines According to Characteristics of Light Oil at Low Temperature (경유의 저온특성에 따른 농용 디젤엔진의 저온시동성)

  • 신승엽;김학주;이용복;김병갑;윤진하;김기택;양대준
    • Journal of Biosystems Engineering
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    • v.28 no.1
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    • pp.11-18
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    • 2003
  • This study was carried cut to get basic data of troubles in starting and supply of farm diesel engines in cold winter. The results of the study are summarized as follows: 1. As the result of farm survey. the proportions of farms which had starting problems or troubles in fuel supply in cold winter for the last 5 years were 38% for the farms with power-tillers and 32% for the farms with tractors. Most of the farms which had starting problems or troubles in fuel supply in cold winter used light oil for summer. spring or fall rather than for winter. 2. As the result of fuel supply test, fuel supply was stopped at -6$^{\circ}C$ and -18$^{\circ}C$ for summer light oil and winter light oil. respectively 3. The lowest temperatures of winter light oil for starting engine were -7.5$^{\circ}C$ for power-tiller. -12.5$^{\circ}C$ for tractor of 38ps, and -17.5$^{\circ}C$ for tractor of 45ps. which were 5~7.5$^{\circ}C$ lower than that of summer light oil. 4. The performance of engine starting and the trouble of fuel supply system at lower temperature were significantly improved by using winter hight oil rather than summer light oil.

Effect of Shroud Split on the Performance of a Turbopump Turbine Rotor (터보펌프 터빈 로터의 슈라우드 스플릿이 성능에 미치는 영향)

  • Lee, Hanggi;Jeong, Eunhwan;Park, Pyungoo;Yoon, Sukhwan;Kim, Jinhan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.4
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    • pp.25-31
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    • 2013
  • A blisk with rotor shroud is usually adopted in LRE turbine to maximize its performance. However it experiences the severe thermal load and resulting damage during engine stating and stop. Shroud splitting is devised to relieve the thermal stress on the turbine rotor. Structural analysis confirmed the reduction of plastic strain at the blade hub and tip. However, split gap at the rotor shroud entails additional tip leakage and results performance degradation. In order to assess the effect of shroud split on the turbine performance, tests have been performed for various settings of shroud split. For the maximum number of shroud splitting, measured efficiency reduction ratio was 2.65% to the value of original shape rotor.

The Wave Power Generator on Small Ship for Charging Engine Start-Up Battery (엔진 시동용 소형선 탑재형 파력 발전 시스템)

  • Kisoo, Ryu;Sungjin, Kang;Byeongseok, Yu
    • Journal of the Society of Naval Architects of Korea
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    • v.59 no.6
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    • pp.439-446
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    • 2022
  • Efforts to reduce carbon dioxide(CO2) emissions are being carried out due to climate environmental problems. Eco-friendly ships are also being developed, and various energy saving measures have been developed and applied. In ships, researches have been conducted in various fields such as electric propulsion system and energy saving devices. In addition, the development of ships using various renewable energy, such as kite using wind power and wind power generation, has been carried out. This paper proposes a plan to use renewable energy for ships by applying wave generators to small ships. In 2016, 130 small domestic ships drifted by sea due to discharge of starting storage batteries, and discharge cases accounted for the largest portion of the causes of domestic ship accidents. This is due to the excessive use of storage batteries for starting the main engine by departing in a weak storage battery state for small ships. Accordingly, two type wave power generators - opened flow wave power generator and enclosed vibrator type wave power generator - are developed for charging a starting storage battery when the ships are stationary at sea or port. Opened flow wave power generator utilizes the flow of fluid in the ship by using wave induced ship motion. Enclosed vibrator type wave power generator utilizes the pendulum kinetic energy located in a ship due to wave induced ship motion.

An Experimental Study on the Fundamental Characteristics of LPG Gas Injections System (LPG 가스분사시스템의 기초특성에 대한 실험적 연구)

  • Jang, Yeol-Sung;Woo, Sung-Dong;Kim, Hyeong-Sig;Park, Chan-Jun;Ohm, In-Yong
    • 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.

Prediction of Battery Performance of Electric Propulsion Lightweight Airplane for Flight Profiles (비행프로파일에 대한 전기추진 경량비행기의 배터리 성능 예측)

  • Kim, Hyun-Gi;Kim, Sungchan
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.22 no.5
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    • pp.15-21
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    • 2021
  • Electrically powered airplanes can reduce CO2 emissions from fossil fuel use and reduce airplane costs in the long run through efficient energy use. For this reason, advanced aviation countries such as the United States and the European Union are leading the development of innovative technologies to implement the full-electric airplane in the future. Currently, the research and development to convert existing two-seater engine airplanes to electric-powered airplanes are underway domestically. The airplane converted to electric propulsion is the KLA-100, which aims to carry out a 30-minute flight test with a battery pack installed using the engine mounting space and copilot space. The lithium-ion battery installed on the airplane converted to electric propulsion was designed with a specific power of 150Wh/kg, weight of 200kg, and a C-rate 3~4. This study confirmed the possibility of a 30-minute flight with a designed battery pack before conducting a flight test of a modified electrically propelled airplane. The battery performance was verified by dividing the 30-minute flight profile into start/run stage, take-off stage, climbing stage, cruise stage, descending stage, and landing/run stage. The final target of the 30-minute flight was evaluated by calculating the battery capacity required for each stage. Furthermore, the flight performance of the electrically propelled airplane was determined by calculating the flight availability time and navigation distance according to the flight speed.