The Influence of a Piston Ring Coating on the Wear and Friction Generated During Linear Oscillation

Total Page:16

File Type:pdf, Size:1020Kb

The Influence of a Piston Ring Coating on the Wear and Friction Generated During Linear Oscillation lubricants Article The Influence of a Piston Ring Coating on the Wear and Friction Generated during Linear Oscillation Arthur Rozario 1,*, Christoph Baumann 2 and Raj Shah 3,* 1 Electrical and Computer Engineering Department, Stony Brook University, Stony Brook, NY 11794, USA 2 Optimol Instruments Prüftechnik GmbH, Westendstraße 125, 80339 München, Germany; [email protected] 3 Koehler Instrument Company, Inc., 85 Corporate Drive, Holtsville, NY 11742, USA * Correspondence: [email protected] (A.R.); [email protected] (R.S.); Tel.: +1-631-589-3800 (R.S.) Received: 24 June 2018; Accepted: 10 January 2019; Published: 14 January 2019 Abstract: The piston group is responsible for contributing to ~50% of the frictional losses of an engine, which ultimately leads to the waste of fuel. This coupled with the fact that gasoline is a finite resource linked to CO2-emissions, there is an increased demand of higher performance vehicles, which coincidently further loads the piston ring. As of yet, there are plenty of studies that already study the piston ring’s contact with the cylinder liner. However, this study focuses on a cost-effective Schwing, Reib, Verschleiss (SRV) instrumentation that allows to pre-screen lubricants, additives, materials and coatings for their friction, wear and load carrying capacity including scuffing resistance. As a result of the pre-screening conducted outside of engine by using the SRV instrument, it brings us to the following conclusion: the PVD CrN-TiN 1o Group coating on the piston ring produces the least wear, as well as the lowest coefficient of friction. Moreover, it is concluded that a coating that is based from CrN and TiN allows the piston ring to perform better in engine settings. A continued understanding of the piston-cylinder-contact assembly only helps engineers, scientists and any other stakeholder to improve on the piston ring and cylinder liner interaction. Keywords: internal combustion engine; compression rings; viscosity 1. Introduction The purpose of piston rings (PR) is to provide a sealing between the gap of the piston and the cylinder wall, whilst distributing and controlling the oil and transferring the heat along with stabilizing the piston. This is a departure from earlier days, where the sole purpose of the PR was just to seal off the combustion chamber. The PR in the internal combustion engine (ICE) is accountable for a significant amount of friction loss and the optimization of this tribosystem is very important to increase the overall fuel economy of the engine [1]. For example, frictional losses of the piston-cylinder-contact (PCC, where the PR is in contact with the cylinder liner) in heavy duty diesel engines of trucks can contribute to the overall 4–15% of fuel consumption. As a result, billions of liters of fuel are lost to just overcoming the friction in these vehicles [2]. Significant studies have been conducted in this area, such as R. Rahmani et al. explaining that the internal combustion engine will continue as the main ‘source of vehicular propulsion for the foreseeable future.’ The authors present a study that takes an integrated approach to the frictional losses, as well as discuss the emission losses of the piston-cylinder system. The conclusions of this experiment state that the cylinder liner temperature is critical in mitigating power loss, in addition to reducing Hydrocarbon and Nitrogen oxide emissions from the compression ring [3]. It is important to note that the compression ring is located nearest to the piston head, which is the top of the piston [4]. Lubricants 2019, 7, 8; doi:10.3390/lubricants7010008 www.mdpi.com/journal/lubricants Lubricants 2019, 7, 8 2 of 9 Lubricants 2019, 7, x FOR PEER REVIEW 2 of 9 ThisThis paperpaper offersoffers aa novelnovel wayway toto investigateinvestigate thethe wearwear andand frictionfriction generatedgenerated byby thethe PRPR oscillatingoscillating againstagainst thethe cylinder cylinder liner liner using using the the SRV SRV tester. tester. This This is otherwise is otherwise known known as SRV, as SRV, which which translated translated from Germanfrom German means means oscillation, oscillation, friction friction and wear. andThe wear. SRV The instrument SRV instrument can be used can tobeclosely used to simulate closely specificsimulate operating specific operating conditions conditions relevant for relevant the functioning for the functioning of the PR inof thethe ICE.PR in the ICE. TheThe primaryprimary investigationinvestigation ofof thisthis paperpaper is:is: HowHow differentdifferent pistonpiston ringring coatingscoatings influenceinfluence thethe wearwear andand thethe frictionfriction generatedgenerated fromfrom thethe slidingsliding motionmotion ofof thethe PCC.PCC. ToTo thethe authors’authors’ knowledge,knowledge, therethere areare studiesstudies thatthat dodo considerconsider PRPR coatingscoatings andand thethe effecteffect ofof itit onon thethe PCCPCC assemblyassembly butbut itit isis thethe noveltynovelty ofof howhow thisthis investigationinvestigation waswas conductedconducted thatthat presentspresents aa realistic,realistic, cost-efficientcost-efficient wayway ofof studyingstudying thethe PCCPCC movement.movement. Ultimately, itit isis thethe goalgoal ofof suchsuch screeningscreening toto suggestsuggest possiblepossible coatingscoatings ofof thethe PRPR inin thethe PCCPCC assembly,assembly, so so thatthat thethe PRPR cancan bebe possiblypossibly furtherfurther optimized.optimized. By choosing this parameter of study, itit offersoffers aa viableviable wayway thethe PRPR cancan bebe advancedadvanced withoutwithout aa needneed forfor aa largelarge changechange inin thethe currentcurrent settingssettings ofof thethe PCCPCC assemblyassembly inin thethe engine,engine, makingmaking itit aa feasiblefeasible optionoption toto bebe consideredconsidered forfor moremore studies.studies. ThisThis approachapproach isis alsoalso suitedsuited forfor developmentdevelopment ofof alternativealternative andand lowlow viscosity viscosity engine engine oils. oils. 2.2. ModelingModeling thethe FrictionFriction ofof thethe Piston-Cylinder-ContactPiston-Cylinder-Contact duringduring EngineEngine OperationOperation ◦ DuringDuring operationoperation cyclecycle ofof 720720° inin thethe ICE,ICE, thethe PRPR passespasses allall lubricationlubrication modesmodes onon thethe cylindercylinder linerliner andand willwill generategenerate differentdifferent levelslevels ofof frictionfriction [5[5].]. PistonPiston coatingscoatings havehave thethe potentialpotential toto reducereduce frictionfriction and/orand/or wear of the piston’s sliding components [[6]6] but alsoalso toto preventprevent scuffing.scuffing. ToTo measuremeasure reductionreduction inin wearwear andand frictionfriction ofof thethe PCC,PCC, twotwo variablesvariables areare considered:considered: LossLoss ofof massmass ofof thethe PRPR andand coefficientcoefficient ofof frictionfriction (COF)(COF) of the PCC as a function of of time. time. The The following following explanations explanations provide provide a abasis basis of of why why both both these these parameters parameters are are valid valid to to observe. observe. FigureFigure1 illustrates1 illustrates the the surface surface of contact of contact between between the PR the and PR the and cylinder the cylinder liner. Over liner. the distance:Over the Dx = x − x the PCC can be assumed to experience mixed friction, due to the combination of pure distance:2 Δx1 = x2 − x1 the PCC can be assumed to experience mixed friction, due to the combination of hydrodynamicpure hydrodynamic lubrication lubrication points points (where (where sufficient sufficient amount amount of lubricant of lubricant exists exists to separate to separate the two the surfacestwo surfaces in contact) in contact) and and pure pure boundary boundary friction friction points points (where (where there there is is an an insufficient insufficient amount amount ofof lubricantlubricant betweenbetween thethe twotwo surfacessurfaces inin contact)contact) [ [7].7]. FigureFigure 1.1. PistonPiston ringring (PR)(PR) andand CylinderCylinder LinerLiner Contact.Contact. Furthermore,Furthermore, scuffingscuffing failure failure can can bebe categorizedcategorized asas catastrophiccatastrophic failurefailurecoupled coupled withwith severesevere formform ofof wearwear byby substantial substantial material material transfer, transfer, which which can can occur occur during during the the PCC PCC operation operation [8]. [8]. The The location location in whichin which the oilthe film oil isfilm penetrated is penetrated is where is thewhere sliding the on sliding the PR on of thethe cylinderPR of the will cylinder cause deformation will cause anddeformation therefore and wear therefore [9]. wear [9]. ToTo extrapolateextrapolate fromfrom thesethese foundationalfoundational ideas,ideas, whenwhen therethere isis aa penetrationpenetration ofof thethe oiloil film,film, thethe PRPR willwill slide slide over over the the cylinder cylinder liner liner without without sufficient sufficient lubrication lubrication between between the two the surfaces. two surfaces. This will This cause will cause deformation and wear. Additionally, the metal to metal contact and the subsequent sliding of it leads to increased friction [10]. This potentially increases the COF leads to higher fuel consumption Lubricants 2019, 7, 8 3 of 9 Lubricantsdeformation 2019, and7, x FOR wear. PEER Additionally, REVIEW the metal to metal contact and the subsequent sliding
Recommended publications
  • 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
    [Show full text]
  • 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.
    [Show full text]
  • Poppet Valve
    POPPET VALVE A poppet valve is a valve consisting of a hole, usually round or oval, and a tapered plug, usually a disk shape on the end of a shaft also called a valve stem. The shaft guides the plug portion by sliding through a valve guide. In most applications a pressure differential helps to seal the valve and in some applications also open it. Other types Presta and Schrader valves used on tires are examples of poppet valves. The Presta valve has no spring and relies on a pressure differential for opening and closing while being inflated. Uses Poppet valves are used in most piston engines to open and close the intake and exhaust ports. Poppet valves are also used in many industrial process from controlling the flow of rocket fuel to controlling the flow of milk[[1]]. The poppet valve was also used in a limited fashion in steam engines, particularly steam locomotives. Most steam locomotives used slide valves or piston valves, but these designs, although mechanically simpler and very rugged, were significantly less efficient than the poppet valve. A number of designs of locomotive poppet valve system were tried, the most popular being the Italian Caprotti valve gear[[2]], the British Caprotti valve gear[[3]] (an improvement of the Italian one), the German Lentz rotary-cam valve gear, and two American versions by Franklin, their oscillating-cam valve gear and rotary-cam valve gear. They were used with some success, but they were less ruggedly reliable than traditional valve gear and did not see widespread adoption. In internal combustion engine poppet valve The valve is usually a flat disk of metal with a long rod known as the valve stem out one end.
    [Show full text]
  • History of a Forgotten Engine Alex Cannella, News Editor
    POWER PLAY History of a Forgotten Engine Alex Cannella, News Editor In 2017, there’s more variety to be found un- der the hood of a car than ever. Electric, hybrid and internal combustion engines all sit next to a range of trans- mission types, creating an ever-increasingly complex evolu- tionary web of technology choices for what we put into our automobiles. But every evolutionary tree has a few dead end branches that ended up never going anywhere. One such branch has an interesting and somewhat storied history, but it’s a history that’s been largely forgotten outside of columns describing quirky engineering marvels like this one. The sleeve-valve engine was an invention that came at the turn of the 20th century and saw scattered use between its inception and World War II. But afterwards, it fell into obscurity, outpaced (By Andy Dingley (scanner) - Scan from The Autocar (Ninth edition, circa 1919) Autocar Handbook, London: Iliffe & Sons., pp. p. 38,fig. 21, Public Domain, by the poppet valves we use in engines today that, ironically, https://commons.wikimedia.org/w/index.php?curid=8771152) it was initially developed to replace. Back when the sleeve-valve engine was first developed, through the economic downturn, and by the time the econ- the poppet valves in internal combustion engines were ex- omy was looking up again, poppet valve engines had caught tremely noisy contraptions, a concern that likely sounds fa- up to the sleeve-valve and were quickly becoming just as miliar to anyone in the automotive industry today. Charles quiet and efficient.
    [Show full text]
  • High Pressure Ratio Intercooled Turboprop Study
    E AMEICA SOCIEY O MECAICA EGIEES 92-GT-405 4 E. 4 S., ew Yok, .Y. 00 h St hll nt b rpnbl fr ttnt r pnn dvnd In ppr r n d n t tn f th St r f t vn r Stn, r prntd In t pbltn. n rnt nl f th ppr pblhd n n ASME rnl. pr r vlbl fr ASME fr fftn nth ftr th tn. rntd n USA Copyright © 1992 by ASME ig essue aio Iecooe uoo Suy C. OGES Downloaded from http://asmedigitalcollection.asme.org/GT/proceedings-pdf/GT1992/78941/V002T02A028/2401669/v002t02a028-92-gt-405.pdf by guest on 23 September 2021 Sundstrand Power Systems San Diego, CA ASAC NOMENCLATURE High altitude long endurance unmanned aircraft impose KFT Altitude Thousands Feet unique contraints on candidate engine propulsion systems and HP Horsepower types. Piston, rotary and gas turbine engines have been proposed for such special applications. Of prime importance is the HIPIT High Pressure Intercooled Turbine requirement for maximum thermal efficiency (minimum specific Mn Flight Mach Number fuel consumption) with minimum waste heat rejection. Engine weight, although secondary to fuel economy, must be evaluated Mls Inducer Mach Number when comparing various engine candidates. Weight can be Specific Speed (Dimensionless) minimized by either high degrees of turbocharging with the Ns piston and rotary engines, or by the high power density Exponent capabilities of the gas turbine. pps Airflow The design characteristics and features of a conceptual high SFC Specific Fuel Consumption pressure ratio intercooled turboprop are discussed. The intended application would be for long endurance aircraft flying TIT Turbine Inlet Temperature °F at an altitude of 60,000 ft.(18,300 m).
    [Show full text]
  • UNIVERSAL-- AMERICAN LEADER in MARINE POWER Slnce 1898
    MANUAL NO. 1-89 ---UNIVERSAL-- AMERICAN LEADER IN MARINE POWER SlNCE 1898 SERVICE MANUAL MODELS M-12 M2-t2 M3-20 M4-30 M-18 M-25 M-25XP M-35 -------[IDID]]~o~I----- MANUAL NO. 1-89 ---UNIVERSAL-- AMERICAN LEADER IN MARINE POWER SlNCE 1898 SERVICE MANUAL MODELS M-12 M2-t2 M3-20 M4-30 M-18 M-25 M-25XP M-35 -------[IDID]]~o~I----- CONTENTS NOTE: Refer to the beginning of the individual sections for a complete table of contents for that section. SECTION I - SPECIFICATIONS .................................................... 1-38 SECTION II - PREVENTIVE MAINTENANCE ........................................ 39-44 SECTION III - CONSTRUCTION AND FUNCTION .................................... 45-50 SECTION IV - LUBRICATION, COOLING, AND FUEL SYSTEMS ....................... 51-69 SECTION V - ELECTRICAL SYSTEM ............................................. 71-102 SECTION VI - DISASSEMBLY AND REASSEMBLy ................................ 103-150 SECTION VII - DYNAMO AND REGULATOR ...................................... 151-165 TROUBLESHOOTING ......................................................... 166-175 NOTES ii SECTION I - SPECIFICATIONS Model M-12 ..................................................................... 2,3 Model M2-12 .................................................................... 4,5 Model M3-20 . 6,7 Model M4-30 .................................................................... 8,9 Model M-18 ................................................................... 10,11 Model M-25 ..................................................................
    [Show full text]
  • Piston and Connecting Rod Assembly January 2013
    1 50-13 1 1 50-13 SUBJECT DATE Installation of the Piston and Connecting Rod Assembly January 2013 Additions, Revisions, or Updates Publication Number / Title Platform Section Title Change DDC-SVC-MAN-0081 Piston and Connecting DD Platform Added special tool chart. Altered wording in step 21. Rod Assembly All information subject to change without notice. 3 1 50-13 Copyright © 2013 DETROIT DIESEL CORPORATION 2 Installation of the Piston and Connecting Rod Assembly 2 Installation of the Piston and Connecting Rod Assembly Table 1. Service Tools Used in the Procedure Tool Number Description W470589011400 DD13 Carbon Scraper Ring tool W470589021400 DD15 Carbon Scraper Ring tool W470589005900 DD13 Piston Ring Compressor J-47386 DD15/16 Piston Ring Compressor W470589015900 DD15/16 Piston Ring Compressor W470589002500 DD15/16 Cylinder Head Leak Tool NOTICE: DO NOT over-expand the piston rings. Over expansion of the piston rings during installation can lead to hairline cracks resulting in ring failure. Install as follows: 1. If the rings have been removed, install them into the grooves of the piston and rotate 120° apart as follows: a. Install the oil ring expander in the lowest groove in the piston. b. Install the oil control ring (top label up) in the lowest groove around the oil ring expander. c. Install the compression ring (top label up) in the middle groove. d. Install the fire ring (top label up) in the top groove. 2. Allowable new ring end gaps for (A), (B), and (C) are shown below. 4 All information subject to change without notice. Copyright © 2013 DETROIT DIESEL CORPORATION 1 50-13 1 50-13 Table 2.
    [Show full text]
  • Thermodynamic Benefits of Opposed-Piston Two- 2011-01-2216 Published Stroke Engines 09/13/2011
    Gratis copy for Randy Herold Copyright 2011 SAE International E-mailing, copying and internet posting are prohibited Downloaded Thursday, August 18, 2011 12:14:28 PM Thermodynamic Benefits of Opposed-Piston Two- 2011-01-2216 Published Stroke Engines 09/13/2011 Randy E. Herold, Michael H. Wahl, Gerhard Regner and James U. Lemke Achates Power, Inc. David E. Foster Univ. of Wisconsin - Madison Copyright © 2011 SAE International doi:10.4271/2011-01-2216 piston two-stroke engine has inherently lower peak in- ABSTRACT cylinder temperatures than the four-stroke engine, lower A detailed thermodynamic analysis was performed to intake pressure was required to meet the NOx emissions demonstrate the fundamental efficiency advantage of an constraint and as a result lower pumping work was needed. opposed-piston two-stroke engine over a standard four-stroke At the simulated condition considered, the opposed-piston engine. Three engine configurations were considered: a two-stroke engine had approximately 9.0% lower brake- baseline six-cylinder four-stroke engine, a hypothetical three- specific fuel consumption than the four-stroke engine. cylinder opposed-piston four-stroke engine, and a three- cylinder opposed-piston two-stroke engine. The bore and INTRODUCTION stroke per piston were held constant for all engine Opposed-piston two-stroke engines were conceived in the configurations to minimize any potential differences in 1800's in Europe and subsequently developed in multiple friction. The closed-cycle performance of the engine countries for a wide variety of applications including aircraft, configurations were compared using a custom analysis tool ships, tanks, trucks, and locomotives and maintained their that allowed the sources of thermal efficiency differences to presence throughout most of the twentieth century [1,2,3,4,5].
    [Show full text]
  • Analysis of the Influences of Piston Crankshaft Offset on Piston Secondary Movements Yan Hongwei*, Yang Jin and Zhang Baocheng
    Send Orders for Reprints to [email protected] The Open Mechanical Engineering Journal, 2015, 9, 933-937 933 Open Access Analysis of the Influences of Piston Crankshaft Offset on Piston Secondary Movements Yan Hongwei*, Yang Jin and Zhang Baocheng School of Mechanical and Power Engineering, North University of China, Taiyuan, Shanxi, 030051, P.R. China Abstract: This paper takes dynamics analysis on the piston and the dynamic lubrication theory on the skirt and the ring of piston as the basis. Using AVL Glide software, through the establishment of the analysis model of the piston secondary movements, this study focuses on the effects of the crankshaft bias on piston secondary movements’ characteristics. This paper takes 5 different offsets, by comparing the piston lateral displacement, transverse movement speed, transverse acceleration, swinging angle, swing angular velocity and angular acceleration, finds out the relationships between crank offset value and the piston “slap”, piston impact energy and piston skirt friction loss, thus, provides the basis for the design of internal combustion engines. Keywords: Crank offset, piston, piston impact energy, secondary movement. 1. INTRODUCTION liner, piston stiffness matrices’ calculation, the confirmation of the mass of piston group, confirmation of inertia and data The piston secondary movements are some small preparation [6]. Other needed data mainly includes movements exist in the processes of the reciprocating work parameters of the piston and cylinder liner piston structure of internal combustion engines. They specifically refer to, size, the mass of all parts of the group and inertia and under the pressure of the gas deflagration, inertia force, the crankshaft connecting rod size [7].
    [Show full text]
  • 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.
    [Show full text]
  • 1 Fuels and Combustion Bengt Johansson
    1 1 Fuels and Combustion Bengt Johansson 1.1 Introduction All internal combustion engines use fuel as the source for heat driving the thermo- dynamic process that will eventually yield mechanical power. The fuel properties are crucial for the combustion process. Some combustion processes require a fuel that is very prone to ignition, and some have just the opposite requirement. Often, there is a discussion on what is the optimum. This optimum can be based on the fuel or the combustion process. We can formulate two questions: • What is the best possible fuel for combustion process x? • What is the best possible combustion process for fuel y? Both questions are relevant and deserve some discussion, but it is very seldom that the fuel can be selected without any considerations, and similarly, there is only a limited selection of combustion processes to choose from. This brief intro- duction discusses the combustion processes and the link to the fuel properties that are suitable for them. Thus, it is more in the line of the first question ofthe aforementioned two. 1.2 The Options For internal combustion engines, there are three major combustion processes: • Spark ignition (SI) with premixed flame propagation • Compression ignition (CI) with nonpremixed (diffusion) flame • Homogeneous charge compression ignition, HCCI with bulk autoignition of a premixed charge. These three processes can be expressed as the corner points in a triangle accord- ing to Figure 1.1. Within this triangle, all practical concepts reside. Some are a combination of SI and HCCI, some a combination of SI and CI, and others a Biofuels from Lignocellulosic Biomass: Innovations beyond Bioethanol, First Edition.
    [Show full text]
  • Piston Spool Valves and Poppet Valves - a Technical Comparison of Available Solenoid Valves
    Piston spool valves and poppet valves - A technical comparison of available solenoid valves White Paper This whitepaper includes information on: • An introduction to valve technologies • Poppet valves, piston spool valves and the cartridge principle – what you need to know • Which valve type suits you best? A valve selection aid © Copyright 2018, Festo AG & Co. 1 Executive Summary Why should you choose your valves carefully? The increasing demands placed on valve technology in recent years has led to a formidable extension of the range of available technologies and valve types, models, and properties. The most commonly used are poppet valves and piston spool valves. Nowadays, there is a much wider choice of valve technologies to successfully plan a project. However, choosing the right parts for the application at hand requires comprehensive knowledge and an accurate appraisal by the consulting engineer or technician. This White Paper is intended to offer you a brief overview. Figure 1: Examples of valve technologies © Copyright 2018, Festo Inc. 2 Introduction Figure 2 shows when the air flows through the valve from channel 1 to channel 2, the surface area D2 is larger than D1. The supplied Poppet valves and piston spool valves are the operating pressure acts on both surfaces most commonly used valves for controlling resulting in the forces on the spool to be compressed air. Flat slide valves, rotary slide unbalanced. To increase actuation force to valves, piezo valves and other technologies shift spool, pressure, depended poppet tend not to be used as often. The chart in valves need to have larger pilot control Figure 1 offers an example of how the two components.
    [Show full text]