Design and Development of Intake Pulse Resonance Chamber for Four Stroke Engine
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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. -
Not for Reproduction
use back code C BRIGGS & STRATTON CORPORATION 1 2 16 3 718 46 615 Illustrated Parts List 404 VERTICAL CRANKSHAFT SHORT BLOCK ASSEMBLIES 616 792738, 792739, 792740, 792741, 792742, 792743 22 51 For use on Engine Model Series 120K00, 121K00, 122K00, 122L00, 146 163 9 123J00, 123K00, 124K00, 124L00, 741 125K00,126L00, 127H00, 128H00, 617 128L00, 129H00 7 668 842 INSTRUCTIONS 883 To obtain the correct part numbers for an engine 869 45 40 4 which has been rebuilt with a Short Block Assem- 870 36 524 bly, follow these instructions: 871 868 45 684 12 A. For all parts shown in the illustrated view to the 40 28 33 left, use this Parts List. 35 584 B. For all other parts, refer to the Illustrated Parts 34 List which is appropriate for your engine by 27 Model, Type and Code (Serial) Number. 585 TO INSTALLER: GIVE THIS PARTS LIST TO 25 27 CUSTOMER AFTER SHORT BLOCK INSTALLATION. 43 51A 15 20 THIS IPL IS SPECIFIC TO THE SHORT 29 BLOCK(S) LISTED. RETAIN FOR FUTURE PARTS REFERENCE. 26 32 32A REF. PART REF. PART REF. PART NO. NO. DESCRIPTION NO. NO. DESCRIPTION NO. NO. DESCRIPTION 1 697322 Cylinder Assembly 25 797302 Piston Assembly 524 692296 Seal−Dipstick Tube 2 399269 Kit−Bushing/Seal (Mag- (Standard) 585 691879 Gasket−Breather Passage neto Side) for 797303 Piston Assembly 615 690340 Retainer−Governor Shaft 3 299819s Seal−Oil (.020” Oversize) 616 698801 Crank−Governor (Magneto Side) 26 797304 Ring Set (Standard) 617 270344s Seal−O Ring 4 493279 Sump−Engine 797305 Ring Set (Intake Manifold) −−−−−−− Note −−−−− (.020” Oversize) 668 493823 Spacer 696294 -
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 ........................................................................................................... -
Flow Through a Throttle Body a Comparative Study of Heat Transfer, Wall Surface Roughness and Discharge Coefficient
Flow Through a Throttle Body A Comparative Study of Heat Transfer, Wall Surface Roughness and Discharge Coefficient LIU-IEI-TEK-A–07/0071-SE Per Carlsson, Linköping February 23, 2007 Copyright The publishers will keep this document online on the Internet – or its possible replace- ment – for a period of 25 years starting from the date of publication barring exceptional circumstances. The online availability of the document implies permanent permission for anyone to read, to download, or to print out single copies for his/her own use and to use it unchanged for non-commercial research and educational purposes. Subsequent transfers of copyright cannot revoke this permission. All other uses of the document are conditional upon the consent of the copyright owner. The publisher has taken technical and administrative measures to assure authenticity, security and accessibility. Accord- ing to intellectual property law, the author has the right to be mentioned when his/her work is accessed as described above and to be protected against infringement. For additional information about Linköping University Electronic Press and its procedures for publication and for assurance of document integrity, please refer to its www home page: http://www.ep.liu.se/. c 2007 Per Carlsson. Abstract When designing a new fuel management system for a spark ignition engine the amount of air that is fed to the cylinders is highly important. A tool that is being used to improve the performance and reduce emission levels is engine modeling were a fuel management system can be tested and designed in a computer environment thus saving valuable setup time in an engine test cell. -
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. -
Banks Ram-Air® Intake System
Banks Ram-Air® Intake System 1997-2006 Jeep 4.0L THIS MANUAL IS FOR USE WITH KITS 41816 Gale Banks Engineering 546 Duggan Avenue • Azusa, CA 91702 (626) 969-9600 • Fax (626) 334-1743 Product Information & Sales: (888) 635-4565 bankspower.com ©2009 Gale Banks Engineering 02/17/09 PN 96575 v.3.0 General Installation Practices 5. Route and tie wires and hoses Dear Customer, a minimum of 6 inches away from If you have any questions exhaust heat, moving parts and sharp concerning the installation of edges. Clearance of 8 inches or more your Banks Ram-Air System, is recommended where possible. please call our Technical Service 6. During installation, keep the Hotline at (888) 839-2700 work area clean. If foreign debris between 7:00 am and 5:00 pm is transferred to any Banks system (PT). If you have any questions component, clean it thoroughly before relating to shipping or billing, installing. please contact our Customer Service Department at 7. When raising the vehicle, support (888) 839-5600. it on properly weight-rated safety stands, ramps or a commercial hoist. Thank you.1 Follow the manufacturer’s safety precautions. Take care to balance the vehicle to prevent it from slipping or 1. For ease of installation of your falling. When using ramps, be sure the Banks Ram-air intake system, front wheels are centered squarely on familiarize yourself with the procedure the topsides; put the transmission in by reading the entire manual before park; set the parking brake; and place starting work. This manual contains blocks behind the rear wheels. -
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. -
3.4L (DOHC) Engine Mechanical Specifications
60DegreeV6.com 3.4L (DOHC) Engine Mechanical Specifications Millimeters Inches Application General Data Engine Type -- 60° V-6 Displacement -- 240 Cu In Liter (VIN) -- 3.4 (X) RPO -- LQ1 Bore 92 3.622 Stroke 84 3.307 Deck Height 224 8.818 Compression Ratio -- 9.50:1 Firing Order -- 1-2-3-4-5-6 Oil Pressure @ Operating 103 kPa @ 1100 RPM 15 psi min @ 1100 RPM Temperature Cylinder Bore Diameter 92.020-92.038 3.6228-3.6235 Out Of Round Maximum 0.010 0.0004 Taper -- Thrust Side Maximum 0.013 0.00051 Center Distance 111.76 4.4 Piston Diameter-gauged at skirt 91.985-92.000 3.6215-3.6220 10.44 mm (0.413 in) below centerline of piston pin bore Clearance 0.020-0.052 0.0008-0.0020 Pin Bore 23.003-23.010 0.9056-0.9059 Piston Ring Compression Groove 0.033-0.079 0.0013-0.0031 Clearance 1st and 2nd Gap (at gauge diameter) 1st 0.20-0.45 0.008-0.018 1 60DegreeV6.com Gap (at gauge diameter) 2nd 0.56-0.81 0.022-0.032 Oil Groove Clearance 0.028-0.206 0.0011-0.0081 Gap (segment at gauge 0.25-0.76 0.0098-0.0299 diameter) Tension 1st 27.6 N 6.2 lbs Tension 2nd 19.8 N 4.5 lbs Tension Oil 31.2 N 7.0 lbs Piston Pin Diameter 22.9915-22.9964 0.9052-0.9054 Clearance 0.0066-0.0185 0.00026-0.00073 Fit In Rod 0.0165-0.0464 0.0006-0.0018 Crankshaft Main Journal Diameter-All 67.239-67.257 2.6472-2.6479 Taper-Maximum 0.005 0.0002 Out Of Round-Maximum 0.005 0.0002 Cylinder Block Main Bearing 72.155-72.168 2.8407-2.8412 Bore Diameter Crankshaft Main Bearing Inner 67.289-67.316 2.6492-2.6502 Diameter Main Bearing Clearance 0.019-0.064 0.0008-0.0025 Main Thrust Bearing Clearance -
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.