• 제목/요약/키워드: Ion Engine

검색결과 62건 처리시간 0.026초

제올라이트 종류 및 이온교환 물질에 따른 NH3-SCR 촉매 반응 특성 (The Effects of Zeolite Structure and Ion-exchange Material on NH3-SCR Reaction)

  • 황인혜;이준호;김홍석;정용일
    • 한국자동차공학회논문집
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    • 제22권1호
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    • pp.135-141
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    • 2014
  • $NH_3$-SCR has high NOx removal efficiency approximately 80~90%. Recently, the copper or iron ion-exchanged zeolite catalysts are widely used as automobile SCR catalysts. In this paper, the effect of the space velocity, temperature of reaction and $NO_2$ addition on the $NH_3$-SCR reaction were studied using various zeolite SCR catalysts. The test was conducted with small sized fresh catalysts in a laboratory fixed-bed flow reactor system using simulated gases. It is found that the activity of the BEA is better than MFI. It seems that three-dimensional framework and a wide pore entrance of BEA enhances the SCR activity. It is also found that low temperature activity of Cu-zeolites was better than Fe-zeolites. Once $NO_2$ was added, the NOx conversion activity of the Cu-zeolite was slightly enhanced, whereas remarkable improvement was achieved by Fe-zeolite.

Lineup of Microwave Discharge Ion Engines $"\mu"$ series

  • Kuninaka, Hitoshi;Nishiyama, Kazutaka;Hayashi, Hiroshi;Hosoda, Satoshi;Shimizu, Yukio;Koizumi, Hiroyuki
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.546-549
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    • 2008
  • Institute of Space and Astronautical Science of Japan Aerospace Exploration Agency(ISAS/JAXA) successfully developed and operated the microwave discharge ion engines onboard Hayabusa asteroid explorer. The ${\mu}10$ ion engines feature the cathode-less plasma generation in both the ion generators and neutralizers with the results of long life and high reliability in space. Based on the space achievements of ${\mu}10$ ion engines with 8mN thrust, 3,000sec Isp and 350W consumption power, several programs are currently under developments: ${\mu}20$, ${\mu}10$HIsp and ${\mu}1$. The first is a 20-cm diameter microwave discharge ion engine, aiming to achieve 30mN/kW in the thrustto-power ratio for the asteroid sample return mission larger than Hayabusa. The second is a high Isp version of ${\mu}10$, and exhausts the plasma beam over 10,000sec Isp using 15kV acceleration voltage for deep space missions to such as Jupiter and Mercury. The third is ${\mu}1$ to be adapted to small satellites for drag-free.

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하이브리드 로켓의 연소기술동향 분석

  • 김용모;윤명원;김윤곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2001년도 제17회 학술발표회 논문초록집
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    • pp.55-60
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    • 2001
  • Recently, there have been many research efforts to improve the fuel regression rate in the hybrid rocket engines. In the present study, the ongoing research and development of the next general ion hybrid rocket engine are systematically reviewed. The detailed discussions have been made for the innovative combust ion technologies including the vortex hybrid rocket engines , cryogenic sol id propellant hybrid rocket engine, and the gas generator hybrid rocket engines.

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수소기관의 이상점화에 의한 역화발생 (Backfire Occurrence by Abnormal Electric Discharge in Hydrogen Fueled Engine)

  • 김윤영;류태호;이종태
    • 한국수소및신에너지학회논문집
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    • 제13권1호
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    • pp.65-73
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    • 2002
  • Because of low flame ion density in hydrogen-air mixture, many residual electric energy could be existed in the ignition system of hydrogen engine, If these residual energy discharged abnormally during intake stroke, it may be the cause of backfire occurrence which is serious problem in development of hydrogen fueled engine but unsolved in spite of many concerned research on it. In this study, the possibility of backfire occurrence by abnormal electric discharge and countermeasure of that were investigated by using the experimental single cylinder hydrogen fueled engine with two types of ignition system. The results show that abnormal electric discharge appeared in low load with low ion density and then results in back fire occurrence, It is also seen that countermeasure method installing larger earth resistance in high tension code is effective to control abnormal electric discharge.

이온전류법에 의한 가솔린엔진 연소실 형상별 급속연소효과 연구 (A Study on the Effect of Fast Burn for Different Combustion Chamber Geometries of Gasoline Engine Using an Ion Current Method)

  • 강건용;서승우;정동수;장영준
    • 대한기계학회논문집
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    • 제17권6호
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    • pp.1633-1639
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    • 1993
  • 본 연구에서는 급속연소기술의 가솔린엔진에 적용을 목적으로 흡입과정시 강한 와류(swirl)를 생성하는 마스크부착 헤드(masked shroud head, MSH)형을 급속연 소형으로 제작하여 마스크부착 헤드형에서의 급속연소효과를 이온전류법에 의한 화염 속도를 측정하므로서 규명하려한다. 이온전류는 이온탐침계(ion probe)를 연소실 표면의 두 지점에 설치하여 검출하며, 이온전류 신호를 정성적인 방법으로 검증한 후 표준 헤드형과 마스크부착헤드형을 장착한 엔진에 대해서 화염전파 속도를 비교 측정 한다. 측정된 화염 전파속도는 정확한 연소특성 분석을 위해 각 사이클에서의 값을 표본으로 하는 통계적 방법으로 처리한다.

기어 래틀 저감을 위한 시스템 파라미터 연구 (A Study on the System Parameters to Reduce the Idle Gear Rattle)

  • 안병민;장일도;최은오;홍동표;정태진
    • 한국자동차공학회논문집
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    • 제6권3호
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    • pp.88-96
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    • 1998
  • The rattle noise is the most significant in many kinds of manual gearbox nioses, which is generated at the idle stage of the engine operation. The main torsional vibrat- ion source of the driveline is the fluctuation of the engine torque. The gear rattle is impacts generating in the backlash of the free gear due to this torsional vibration. Many researchers reported the clutch torsional characteristic optimization method to reduce the idle gear rattle but only few of them give sufficient consideration to the system parameters like gear backlash, drag torque, system inertia, inertia distribution, engine torque fluctuation, idle engine rotation speed, and accessory load. In this paper, influence rate of system parameters on the gear rattle is presented and counterplans like backlash reduction, drag torque increase, inertia addition, inertia distribution modification and engine torque characteristic control are suggested.

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부실식 정적연소실내 연소특성에 관한 연구 (II) 임계연락공의 형상변화에 따른 연소촉진효과 (Combustion Characteristics in a Constant Volume Combustion Chamber with Sub-Chamber (II) Effect of Combustion Promotion with Configuration Change of the Critical Passagehole)

  • 김봉석;권철홍;류정인
    • 대한기계학회논문집
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    • 제17권10호
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    • pp.2611-2623
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    • 1993
  • To construct the design back data for a lean-burn gas engine, we investigated the combustion characteristics in the main chamber using a constant volume combustion chamber with subchamber. The combustion characteristics with configuration change of the critical passageholes have been studied by taking pressure data, schlieren photograph, ion current and light emission signal of flame. Heat release rate with various critical passageholes also have been analysed by using the combustion model of a prechamber diesel engine. It was found that combustion characteristics in the main combustion chamber were greatly influenced by the geometric configurations of critical passagehole.

엔진실린더 모형 연소실내의 메탄-공기 예혼합기의 화염전파속도 특성 (Propagation Speed Characteristics of Premixed Methane-Air Flame in a Combustion Chamber with Model of Engine Cylinder)

  • 전충환
    • Journal of Advanced Marine Engineering and Technology
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    • 제22권2호
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    • pp.225-231
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    • 1998
  • Flame propagation speed characteristics of methante-air mixtures were experimentally investigated in combustion chamber modelled engine. Flame propagation process was known as a funtion of equivalence ratio initial pressure and initial temperature. Ion probe and schlieren photograph were applied to measure the local flame speed and flame radius in quiescent mixtures. Pressure was also measured to make sure of the reproducibility and to apply combustion analysis. Burning velocity was calculated from the flame propagation speed and combustion analysis. Flames were developed faster with higher initial pressure and initial temperature but showed maximum propagation speed at equivalence ratio 1.1 regardless of initial pressure and temperature. Local flame speed was maximum values at near midpoint between center and wall.

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2사이클 기관 흡기 포오트의 가스 유동 특성에 관한 연구 (A study on the characteristics of gas flow in inlet port of 2 cycle engine)

  • 이창식
    • 대한기계학회논문집
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    • 제11권5호
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    • pp.725-730
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    • 1987
  • 본 연구에서는 2사이클 기관의 흡입 포오트 부근의 가스 유동을 레이저 도플 러 유속계를 이용하여 측정하고 가스의 평균 속도, 속도 변동, 유속 벡터 등을 기관의 회전 속도, 실린더 헤드의 모양 및 실린더로의 흡입 속도 측정점의 위치 변화에 대하 여 비교 검토하고, 유동 특성을 고찰하였다.

SIMULATION OF KNOCK WITH DIFFERENT PISTON SHAPES IN A HEAVY-DUTY LPG ENGINE

  • CHOI H.;LIM J.;MIN K.;LEE D.
    • International Journal of Automotive Technology
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    • 제6권2호
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    • pp.133-139
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    • 2005
  • In this study, a three-dimensional transient simulation with a knock model was performed to predict knock occurrence and autoignition site in a heavy-duty LPG engine. A FAE (Flame Area Evolutoin) premixed combustion model was applied to simulate flame propagation. The coefficient of the reduced kinetic model was adjusted to LPG fuel and used to simulate autoignition in the unburned gas region. Engine experiments using a single-cylinder research engine were performed to calibrate the reduced kinetic model and to verify the results of the modeling. A pressure transducer and a head-gasket type ion-probe circuit board were installed in order to detect knock occurrences, flame arrival angles, and autoignition sites. Knock occurrence and position were compared for different piston bowl shapes. The simulation concurred with engine experimental data regarding the cylinder pressure, flame arrival angle, knock occurrence, and autoignition site. Furthermore, it provided much information about in-cylinder phenomena and solutions that might help reducing the knocking tendency. The knock simulation model presented in this paper can be used for a development tool of engine design.