• Title/Summary/Keyword: engine intake system

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A Study on the Behavior of Liquid Film Flow in Intake Manifold - On the improvement of intake manifold system - (흡기관내(吸氣管內) 액막류(液膜流) 거동(擧動)에 관(開)한 연구(硏究) (I) - 흡기계통(吸氣系統)의 품질개선(品質改善)을 위(爲)하여 -)

  • Jeon, Heung-Sin;Lee, Gyu-Yeong;Park, Gyeong-Seok;Yang, Ok-Yong;Seong, Hwan-Tae
    • Journal of Korean Society for Quality Management
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    • v.9 no.2
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    • pp.15-25
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    • 1981
  • This paper deals with the experimental study on the behavior of fuel flow in intake manifold of gasoline engine. The main purpose of this study is an analysis of air stream velocity, behavior of liquid film flow, generation of atomization and atomization rate by using the basic apparatus which is manufactured the visible, straight tube type model of intake manifold. As the result, we have found factors which influenced on the behavior of liquid film flow in intake manifold.

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Simulation of Natural Gas Injected Dual-Fuel DI 2-Stroke Diesel Engine (천연가스를 파이럿오일과 이원공급하는 직접분사식 2행정 디이젤기관의 시뮬레이션)

  • Choi, In Su
    • Transactions of the Korean Society of Automotive Engineers
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    • v.3 no.3
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    • pp.9-18
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    • 1995
  • The substitution of conventional fuel oil by alternative fuels is of immense interest due to liquid oil shortage and requirements of emission control standard. Among the alternative fuels, natural gas may be the most rational fuel, because of its widespread resource and clean est burning. Meanwhile, engine simulation is of great importance in engine development. Hence a zero-dimensional combustion model was developed for dual-fuel system. Natural gas was injected directly into the cylinder and small amount of distillate was used to provide the ignition kernel for natural gas burning. The intake air and exhaust gas flow was modeled by filling and emptying method. Although the single zone approach has an inherent limitation, the model showed promise as a predictive tool for engine performance. Its simulation was also made to see how the engine performance was influenced by the fuel injection timings and amount of each fuel.

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A Study on the Effect of Exhaust Pipe Length of 4 Cycle 4 Cylinder S.I. Engine on the Performance (배기관의 길이변화가 4사이클 4기통 전기 점화기관의 성능에 미치는 영향에 관한 연구)

  • 정수진;김태훈;조진호
    • Journal of the Korean Society of Safety
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    • v.8 no.3
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    • pp.3-12
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    • 1993
  • In reciprocating internal combustion engine, engine performance Is greatly affected by volumetric efficiency. For gas flow, the dynamic effects caused by the pressure pulsation have influence on the volumetric efficiency and correlate to the configuration and pipe length of intake-exhaust system. In this study, the analytic investigation of the unstudy flow In exhaust pipe has been carried out by using the method of characteristics to predict volumetric efficiency. In conculusion, it is possible to take account of the exhaust pipe tuning effect in predicting the engine performance, by the analytic solution of the unsteady flow in the pipes, and comparision of prediction with experimental datas show a good agreement on the pressure varision in the exhaust pipe which has Influence on the volumetric efficiency and performance of engine.

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Precise Air-Fuel Ratio Control on Transient Conditions with the PC-ECU in SI Engine (PC-ECU를 이용한 SI 기관의 비정상상태 정밀공연비 제어)

  • Yoon, S.H.
    • Journal of ILASS-Korea
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    • v.5 no.3
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    • pp.9-16
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    • 2000
  • In a SI engine, three-way catalyst converter has the best efficiency when A/F ratio is near the stoichiometry. The feedback control using oxygen sensors in the commercial engine has limits caused by the system delays. So it is necessary to control fuel quantity in accordance with intake air amount in order to reduce exhaust emission and improve the specific fuel consumption. Precise A/F ratio control requires measurement of air amount with respect to the cylinder and injection fuel according to the air amount In this paper, we applied nonlinear fuel injection model and developed the algorithm of A/F ratio control. This algorithm includes the methods of measurement of transient air mass flowing into each cylinder, of calculation of injection pulse width for measured air mass, and the method of feedback and engine control by using lambda sensor. Also we developed control program for IBM-PC by using C++ Builder, and tested it in the commercial engine.

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A Study on the Problem-Solving Method and Thermal Efficiency Properties at the Time of High Expansion Realization in a 4-Cycle Diesel Engine (4사이클 디젤기관에서 고팽창 실현 시 문제점 해결방안과 열효율 특성에 대한 연구)

  • Jang, Tae-Ik
    • Journal of Advanced Marine Engineering and Technology
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    • v.33 no.6
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    • pp.835-842
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    • 2009
  • The present thesis carried out a research on a compression pressure's reduction phenomenon and its countermeasure according to the thermal efficiency improvement method by a Miller method in 4-cycle low speed diesel engine. In case of retardation of intake valve closing time in a engine, the theoretical heat efficiency shows a remarkably reducing trend when a compression ratio is not compensated. Accordingly, the thermal efficiency showed an increasing trend in case of compensating the compression ratio. Especially, it could be understood that the theoretical heat efficiency at near ABDC $100^{\circ}$ of intake valve closing time in case of compensation of the compression ratio was improved by around 25.1%, and the mean effective pressure was also increased by around 18.6%. Also, as the retardation of intake valve closing time increases, air quantity becomes insufficient due to a backflow phenomenon of intake air and thus thermal efficiency was decreased in a high load operation domain. The solving method of this problem is possible by supercharge. Therefore, in order to improve thermal efficiency by retardation of ntake valve closing time, the thermal efficiency improvement according to low compression is possible when there are a compensation device of a compression ratio and a supercharge device. This is a problem-solving method of low compression and high expansion cycle.

COMPUTATIONAL PREDICTION OF ICE ACCRETION AROUND A ROTORCRAFT AIR INTAKE (회전익기 공기흡입구의 표면발생 결빙에 관한 전산 예측)

  • Jung, K.Y.;Ahn, G.B.;Myong, R.S.;Cho, T.H.;Jung, S.K.;Shin, H.B.
    • Journal of computational fluids engineering
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    • v.17 no.2
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    • pp.100-106
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    • 2012
  • Ice accretion on the surface of aircraft in flight can adversely affect the safety of aircraft. In particular, it can cause degradation of critical aircraft performances such as maximum lift coefficient and total pressure recovery factor in engine air intake. In this study, computational prediction of ice accretion around a rotorcraft air intake is conducted in order to identify the impingement region with high droplet collection efficiency. Then the amount of ice accretion on the air intake, which is essential in determining the required power of ice protection system, is calculated. Finally, the effect of icing wind tunnel size is investigated in order to check the compatibility with the real in-flight test environment.

$\mu\textrm{p}$-based Electronic Control System for Automobiles Part1. Electronic Engine Control System (자동차의 마이크로프로셋서를 이용한 전자식 제어시스템에 대한 연구 제1편 : 전자식 엔진 제어시스템)

  • Chae, Suk;Kim, Young-Lip;Liu, Joon;Kim, Kwang-Rak;Bien, Zeungnam
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.17 no.5
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    • pp.15-21
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    • 1980
  • An engine control system in which the conventional mechanical ignition system is studied. The contact point of the breaker is replaced by the contactless magnetic pick up sensor from which the information of the speed and the position of the crankshaft is extracted , and further an electronic High Energy Ignitim System Is designed, implemented and tested . The High Energy Igniticwl System increases the secondary spark voltage of the ignition coil from the conventional 10000~15000 volts to the 30000~40000 volts resulting in improving the combustion efficiency. Also, instead of the conventional advimce mechanism forigniliontiming control, a microprocessorbased timinng mechanisn is installed to determine the ignition timing data in response to the engine rpm and the intake manifold vacuum.

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A Study on Characteristics of Performance and Emission by CRDI Engine's Injection Strategy (커먼레일 디젤기관에서 분사전략에 따른 성능 및 배출가스에 관한 연구)

  • Eom, Dong-Seop;Ko, Dong-Kyun;Ra, Wan-Yong;Lee, Seang-Wock
    • Journal of ILASS-Korea
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    • v.16 no.3
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    • pp.134-139
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    • 2011
  • Recent research has focused on engine combustion technology as well as application of after-treatment in order to comply with emission regulation. However, it is much more efficient way to control emissions from engine itself and furthermore research on engine control will provide the direction of after-treatment technology in future. Furthermore, emission standard regulation for passenger diesel vehicles has been stringent compared to others and nano-particles will be included in EURO6 regulation in Europe and similar emission standard will be introduced in Korea. A 3.0 liter high speed diesel engine equipped with by CRDI system of 160MPa injection pressure, and an intake/exhaust system of V type 6 cylinder turbo-intercooler was applied. The injection duration and injection quantity, pilot injection types which are related to CRDI and air/fuel ratio control applied by EVGT were changed simultaneously. Standard experiment procedure constituted dilution apparatus and CPC system to collect nano-particles and these test results were compared with regulated materials of CO, HC, NOx and investigated their relations and characteristics of nano-particles.

Ramjet Mode Combustion Test for a Dual-Mode Ramjet Engine Model with a Large Backward-Facing Step (큰 후향 계단이 있는 이중 모드 램젯 엔진 모델의 램젯 모드 연소 시험)

  • Yang, Inyoung;Lee, Kyung-jae;Lee, Yang-ji;Kim, Chun-taek
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.6
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    • pp.83-90
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    • 2016
  • Ramjet mode combustion test was performed for a dual-mode ramjet engine model. The engine model consists of an air intake, a combustor and a nozzle. The combustor in the model has a large backward-facing step, designed to be used as a part of a rocket-based combined cycle engine. The test was performed at the flight speed of Mach 5 and the altitude of 24 km. Strong combustion was established only when the fuel was injected from both of the bottom-side and cowl-side wall. When the total fuel stoichiometric ratio was 1.0, distributed as 0.5 on the cowl side and 0.5 on the bottom side, the flow became subsonic at some portion in the combustor by thermal choking, i.e., ramjet mode was established for this condition.

Flow and Combustion Characteristics according Control Strategy of Variable Valve Duration System for Compression Ignition Engine (압축착화기관용 가변밸브 듀레이션(VVD)시스템의 제어전략에 따른 유동 및 연소성능 해석)

  • Cho, Insu;Kim, Wootaek;Lee, Jinwook
    • Journal of ILASS-Korea
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    • v.25 no.2
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    • pp.45-50
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    • 2020
  • Recently, global warming and environmental pollution are becoming more important, and fuel economy is becoming important. Each automobile company is actively developing various new technologies to increase fuel efficiency. CVVD(Continuously Variable Valve Duration) system means a device that continuously changes the rotational speed of the camshaft to change the valve duration according to the state of the engine. In this paper, VVT(Variable Valve Timing) and CVVD were applied to a single-cylinder diesel engine, and the characteristics of intake and exhaust flow rate and in-cylinder pressure characteristics were analyzed by numerical analysis. In order to analyze the effect of CVVD on the actual engine operation, the study was performed by setting the valve control and injection pressure as variables in two sections of the engine operating region. As a result, In the case of applying CVVD, the positive overlap with the exhaust valve is maintained, thus it is possible to secure the flow smoothness of air and increase the volumetric efficiency by improving the flow rate. The section 2 condition showed the highest peak pressure, but the pressure rise rate was similar to that of the VVT 20 and CVCD 20 conditions up to 40 bar due to the occurrence of ignition delay.