Combustion Chambers in CI Engines: a Review
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Engine Components and Filters: Damage Profiles, Probable Causes and Prevention
ENGINE COMPONENTS AND FILTERS: DAMAGE PROFILES, PROBABLE CAUSES AND PREVENTION Technical Information AFTERMARKET Contents 1 Introduction 5 2 General topics 6 2.1 Engine wear caused by contamination 6 2.2 Fuel flooding 8 2.3 Hydraulic lock 10 2.4 Increased oil consumption 12 3 Top of the piston and piston ring belt 14 3.1 Hole burned through the top of the piston in gasoline and diesel engines 14 3.2 Melting at the top of the piston and the top land of a gasoline engine 16 3.3 Melting at the top of the piston and the top land of a diesel engine 18 3.4 Broken piston ring lands 20 3.5 Valve impacts at the top of the piston and piston hammering at the cylinder head 22 3.6 Cracks in the top of the piston 24 4 Piston skirt 26 4.1 Piston seizure on the thrust and opposite side (piston skirt area only) 26 4.2 Piston seizure on one side of the piston skirt 27 4.3 Diagonal piston seizure next to the pin bore 28 4.4 Asymmetrical wear pattern on the piston skirt 30 4.5 Piston seizure in the lower piston skirt area only 31 4.6 Heavy wear at the piston skirt with a rough, matte surface 32 4.7 Wear marks on one side of the piston skirt 33 5 Support – piston pin bushing 34 5.1 Seizure in the pin bore 34 5.2 Cratered piston wall in the pin boss area 35 6 Piston rings 36 6.1 Piston rings with burn marks and seizure marks on the 36 piston skirt 6.2 Damage to the ring belt due to fractured piston rings 37 6.3 Heavy wear of the piston ring grooves and piston rings 38 6.4 Heavy radial wear of the piston rings 39 7 Cylinder liners 40 7.1 Pitting on the outer -
Small Engine Parts and Operation
1 Small Engine Parts and Operation INTRODUCTION The small engines used in lawn mowers, garden tractors, chain saws, and other such machines are called internal combustion engines. In an internal combustion engine, fuel is burned inside the engine to produce power. The internal combustion engine produces mechanical energy directly by burning fuel. In contrast, in an external combustion engine, fuel is burned outside the engine. A steam engine and boiler is an example of an external combustion engine. The boiler burns fuel to produce steam, and the steam is used to power the engine. An external combustion engine, therefore, gets its power indirectly from a burning fuel. In this course, you’ll only be learning about small internal combustion engines. A “small engine” is generally defined as an engine that pro- duces less than 25 horsepower. In this study unit, we’ll look at the parts of a small gasoline engine and learn how these parts contribute to overall engine operation. A small engine is a lot simpler in design and function than the larger automobile engine. However, there are still a number of parts and systems that you must know about in order to understand how a small engine works. The most important things to remember are the four stages of engine operation. Memorize these four stages well, and everything else we talk about will fall right into place. Therefore, because the four stages of operation are so important, we’ll start our discussion with a quick review of them. We’ll also talk about the parts of an engine and how they fit into the four stages of operation. -
RECIPROCATING ENGINES Franck Nicolleau
RECIPROCATING ENGINES Franck Nicolleau To cite this version: Franck Nicolleau. RECIPROCATING ENGINES. Master. RECIPROCATING ENGINES, Sheffield, United Kingdom. 2010, pp.189. cel-01548212 HAL Id: cel-01548212 https://hal.archives-ouvertes.fr/cel-01548212 Submitted on 27 Jun 2017 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Distributed under a Creative Commons Attribution - NonCommercial| 4.0 International License Mechanical Engineering - 14 May 2010 -1- UNIVERSITY OF SHEFFIELD Department of Mechanical Engineering Mappin street, Sheffield, S1 3JD, England RECIPROCATING ENGINES Autumn Semester 2010 MEC403 - MEng, semester 7 - MEC6403 - MSc(Res) Dr. F. C. G. A. Nicolleau MD54 Telephone: +44 (0)114 22 27700. Direct Line: +44 (0)114 22 27867 Fax: +44 (0)114 22 27890 email: F.Nicolleau@sheffield.ac.uk http://www.shef.ac.uk/mecheng/mecheng cms/staff/fcgan/ MEng 4th year Course Tutor : Pr N. Qin European and Year Abroad Tutor : C. Pinna MSc(Res) and MPhil Course Director : F. C. G. A. Nicolleau c 2010 F C G A Nicolleau, The University of Sheffield -2- Combustion engines Table of content -3- Table of content Table of content 3 Nomenclature 9 Introduction 13 Acknowledgement 16 I - Introduction and Fundamentals of combustion 17 1 Introduction to combustion engines 19 1.1 Pistonengines.................................. -
Study of Spark Ignition Engine Combustion Model for the Analysis of Cyclic Variation and Combustion Stability at Lean Operating Conditions
Michigan Technological University Digital Commons @ Michigan Tech Dissertations, Master's Theses and Master's Dissertations, Master's Theses and Master's Reports - Open Reports 2013 STUDY OF SPARK IGNITION ENGINE COMBUSTION MODEL FOR THE ANALYSIS OF CYCLIC VARIATION AND COMBUSTION STABILITY AT LEAN OPERATING CONDITIONS Hao Wu Michigan Technological University Follow this and additional works at: https://digitalcommons.mtu.edu/etds Copyright 2013 Hao Wu Recommended Citation Wu, Hao, "STUDY OF SPARK IGNITION ENGINE COMBUSTION MODEL FOR THE ANALYSIS OF CYCLIC VARIATION AND COMBUSTION STABILITY AT LEAN OPERATING CONDITIONS", Master's report, Michigan Technological University, 2013. https://doi.org/10.37099/mtu.dc.etds/662 Follow this and additional works at: https://digitalcommons.mtu.edu/etds STUDY OF SPARK IGNITION ENGINE COMBUSTION MODEL FOR THE ANALYSIS OF CYCLIC VARIATION AND COMBUSTION STABILITY AT LEAN OPERATING CONDITIONS By Hao Wu A REPORT Submitted in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE In Mechanical Engineering MICHIGAN TECHNOLOGICAL UNIVERSITY 2013 © 2013 Hao Wu This report has been approved in partial fulfillment of the requirements for the Degree of MASTER OF SCIENCE in Mechanical Engineering. Department of Mechanical Engineering-Engineering Mechanics Report Advisor: Dr. Bo Chen Committee Member: Dr. Jeffrey D. Naber Committee Member: Dr. Chaoli Wang Department Chair: Dr. William W. Predebon CONTENTS LIST OF FIGURES ........................................................................................................... -
US5136990.Pdf
|||||||||||||| USOO5136990A United States Patent (19) 11) Patent Number: 5,136,990 Motoyama et al. 45) Date of Patent: Aug. 11, 1992 54 FUEL INJECTION SYSTEM INCLUDING 4,779,581 10/1988 Maier ................................ 123A73. A SUPPLEMENTAL FUEL NJECTOR Primary Examiner-Andrew M. Dolinar 75 Inventors: Yu Motoyama; Toshikazu Ozawa; Assistant Examiner-M. Macy Junichi Kaku, all of Iwata, Japan Attorney, Agent, or Firm-Ernest A. Beutler 73 Assignee: Yamaha Hatsudoki Kabushiki Kaisha, 57 ABSTRACT Iwata, Japan A fuel injection system for a two cycle crankcase com 21 Appl. No.: 591,957 pression internal combustion engine including a first injector that supplies fuel directly to the combustion 22 Filed: Oct. 2, 1990 chamber of the engine. An induction system is provided (30) Foreign Application Priority Data for inducting air into the crankcase chamber of the Oct. 2, 1989 JP Japan .................................. 1-257459 engine and in a multiple cylinder engine this includes a manifold having a single inlet. A throttle body having a 51 Int. Cl.............................. 12373 A; FO2B33/04 throttle valve controls the flow of air through the inlet 52 U.S. C. ................................................... 123/73 C and a second fuel injector sprays fuel into the throttle 58 Field of Search ............. 123/73 A, 73 AD, 73 C, body upstream of the throttle valve and against the 123/73 R, 73 B, 304 throttle valve in certain positions of the throttle valve. 56) References Cited In accordance with one disclosed embodiment of the invention, the second fuel injector supplies the fuel U.S. PATENT DOCUMENTS requirements for maximum power while the first fuel 4,446,833 5/1984. -
Design and Assembly of a Throttle for an HCCI Engine
Design and assembly of a throttle for an HCCI engine ÀLEX POYO MUÑOZ Master of Science Thesis Stockholm, Sweden 2009 Design and assembly of a throttle for an HCCI engine Àlex Poyo Muñoz Master of Science Thesis MMK 2009:63 MFM129 KTH Industrial Engineering and Management Machine Design SE-100 44 STOCKHOLM Examensarbete MMK 2009:63 MFM129 Konstruktion och montering av ett gasspjäll för en HCCI-motor. Àlex Poyo Muñoz Godkänt Examinator Handledare 2009-Sept-18 Hans-Erik Ångström Hans-Erik Ångström Uppdragsgivare Kontaktperson KTH Hans-Erik Ångström Sammanfattning Denna rapport handlar om införandet av ett gasspjäll i den HCCI motor som utvecklas på Kungliga Tekniska Högskolan (KTH) i Stockholm. Detta gasspjäll styr effekten och arbetssättet i motorn. Med en gasspjäll är det möjligt att byta från gnistantändning till HCCI-läge. Under projektet har många andra områden förbättrats, till exempel luft- och oljepump. För att dra slutsatser är det nödvändigt att analysera några av motorns data som insamlats under utvecklingen, såsom cylindertryck, insprutningsdata och tändläge. Man analyserade data under olika tidpunkter av motorns utveckling, med olika komponenter, för att uppnå olika prestanda i varje enskilt fall. För att köra motorn i HCCI-läge är det nödvändigt att ha ett lambda-värde mellan 1,5 och 2. Även om resultaten visar att det är bättre att köra i "Pump + Throttle + Intake" kommer pumpen överbelastas på grund av ett extra tryckfall. Av detta skäl kommer är det nödvändigt att arbeta i "Throttle + Pump + Intake" i framtiden. Eftersom det är nödvändigt att minska insprutningstiden, av detta skäl, är det också viktigt att öka luftflödet. -
The Effects of Combustion Chamber Design On
THE EFFECTS OF COMBUSTION CHAMBER DESIGN ON TURBULENCE, CYCLIC VARIATION AND PERFORMANCE IN AN SI ENGINE By Esther Claire Tippett B.E.Mech (Hons) University of Canterbury, New Zealand. 1983 A THESIS SUBMITTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF APPLIED SCIENCE in THE FACULTY OF GRADUATE STUDIES DEPARTMENT OF MECHANICAL ENGINEERING We accept this thesis as conforming to the required standard THE UNIVERSITY OF BRITISH COLUMBIA August, 1989 © Esther Claire Tippett, 1989 In presenting this thesis in partial fulfilment of the requirements for an advanced degree at the University of British Columbia, I agree that the Library shall make it freely available for reference and study. I further agree that permission for extensive copying of this thesis for scholarly purposes may be granted by the head of my department or by his or her representatives. It is understood that copying or publication of this thesis for financial gain shall not be allowed without my written permission. Department of Mechanical Engineering The University of British Columbia Vancouver, Canada Date: ABSTRACT An experimental program of motored and fired tests has been undertaken on a single cylinder spark ignition engine to determine the influence of combustion chamber design on turbulence enhancement in the achievement of fast lean operation. Flow field measurements were taken using hot wire anemometry in the cylinder during motored operation. On line performance tests and in-cylinder pressure data were recorded for the operation of the engine by natural gas at lean and stoichiometric conditions over a range of speed and loads. Squish and squish jet action methods of turbulence enhancement were investigated for six configurations, using a standard bathtub cylinder head and new piston designs incorporating directed jets through a raised wall, a standard bowl-in-piston chamber and an original squish jet design piston. -
Spark Ignition and Pre-Chamber Turbulent Jet Ignition Combustion
Downloaded from SAE International by Brought To You Michigan State Univ, Thursday, April 02, 2015 Spark Ignition and Pre-Chamber Turbulent Jet 2012-01-0823 Published Ignition Combustion Visualization 04/16/2012 William P. Attard MAHLE Powertrain LLC Elisa Toulson, Andrew Huisjen, Xuefei Chen, Guoming Zhu and Harold Schock Michigan State University Copyright © 2012 SAE International doi:10.4271/2012-01-0823 ABSTRACT INTRODUCTION AND BACKGROUND Natural gas is a promising alternative fuel as it is affordable, available worldwide, has high knock resistance and low In recent years there has been renewed interest in lean burn carbon content. This study focuses on the combustion technologies, primarily due to the improvement in fuel visualization of spark ignition combustion in an optical single efficiency that these technologies can provide [1,2,3]. Lean cylinder engine using natural gas at several air to fuel ratios burn occurs when fuel is burnt in excess air and running an and speed-load operating points. In addition, Turbulent Jet engine in this manner has many advantages over conventional Ignition optical images are compared to the baseline spark stoichiometric combustion. One advantage of running lean ignition images at the world-wide mapping point (1500 rev/ occurs as the introduction of additional air increases the min, 3.3 bar IMEPn) in order to provide insight into the specific heat ratio, which leads to an increase in thermal relatively unknown phenomenon of Turbulent Jet Ignition efficiency. Additionally, lean engine operation reduces combustion. Turbulent Jet Ignition is an advanced spark pumping losses for a given road load by tending towards initiated pre-chamber combustion system for otherwise throttle-less operation, which can further improve drive-cycle standard spark ignition engines found in current passenger fuel economy. -
Gas Turbine Combustion Chamber (Source: ‘Gas Turbine Theory’, Cohen, Rogers)
Gas Turbine Combustion Chamber (Source: ‘Gas Turbine Theory’, Cohen, Rogers) Akash James Asst. Professor, Dept. of Mechanical Engineering, RSET Simple Open Cycle Gas Turbine Schematic Diagram AJ 2 Contents • Combustion Process • Types of Combustion Chambers • Performance Parameters • Pressure Loss • Combustion Efficiency • Stability Loop • Combustion Intensity AJ 3 Combustion Process Process → Combustion in the normal, open cycle, gas turbine is a continuous process in which fuel is burned in the air supplied by the compressor; an electric spark is required only for initiating the combustion process, and thereafter the flame must be self-sustaining. → Combustion of a liquid fuel involves the mixing of a fine spray of droplets with air, vaporization of the droplets, the breaking down of heavy hydrocarbons into lighter fractions, the intimate mixing of molecules of these hydrocarbons with oxygen molecules, and finally the chemical reactions themselves. → A high temperature, such as is provided by the combustion of an approximately stoichiometric mixture, is necessary if all these processes are to occur sufficiently rapidly for combustion in a moving air stream to be completed in a small space → But in actual practice A/F ratio is in the range of 100:1, while stoichiometric ratio is around 15:1. This is to reduce the turbine inlet temperatures due to practical limits. AJ 4 Factors influencing design → Low turbine inlet temperature → Uniform temperature distribution at turbine inlet (i.e., to avoid local over heating of turbine blades) → Stable operation even when factors like air velocity, A/F ratio & chamber pressure varies greatly, especially for aircraft engines (the limit is the ‘flame- out’ of the combustion chamber) & at the event of a flame-out the combustor should be able to relight quickly. -
The Basics of Four-Stroke Engines
Youth Explore Trades Skills Automotive Service Technician The Basics of Four-Stroke Engines Description Students will be introduced to basic engine parts, theory and terminology. Understanding how an engine works and knowing some key related parts and terminology is important for working on any vehicle. The information is broken down into three major sections: “Basic Engine Parts,” “Basic Engine Terminology” and “Basic Four-Stroke Cycle Engine Theory.“ Lesson Outcomes The student will be able to: • Identify and explain the function of basic engine parts • Identify and explain basic engine terminology • Identify the four piston strokes of a four-stroke cycle engine • Describe the action and function of each piston stroke Assumptions • The students will have little or no prior knowledge of how engines work, terminology or parts. • The teacher is familiar with the information being taught. Note: This information is given as a guide to the minimum amount of material to be covered for a basic understanding of the engine and how it works. Much more can be added as the instructor sees fit. Terminology Valve train: all the parts that are used to open and close valves. This may include parts such as valve springs, keepers, lifters, cam followers, shims, rockers and push rods. Any other terminology used will be explained as required during the activities. Estimated time 90–120 minutes (including a question and answer session) Recommended number of students 20, based on the BC Technology Educators’ Best Practice Guide Facilities A classroom, computer lab or workshop with tables and chairs sufficient for 20 students. This work is licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License unless otherwise indicated. -
Experimental Investigations on Modified Combustion Chamber Geometry in Diesel Engine
International Journal of Recent Technology and Engineering (IJRTE) ISSN: 2277-3878, Volume-7 Issue-5S2, January 2019 Experimental Investigations on Modified Combustion Chamber Geometry in Diesel Engine ShaikHussain, Sanam Ravi Teja Abstract: Today the two disturbing conditions in front of the basedengines is mostly due to the changes in the properties engineers worldwide are to decrease the utilization of of fuel, design of engine and operating parameter. The conventional fuels and to downscale the ever rising characteristics of p of the DI diesel engine are highly effects environmental pollution.The performance characteristics and by the motion of air in the inner side of the cylinder. The emission characteristics of single cylinder water cooled diesel mixing of air-fuel and the following combustion in the DI engine with the effect of piston crown geometries such as HCC (Hemispherical combustion chamber) and RCC (Re-entrant diesel engines are restrained by flow field inside the cylinder combustion chamber) are evaluated. The tests are conducted with happened by the combustion chamber specifications. The diesel and Rice Bran Methyl Ester and Diesel blends as fuels motion of air in the diesel engine, in the course of with different loading conditions. Rice bran methyl ester is compression stroke is causes by the combustion chamber. prepared by using transesterification process. Without modifying Hence, configurations of combustion chambers require a the compression ratio and cylindrical volume of the engine the great attention to contact the global movements in the baseline hemispherical type piston is replaced with Re-entrant consumption of fuel, performance and emissions. type piston. All the engine tests were conducted with diesel and In this stage of exploratory work, without changing the 20% blend with diesel [RBOME20] indiesel engine with HCC engine’s compression ratio, geometry of piston bowl was and RCC. -
Combustion System Development for the Next Generation Hd Gas Engines
COMBUSTION SYSTEM DEVELOPMENT FOR THE NEXT GENERATION HD GAS ENGINES REPORT 2018:477 Combustion System Development for the Next Generation HD Gas Engines COSTGAS LUDVIG ADLERCREUTZ ISBN 978-91-7673-477-3 | © Energiforsk March 2018 Energiforsk AB | Phone: 08-677 25 30 | E-mail: [email protected] | www.energiforsk.se COMBUSTION SYSTEM DEVELOPMENT FOR THE NEXT GENERATION HD GAS ENGINES Foreword COSTGAS is a project in Heavy Duty gas engines in which the combustion system for the next generation gas engines is to be developed. The goal of the project is to increase the efficiency of the current gas engine platform by 10% and increase the torque by 20%. This is done while observing the boundary conditions of the current Euro VI emissions regulations. The report has been produced by AVL Powertrain Scandinavia, Scania CV and the Royal Institute of Technology. The authors are Ludvig Adlercreutz (AVL). The author would like to acknowledge the Swedish Energy Agency, Energiforsk - Swedish Energy Research Center, for its financial contribution to the project within the scope of the program “Samverkansprogram Energigasteknik” – The cooperation research program Energy gas technology. This work was also made possible by financial support from AVL Powertrain Scandinavia. The authors thank research engineer Asko Kinnunen (AVL) and Petri Fransman (AVL) for help during experiments. Special thanks to Daniel Danielsson (AVL) for the assistance in setting up the experiments. Johan Fjällman is also acknowledged for his invaluable help in finalizing the report. The study had a working group with the following members: Thomas Åkerblom (Scania), Fredrik Königsson (AVL), Johannes Andersen (AVL), Jonas Modin (AVL), Andreas Cronhjort (KTH) and Mattias Svensson (Energiforsk).