• Title/Summary/Keyword: High Pressure Combustion Performance

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A Study on the Reduction of NO Emission from a Diesel Engine with 2-Stage Type Combustion Chamber (2단 연소형 연소실을 갖는 디젤기관의 NO 저감에 관한 연구)

  • 진선호;배종욱
    • Journal of Advanced Marine Engineering and Technology
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    • v.26 no.5
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    • pp.554-564
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    • 2002
  • A newly designed combustion chamber of diesel engine with a modified piston crown was prepared for the purpose of investigation for reduction of NO emission. It was intended to realize 2-stage combustion that is to keep fuel rich condition during early stage of combustion and fuel lean condition during next stage. The engine was tested on various conditions concerning exhaust gas emissions especially about NO emission and simultaneously fuel consumption rate. It was found that the engine with 2-stage combustion type piston emits significantly low NO at various speed and torque compared with conventional engines, but it raised points at issue in CO and smoke emissions with fuel consumption rate. The increasing of injection pressure on 2 stage combustion type diesel engine affects on CO and smoke emission considerably to reduce but slightly on NO to increase. The effect of 2-stage combustion was better at low speed than at high speed.

An Experimental Study on Diesel Spray Dynamics and Auto-Ignition Characteristics to use Rapid Comperssion Machine (RCM을 이용한 디젤 분무 거동 및 자발화 특성에 관한 실험적 연구)

  • Ahn, J.H.;Kim, H.M.;Shin, M.C.;Kim, S.W.
    • Journal of ILASS-Korea
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    • v.8 no.3
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    • pp.33-40
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    • 2003
  • The low-emission and high-performance diesel combustion is an important issue in the combustion research community, In order to understand the detailed diesel flame involving the complex physical processes, it is quite desirable to diesel spray dynamics, auto-ignition and spray flame propagation. Dynamics of fuel spray is a crucial element for air-fuel mixture formation, flame stabilization and pollutant formation, In the present study, the diesel RCM (Rapid Compression Machine) and the Electric Control injection system have been designed and developed to investigate the effects of injection pressure, injection timing, and intake air temperature on spray dynamics and diesel combustion processes, In terms of the macroscopic spray combustion characteristics, it is observed that the fuel jet atomization and the droplet breakup processes become much faster by increasing the injection pressure and the spray angle, With increasing the cylinder pressure, there is a tendency that the of spray pattern in the downstream region tends to be spherical due to the increase of air density and the corresponding drag force, Effects of intake temperature and injection pressure on auto-ignition is experimently analysed and discussed in detail.

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An Experimental Study on Diesel Spray Dynamics and Auto-Ignition Characteristics in the Rapid Compression Machine (RCM을 이용한 디젤 분무거동 및 자발화 특성에 관한 연구)

  • Kang, P.J.;Kim, H.M.;Kim, Y.M.;Kim, S.W.
    • Proceedings of the KSME Conference
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    • 2000.04b
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    • pp.447-452
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    • 2000
  • The low-emission and high-performance diesel combustion is an important issue in the combustion research community. In order to understand the detailed diesel flame field involving the complex Physical Processes, It Is quite desirable to study diesel spray dynamics, auto-ignition and spray flame propagation. Dynamics of fuel spray is a crucial element for air-fuel mixture formation flame stabilization and pollutant formation. In the present study, the diesel RCM (Rapid Compression Machine) and the Electric Control injection system have been designed and developed to investigate the effects of injection Pressure, injection timing, and intake air temperature on spray dynamics and diesel combustion processes. In terms of the macroscopic spray combustion characteristics it is observed that the fuel jet atomization and the droplet breakup processes become much faster by increasing the injection pressure and the spray angle. With increasing the cylinder pressure there is a tendency that the shape of spray pattern in the downstream region tends to be spherical due to the increase of air density and the corresponding drag force. Effects of intake temperature and injection pressure on auto-ignition is experimently analysed and discussed in detail.

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The Design and Hot-firing tests of a Water-cooled High Pressure Sub-scale Combustor (물냉각 고압 축소형 연소기의 설계 및 연소시험)

  • Lee, Kwang-Jin;Kim, Jong-Gyu;Lim, Byoung-Jik;Ahn, Kyu-Bok;Seo, Seong-Hyeon;Han, Yeoung-Min;Choi, Hwan-Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.3
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    • pp.1-6
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    • 2007
  • A 3-tonf-class high pressure sub-scale combustor was designed and manufactured to study the performance improvement of combustor. The combustor consists of a combustion chamber with film cooling, thermal barrier coating and water cooling channels to prevent thermal demage of the hardware and an injector head with 37 coaxial swirl injectors. Hot-firing tests were carried out at the design point with varying flow rate for film cooling. The test result revealed that the increase of film cooling flow rate decreases the combustion performance, but in the cases of similar film cooling flow rates, the combustion performance is dependent on the mixture ratio of main injector excluding the film cooling flow rate.

Discussions on the Combustion Dynamics of RDE with Relevance to the Liquid Rocket Combustion Instability (RDE의 연소동역학 및 액체 로켓 연소 불안정과 연관성에 대한 고찰)

  • Choi, Jeong-Yeol
    • 한국연소학회:학술대회논문집
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    • 2012.11a
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    • pp.363-366
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    • 2012
  • Detonative combustion is considered as a promising combustion mechanism for improving thermodynamic efficiency of power generation systems as a PGC, as well as high-speed propulsion systems. Among the various types of detonative combustion, RDE is fascinated by many researchers because of the simplicity and continuos operation characteristics. Present paper is an introduction to the physical and operational concept of RDE with a brief history of RDE researches and recent development activities. Additional discussions will devoted to the relevance to the tangential mode instabilities in liquid rocket engines and improvement of liquid rocket performance.

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A Study on the Effects of EGR on Engine Performance and Emissions of a HCCI(Homogeneous Charge Compression Ignition) Engine (HCCI 엔진에서 엔진성능 및 배출에 미치는 EGR의 영향)

  • Han, Sung-Bin;Chang, Yong-Hoon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.27 no.11
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    • pp.1630-1636
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    • 2003
  • Automobile companies and research institutions in leading automobile-manufacturing nations have recently been very active with research regarding the HCCI engine for use in future vehicles. Because HCCI engines take advantage of high compression ratio and heat release rate, they exhibit high efficiency found in compression ignition engines. HCCI engines also utilize a lean air/fuel ratio resulting in low emissions of NO$_{x}$ and PM (particulate matter). The objective of this research is to determine the effects of EGR rate on the combustion processes of HCCI. for this purpose, a 4-cylinder, compression ignition engine was converted into a HCCI engine, and a heating device was installed to raise the temperature of the intake air and also to make it more consistent. In addition, a pressure sensor was inserted into each of the cylinders to investigate the differences in characteristics among the cylinders. The experimental study of the effects of EGR rate on various gas emissions, engine performance, etc. should prove to be a valuable source of information for the development of the HCCI engine.e.

A Parametric Study on Combustion Stability Characteristics of Fuel-rich Gas Generators (설계 인자에 따른 연료 과농 가스발생기의 연소 안정성 특성 연구)

  • Ahn Kyu-Bok;Moon Il-Yoon;Seo Seong-Hyeon;Han Yeoung-Min;Choi Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.171-176
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    • 2006
  • An experimental study on a fuel-rich gas generator was carried out. Thirty seven double-swirl injectors with recess number of 1.5 were distributed and installed in the injector head, which significantly influences the combustion performance. In the paper, the characteristics of combustion stability are inspected by the parametric varations such as changing length and diameter of a combustion chamber and installing a turbulence ring. The experimental results show that as a resonant frequency took place in a high region, the amplitude of the dynamic pressure generally diminished, however, the combustion instability could not be suppressed perfectly.

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An Experimental Study on Che Spray Characteristic of Pintle Type Nozzle in a High Temperature and High Pressure Chamber (고온.고압용기 내에서 핀틀노즐의 분무특성에 관한 실험적 연구)

  • 송규근;정재연;정병국;안병규;오은탁
    • Journal of Advanced Marine Engineering and Technology
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    • v.27 no.1
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    • pp.57-64
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    • 2003
  • The characteristics of fuel spray have an important effect on engine performance such as power, specific fuel consumption and emission because fuel spray controls the mixing and combustion process in an engine. Therefore, if the characteristics of fuel spray can be measured, they can be effectively used for improving engine performance. The major factors controlling fuel spray are injection pressure, ambient pressure and engine speed. In this study, the experiment is performed in a high temperature and high pressure chamber. In experiments, spray tip penetration, spray angle and spray tip velocity are measured at various injection pressure (10 and 14 MPa), ambient pressure(3,4 and 5 MPa), fuel pump speed(500, 700 and 900 rpm). Experimental results are useful for deriving an experimental spray equation and design an optimal engine. The results showed that injection pressure, ambient pressure and fuel pump speed are important factors influencing on the characteristics of spray. 1) Injection pressure influences on the characteristics of spray. That is, as injection pressure is increased, spray angle is decreased but spray penetration and spray tip velocity is increased. 2) Spray angle and spray penetration are increased as fuel pump speed is increased.

An Investigation on Operating Characteristics of the Closed Cycle System Using High Pressure Diesel Engine (고압 디젤엔진을 이용한 폐회로 시스템의 운전특성에 관한 고찰)

  • 김인교;박신배
    • Transactions of the Korean Society of Automotive Engineers
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    • v.10 no.5
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    • pp.65-72
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    • 2002
  • The closed cycle diesel system is operated in closed circuit system where there is non air breathing with working fluid consists of combination of oxygen, argon and recycled exhaust gas far obtaining underwater or underground power sources. Experimental apparatus using the MTU8V183SE92 high pressurized engine adapted for closed cycle running, capable of operating at the system pressure of maximum 5 bar is constructed with ACAP as data acquisition system in order to operate equally in the open cycle in surface or the closed cycle in submerged conditions. The general features and the characteristics of combustion of HP(high pressure) diesel engine, specially designed and manufactured only for CCDE, are investigated. The test results of performance of HP diesel engine in closed cycle system are presented with respect to power and boost pressure and compared with those of low pressure diesel engine. The oxygen concentration and specific heat ratio are investigated with its deviation

An Experimental Study on Low Nox Combustor Performance at High Pressure and Temperature for 20kW Class Microturbines (20kW급 마이크로터빈용 저공해 연소기의 고압고온 성능실험 연구)

  • Yoon, JeongJung;Oh, Jongsik;Lee, Heonseok
    • 유체기계공업학회:학술대회논문집
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    • 2002.12a
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    • pp.183-190
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    • 2002
  • In order to reduce NOx emissions in the 20kw class microturbines under development, the low NOx characteristics, as being an application to the lean premixed combustion technology, have been investigated. The study has been conducted at the conditions of high temperature and pressure. Air from a compressor with the temperature of 500K to 650K and the pressure of 0.3bar gauge to 0.7bar gauge, was supplied to the combustor through an air preheat-treatment. Sampling exhaust gases were measured at the immediate exit of the combustor. for the effect of temperature on NO and CO emissions. though NOx was increased, CO was decreased with increasing inlet air temperature. With increasing inlet air pressure, NOx and CO were increased also. NOx was decreased, but CO was increased with increasing inlet air mass flow rate. The test has been performed on the equivalent ratios of 0.10 to 0.25 in a lean region. NOx was increased with increasing equivalent ratios, but CO was decreased as an influence of flame temperature. In the very lean region of the equivalent ratio below 0.12, CO was increased suddenly, due to instability. As the results of this study, NOx and CO are found to be reduced to the similar level at the same time when operated at optimal conditions.

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