Overview of Automotive Engine Friction and Reduction Trends– Effects of Surface, Material, and Lubricant-Additive Technologies
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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 -
A Model-Based Design Approach to Redesign a Crankshaft for Powder Metal Manufacturing
A model-based design approach to redesign a crankshaft for powder metal manufacturing VASILEIOS ANGELOPOULOS Master of Science Thesis Stockholm, Sweden 2015 A model-based design approach to redesign a crankshaft for powder metal manufacturing VASILEIOS ANGELOPOULOS Master of Science Thesis MMK 2015:100 MKN 154 KTH Industrial Engineering and Management Machine Design SE-100 44 STOCKHOLM Examensarbete MMK 2015:100 MKN 154 En modellbaserad designstrategi att omkonstruera en vevaxel för pulvermetallurgi Angelopoulos Vasileios Godkänt Examinator Handledare 2015-11-08 Ulf Sellgren Stefan Björklund Uppdragsgivare Kontaktperson Höganäs ab Marcus Persson Sammanfattning En vevaxel är en motorkomponent som används för att omvandla den fram- och återgående rörelsen hos kolv och vevstake till en roterande rörelse. De klassiska metoderna att tillverka vevaxlar har varit dominerande och inte gett någon plats för alternativa tillverkningsmetoder. Powder manufacturing är en metod som kan revolutionera produktionens effektivitet och ekonomi. För att denna tillverkningsmetod ska vara möjlig måste vevaxeln tillverkas i delar. Webs, counter-weights och journal shafts måste produceras individuellt för att sedan sammanfogas. Den största utmaningen för denna avhandling är att förstå om vevaxelns counter webs kan tillverkas med samma form eller med så få olika former som möjligt. Denna avhandling handlar främst om att fastställa dessa tekniska krav och föreslå en ny, modulär design för PM. En kinematisk-kinetisk analys utförs med hjälp av en befintlig vevaxel som skannats och omvandlats till en CAD-modell. De numeriska värdena jämförs med en MBS-modell från Adams. Vevaxeln analyseras med avseende på balansering då motvikternas placering, massa och geometriska egenskaper undersöks. Nya modeller som följer de tekniska krav som krävs skapas och utvärderas med Pugh-matris. -
Wärtsilä 32 PRODUCT GUIDE © Copyright by WÄRTSILÄ FINLAND OY
Wärtsilä 32 PRODUCT GUIDE © Copyright by WÄRTSILÄ FINLAND OY COPYRIGHT © 2021 by WÄRTSILÄ FINLAND OY All rights reserved. No part of this booklet may be reproduced or copied in any form or by any means (electronic, mechanical, graphic, photocopying, recording, taping or other information retrieval systems) without the prior written permission of the copyright owner. THIS PUBLICATION IS DESIGNED TO PROVIDE AN ACCURATE AND AUTHORITATIVE INFORMATION WITH REGARD TO THE SUBJECT-MATTER COVERED AS WAS AVAILABLE AT THE TIME OF PRINTING. HOWEVER, THE PUBLICATION DEALS WITH COMPLICATED TECHNICAL MATTERS SUITED ONLY FOR SPECIALISTS IN THE AREA, AND THE DESIGN OF THE SUBJECT-PRODUCTS IS SUBJECT TO REGULAR IMPROVEMENTS, MODIFICATIONS AND CHANGES. CONSEQUENTLY, THE PUBLISHER AND COPYRIGHT OWNER OF THIS PUBLICATION CAN NOT ACCEPT ANY RESPONSIBILITY OR LIABILITY FOR ANY EVENTUAL ERRORS OR OMISSIONS IN THIS BOOKLET OR FOR DISCREPANCIES ARISING FROM THE FEATURES OF ANY ACTUAL ITEM IN THE RESPECTIVE PRODUCT BEING DIFFERENT FROM THOSE SHOWN IN THIS PUBLICATION. THE PUBLISHER AND COPYRIGHT OWNER SHALL UNDER NO CIRCUMSTANCES BE HELD LIABLE FOR ANY FINANCIAL CONSEQUENTIAL DAMAGES OR OTHER LOSS, OR ANY OTHER DAMAGE OR INJURY, SUFFERED BY ANY PARTY MAKING USE OF THIS PUBLICATION OR THE INFORMATION CONTAINED HEREIN. Wärtsilä 32 Product Guide Introduction Introduction This Product Guide provides data and system proposals for the early design phase of marine engine installations. For contracted projects specific instructions for planning the installation are always delivered. Any data and information herein is subject to revision without notice. This 1/2021 issue replaces all previous issues of the Wärtsilä 32 Project Guides. Issue Published Updates 1/2021 15.03.2021 Technical data updated. -
Methods for Heat Analysis and Temperature Field Analysis of the Insulated Diesel
DOE/NASA/0342-1 NASA CR-174783 19950008390 Methods for Heat Analysis and Temperature Field Analysis of the Insulated Diesel Phase I Progress Report Thomas Morel, Paul N. Blumberg, Edward F. Fort, and Rifat Keribar Integral Technologies Incorporated August 1984 Prepared for NATIONAL AERONAUTICSAND SPACEADMIN ISTRATION Lewis Research Center Under Grant DEN 3-342 1[__ _SPf for ! _i _,:_<,:x._ U.S. DEPARTMENT OF ENERGY L&NGLEY RESEARCHCENTER: Conservationand RenewableEnergy LIBRARYN. ASA Office of Vehicle and Engine R&D .AM__TO_".V,RG,_,_ DISCLAIMER This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof. Printed in the United States of America Available from National Technical Information Service U.S. Department of Commerce 5285 Port Royal Road Springfield, VA 22161 NTIS price codes1 Printed copy: A12 Microfiche copy: A01 1Codes are used for pricing all publications. -
Miniature Free-Piston Homogeneous Charge Compression Ignition Engine
Chemical Engineering Science 57 (2002) 4161–4171 www.elsevier.com/locate/ces Miniature free-piston homogeneous charge compression ignition engine-compressor concept—Part I: performance estimation and design considerations unique to small dimensions H. T. Aichlmayr, D. B. Kittelson, M. R. Zachariah ∗ Departments of Mechanical Engineering and Chemistry, The University of Minnesota, 111 Church St. SE, Minneapolis, MN 55455, USA Received 18 September 2001; received in revised form 7 February 2002; accepted 18 April 2002 Abstract Research and development activities pertaining to the development of a 10 W, homogeneous charge compression ignition free-piston engine-compressor are presented. Emphasis is placed upon the miniature engine concept and design rationale. Also, a crankcase-scavenged, two-stroke engine performance estimation method (slider-crank piston motion) is developed and used to explore the in;uence of engine operating conditions and geometric parameters on power density and establish plausible design conditions. The minimization of small-scale e=ects such as enhanced heat transfer, is also explored. ? 2002 Published by Elsevier Science Ltd. Keywords: Two-stroke engine; Free-piston engine; Homogeneous charge compression ignition; Microchemical; Performance estimation; Micro-power generation 1. Introduction exist: Enhance batteries or develop miniature energy conver- sion devices. Only modest gains may be expected from the This paper is the ÿrst in a two-part series that presents re- former, consequently the latter is being vigorously pursued sults of recent small-scale engine research and development (Peterson, 2001). In particular, miniature engine-generators e=orts conducted at the University of Minnesota. Speciÿ- (Epstein et al., 1997; Yang et al. 1999; Allen et al., 2001; cally, it introduces the miniature free-piston homogeneous Fernandez-Pello, Liepmann, & Pisano, 2001) are considered charge compression ignition (HCCI) engine-compressor especially promising. -
Section 02 - Block Basics
Block Basics – Section 2 Section 02 - Block Basics 2.0 Small Block 330 & 350 Block Key Differences. The key differences between the 330 and 350 are the 350’s larger bore and the Generation 1 Cast Iron Small Block V-8 Facts 330’s forged crank. General. In 1964 Olds replaced their small block 215 V8 with 1964 – 1966 Valve Lifter Angle. All 1964–1966 blocks used a a cast iron block of completely new design. The 330 V-8 different valve lifter angle of attack on the cam (45). Thus shared none of its engine block architecture with that of the 1964–1966 330 blocks CANNOT USE 1967 AND LATER 215 V-8 and the 225 V-6 sourced from Buick. The engine CAMS. All 1964–1966 cams WILL NOT WORK in 1967 and was no longer aluminum, but cast iron, as weight became later blocks. Later blocks used a 39 lifter angle. Blocks with less of a factor with the engine going into both the larger a “1” or “1A” cast up near the oil filler tube used the 45 lifter mid-sized F-85s, Cutlasses and the full-size Jetstars angle and should be avoided, if possible. introduced in that year. The engine was designed as a replacement for the 215, but was cast iron and enlarged in Early 330 Rocker Arms. The first run of 330 blocks was anticipation of the growth in size of the mid-size cars, where equipped with rocker arms similar to the previous 394 block it was to be primarily used and as the workhorse for the that traces its heritage back to 1949. -
Engineering Fundamentals of the Internal Combustion Engine
Engineering Fundamentals of the Internal Combustion Engine . I Willard W. Pulkrabek University of Wisconsin-· .. Platteville vi Contents 2-3 Mean Effective Pressure, 49 2-4 Torque and Power, 50 2-5 Dynamometers, 53 2-6 Air-Fuel Ratio and Fuel-Air Ratio, 55 2-7 Specific Fuel Consumption, 56 2-8 Engine Efficiencies, 59 2-9 Volumetric Efficiency, 60 , 2-10 Emissions, 62 2-11 Noise Abatement, 62 2-12 Conclusions-Working Equations, 63 Problems, 65 Design Problems, 67 3 ENGINE CYCLES 68 3-1 Air-Standard Cycles, 68 3-2 Otto Cycle, 72 3-3 Real Air-Fuel Engine Cycles, 81 3-4 SI Engine Cycle at Part Throttle, 83 3-5 Exhaust Process, 86 3-6 Diesel Cycle, 91 3-7 Dual Cycle, 94 3-8 Comparison of Otto, Diesel, and Dual Cycles, 97 3-9 Miller Cycle, 103 3-10 Comparison of Miller Cycle and Otto Cycle, 108 3-11 Two-Stroke Cycles, 109 3-12 Stirling Cycle, 111 3-13 Lenoir Cycle, 113 3-14 Summary, 115 Problems, 116 Design Problems, 120 4 THERMOCHEMISTRY AND FUELS 121 4-1 Thermochemistry, 121 4-2 Hydrocarbon Fuels-Gasoline, 131 4-3 Some Common Hydrocarbon Components, 134 4-4 Self-Ignition and Octane Number, 139 4-5 Diesel Fuel, 148 4-6 Alternate Fuels, 150 4-7 Conclusions, 162 Problems, 162 Design Problems, 165 Contents vii 5 AIR AND FUEL INDUCTION 166 5-1 Intake Manifold, 166 5-2 Volumetric Efficiency of SI Engines, 168 5-3 Intake Valves, 173 5-4 Fuel Injectors, 178 5-5 Carburetors, 181 5-6 Supercharging and Turbocharging, 190 5-7 Stratified Charge Engines and Dual Fuel Engines, 195 5-8 Intake for Two-Stroke Cycle Engines, 196 5-9 Intake for CI Engines, 199 -
Crankpin Bearings in High Output Aircraft Piston Engines the Evolution of Their Design and Loading by Robert J
Crankpin Bearings in High Output Aircraft Piston Engines The Evolution of their Design and Loading by Robert J. Raymond July 2015 Abstract powered truck. There you will invariably find a 6-cylinder, 4-stroke cycle, open chamber, turbocharged, aftercooled The development of the crankpin bearing in high output engine with electronically controlled fuel injection. Gone are aircraft piston engines is traced over the period 1915-1950 in the two-stroke cycle, divided combustion chambers, and the a large number of liquid and air cooled engines of both many variants of mechanical injection systems found in American and European origin. The changes in bearing truck engines of the past. dimensions are characterized as dimensionless ratios and At the end of the large piston engine era there was still a the resulting changes in the associated weights of rotating broad spectrum of engine configurations being produced and reciprocating parts as weight densities at the crankpin. and actively developed. Along with the major division Bearing materials and developments are presented to indi- between liquid and air-cooled engines there was a turbo- cate how they accommodated increasing bearing loads. compounded engine, a four-row air-cooled radial engine, Bearing loads are characterized by maximum unit bearing engines with poppet valves and engines with sleeve valves, pressure and minimum oil film thickness and plotted as a all in production. There were also a two-stroke turbo-com- function of time. Most of the data was obtained from the lit- pounded Diesel engine, a 2-stroke spark ignition sleeve erature but some results were calculated by the author. -
Cat-3408-3412-Torque
3408 & 34 1 2 G EN E RATO R S ET E N G I N ES SE N R2561 -0 1 CATERPILLAR' Specifications 3408 & 3412 GENERATOR SET ENGINES Media Number -SENR2561-01 Publication Date -01/02/2001 Date Updated -15/10/2001 Engine Design (3408) CYLINDER AND VALVE LOCATION Bore ... 137.2 mm (5.40 in.) Stroke ... 152.4 mm (6.00 in.) Arrangement and Number of Cylinders ... 65° V-8 Valves per Cylinder ... 4 Combustion ... Direct Injection Firing Order (Injection Sequence) ... 1,8,4,3,6,5,7,2 Rotation of Crankshaft (when seen from flywheel end) ... counterclockwise Rotation of Fuel Pump Camshaft (when seen from pump drive end) ... counterclockwise NOTE: Front end of engine is opposite to flywheel end. 3 3408 & 34 1 2 G EN E RATO R S ET E N G I N ES SE N R2561 -0 1 CATERPILLAR' Specifications 3408 & 3412 GENERATOR SET ENGINES Media Number -SENR2561-01 Publication Date -01/02/2001 Date Updated -15/10/2001 Engine Design (3412) CYLINDER AND VALVE LOCATION Bore ... 137.2 mm (5.40 in.) Stroke ... 152.4 mm (6.00 in.) Arrangement and Number of Cylinders ... 65° V-12 Valves per Cylinder ... 4 Combustion ... Direct Injection Firing Order (Injection Sequence) ... 1,4,9,8,5,2,11,10,3,6,7,12 Rotation of Crankshaft (when seen from flywheel end) ... counterclockwise 5 3408 & 3412GENERATOR SET ENGINES S E N R256 1 -0 1 CATERPILLAR Specifications 3408 & 3412 GENERATOR SET ENGINES Media Number -SENR2561-01 Publication Date -01/02/2001 Date Updated -15/10/2001 Cylinder Heads (3408) (1) Large bolts (3/4 inch). -
Heat Engine Driven by Shape Memory Alloys: Prototyping and Design
Heat Engine Driven by Shape Memory Alloys: Prototyping and Design Ean H. Schiller Thesis submitted to the Faculty of Virginia Polytechnic Institute and State University in partial fulfillment of the requirements for a degree of Master of Science in Mechanical Engineering Dr. Charles Reinholtz, Chairman Dr. Harry Robertshaw Dr. Donald J. Leo September 19, 2002 Blacksburg, VA Keywords: shape memory alloy, SMA, Nitinol, heat engine Copyright 2002, Ean Schiller Heat Engine Driven by Shape Memory Alloys: Prototyping and Design Ean H. Schiller (ABSTRACT) This work presents a novel approach to arranging shape memory alloy (SMA) wires into a functional heat engine. Significant contributions include the design itself, a preliminary analytical model and the realization of a research prototype; thereby, laying a foundation from which to base refinements and seek practical applications. Shape memory alloys are metallic materials that, if deformed when cold, can forcefully recover their original, "memorized" shapes, when heated. The proposed engine consists of a set of SMA wires stretched between two crankshafts, synchronized to rotate in the same direction. Cranks on the first crankshaft are slightly longer than cranks on the second. During operation, the engine is positioned between two distinct thermal reservoirs such that half of its wires are heated while the other half are cooled. Wires on the hot side attempt to contract, driving the engine in the direction that relieves the heat-induced stress. Wires on the cold side soften and stretch as the engine rotates. Because the force generated during heated recovery exceeds that required for cooled deformation, the engine is capable of generating shaft power. -
Mike Mavrigian Special Firing Order Camshafts Allow the Performance
Performance Perspectives Special firing order camshafts allow the performance engine builder to create a smoother-running engine, with improved fuel distribution and enhanced crankshaft and main bearing durability. his article falls under the category for the same reasons...to smooth out the harmon- of “thinking outside the box.” It’s a ics in the pursuit of greater engine durability and trite phrase, I know, but the point to potentially generate more power. is that we don’t need to always Power gain potential aside, the primary reason think of an OE carmaker’s engine to address (and alter) cylinder firing order is to Mike firing order specification as gospel. achieve a smoother-running engine (a smoother, Mavrigian In certain racing applications, a special firing or- more lineal acceleration ramp), with less harmonic Tder (SFO) camshaft can be used as a tuning aid, effect (and crank deflection) on the crankshaft and [email protected] allowing the competition engine builder to fur- its main bearings. In theory, virtually all engines can ther address combustion heat and crankshaft dis- benefit from this. The engines that can most bene- turbance (harmonic) issues. fit include those that run at or near peak rpm levels In essence, the goal in changing the firing or- for long periods of time, such as oval track, road der is to create a smoother-running engine and race and marine engine applications, as well as en- more even fuel distribution, with enhanced gines that are called upon to produce maximum crankshaft and main bearing durability. In the power in a very short period of time (drag race). -
The W Engine Concept
Service. Self-Study Programme 248 The W Engine Concept Design and Function Introduction The constantly rising demands regarding The W engines set exacting demands on design. performance, running comfort and fuel economy Large numbers of cylinders were adapted to the have led to the advancement of existing drive extremely compact dimensions of the engine. units and the development of new drive units. In the process, more attention was paid to lightweight design. The new W8 as well as the W12 engine by This Self-Study Programme will familiarise you VOLKSWAGEN are representatives of a new with the engine mechanicals of the W engine engine generation - the W engines. family. S248_101 New Important Note This Self-Study Programme explains the design Please always refer to the relevant Service Literature for cur- and function of new developments. rent inspection, adjustment and repair instructions. The contents will not be updated! 2 At a glance Introduction . .4 Engine mechanicals . 10 Specifications . 10 The crankshaft drive . .14 The engine in detail . 15 The chain drive . 28 The camshaft timing control . 29 The belt drive . 32 The oil circuit . 34 The coolant circuit . 42 The air supply . 46 The exhaust system . 50 Service . .52 Sealing concept . 52 Engine timing overview. 54 Special tools . 56 3 Introduction W engines - what does the W stand for? With the aim of building even more compact When the W engine is viewed from the front, the units with a large number of cylinders, the design cylinder arrangement looks like a double-V. features of the V and VR engines were combined Put the two Vs of the right and left cylinder banks to produce the W engines.