Internal Combustion Piston Engines April 2012
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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 -
Aircraft Engine Performance Study Using Flight Data Recorder Archives
Aircraft Engine Performance Study Using Flight Data Recorder Archives Yashovardhan S. Chati∗ and Hamsa Balakrishnan y Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA Aircraft emissions are a significant source of pollution and are closely related to engine fuel burn. The onboard Flight Data Recorder (FDR) is an accurate source of information as it logs operational aircraft data in situ. The main objective of this paper is the visualization and exploration of data from the FDR. The Airbus A330 - 223 is used to study the variation of normalized engine performance parameters with the altitude profile in all the phases of flight. A turbofan performance analysis model is employed to calculate the theoretical thrust and it is shown to be a good qualitative match to the FDR reported thrust. The operational thrust settings and the times in mode are found to differ significantly from the ICAO standard values in the LTO cycle. This difference can lead to errors in the calculation of aircraft emission inventories. This paper is the first step towards the accurate estimation of engine performance and emissions for different aircraft and engine types, given the trajectory of an aircraft. I. Introduction Aircraft emissions depend on engine characteristics, particularly on the fuel flow rate and the thrust. It is therefore, important to accurately assess engine performance and operational fuel burn. Traditionally, the estimation of fuel burn and emissions has been done using the ICAO Aircraft Engine Emissions Databank1. However, this method is approximate and the results have been shown to deviate from the measured values of emissions from aircraft in operation2,3. -
MACHINES OR ENGINES, in GENERAL OR of POSITIVE-DISPLACEMENT TYPE, Eg STEAM ENGINES
F01B MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES (of rotary-piston or oscillating-piston type F01C; of non-positive-displacement type F01D; internal-combustion aspects of reciprocating-piston engines F02B57/00, F02B59/00; crankshafts, crossheads, connecting-rods F16C; flywheels F16F; gearings for interconverting rotary motion and reciprocating motion in general F16H; pistons, piston rods, cylinders, for engines in general F16J) Definition statement This subclass/group covers: Machines or engines, in general or of positive-displacement type References relevant to classification in this subclass This subclass/group does not cover: Rotary-piston or oscillating-piston F01C type Non-positive-displacement type F01D Informative references Attention is drawn to the following places, which may be of interest for search: Internal combustion engines F02B Internal combustion aspects of F02B 57/00; F02B 59/00 reciprocating piston engines Crankshafts, crossheads, F16C connecting-rods Flywheels F16F Gearings for interconverting rotary F16H motion and reciprocating motion in general Pistons, piston rods, cylinders for F16J engines in general 1 Cyclically operating valves for F01L machines or engines Lubrication of machines or engines in F01M general Steam engine plants F01K Glossary of terms In this subclass/group, the following terms (or expressions) are used with the meaning indicated: In patent documents the following abbreviations are often used: Engine a device for continuously converting fluid energy into mechanical power, Thus, this term includes, for example, steam piston engines or steam turbines, per se, or internal-combustion piston engines, but it excludes single-stroke devices. Machine a device which could equally be an engine and a pump, and not a device which is restricted to an engine or one which is restricted to a pump. -
MARINE ENGINES Power &Propulsion Solutions Index
MARINE ENGINES Power & propulsion solutions Ed. 2018/05 Ed. Index Power range ............................................ 3 Engine range ........................................... 5 Power generation ................................... 8 Marine solutions ..................................... 9 Hybrid systems ..................................... 11 References ............................................ 15 Overall data....... .................................... 18 Anglo Belgian Corporation (ABC) is one of Europe’s leading medium speed engine manufacturers. The company offers more than a century of expertise in ship propulsion. ABC was originally established in 1912 by a group of industri- alists, with participation of the inventor of the diesel engine, Rudolf Diesel himself. An important step in ABC’s history was the acquisition by OGEPAR (1985), a strong fi nancial holding with a large base in metal industry and engineering. Today, ABC has risen far above the standard of engine manufacturer. The company is constantly evolving, developing new solutions in the fi eld of marine propulsion, power generation and locomotive traction. Through innovative thinking, ABC aims to increase sustainability and supply reliable and effi cient products within a framework of ecological development. All engines are designed for heavy duty and continuous operation, straightforward applications and easy maintenance. ABC headquarters and production facility in Ghent, Belgium ABC engines, your * Polar cruise vessel equipped with: 2 x 12DZC @ 750 rpm partner at sea 2 x 6DZC @ 750 rpm For more than 100 years ABC has been supplying power The best quality indicators of our work and engines are solutions to all those who know that the engine is the heart those clients who have trusted us, since 4 generations, of their vessels. ABC engines stand for reliability and good with the installation of our engines in their ships, performance under the hardest and most demanding condi- showing this trust from father to son. -
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. -
500 Years of Maritime History
500 Years of Maritime History By the mid-sixteenth century King Philip of Spain felt an acute need to establish a coastal stronghold in the territory he claimed as “La Florida," a vast expanse including not only present-day Florida but most of the continent. The Atlantic coast of present-day Florida was strategically important for its proximity to Spanish shipping routes which followed the Gulf Stream and annually funneled the treasures of Philip's New Above: Traditional Spanish New World shipping routes. World empire back to Spain. The two biggest threats to this transfer of wealth were pirate attacks and shipwrecks. A military outpost on the Florida coast could suppress piracy while at the same time serve as a base for staging rescue and salvage operations for the increasing number of ships cast away on Florida's dangerous shoals. With these maritime goals in mind, the King charged Don Pedro Menéndez de Avilés with the task of establishing a foothold on Florida's Atlantic coast. Before leaving Spain, word reached the Spanish court that a group of French protestants had set up a fledgling colony in the region, and Menéndez' mission was altered to include the utter destruction of the French enterprise, which represented not only heresy but a direct threat to Spain's North American hegemony. The French Huguenots, led by René de Laudonnière, had by 1563 established Fort Caroline at the bank of the River of May (present-day St. Johns River at Jacksonville, north of St. Augustine). Early in 1565, France's King Charles sent Jean Ribault to re-supply and assume command of the Fort. -
Comparison of Helicopter Turboshaft Engines
Comparison of Helicopter Turboshaft Engines John Schenderlein1, and Tyler Clayton2 University of Colorado, Boulder, CO, 80304 Although they garnish less attention than their flashy jet cousins, turboshaft engines hold a specialized niche in the aviation industry. Built to be compact, efficient, and powerful, turboshafts have made modern helicopters and the feats they accomplish possible. First implemented in the 1950s, turboshaft geometry has gone largely unchanged, but advances in materials and axial flow technology have continued to drive higher power and efficiency from today's turboshafts. Similarly to the turbojet and fan industry, there are only a handful of big players in the market. The usual suspects - Pratt & Whitney, General Electric, and Rolls-Royce - have taken over most of the industry, but lesser known companies like Lycoming and Turbomeca still hold a footing in the Turboshaft world. Nomenclature shp = Shaft Horsepower SFC = Specific Fuel Consumption FPT = Free Power Turbine HPT = High Power Turbine Introduction & Background Turboshaft engines are very similar to a turboprop engine; in fact many turboshaft engines were created by modifying existing turboprop engines to fit the needs of the rotorcraft they propel. The most common use of turboshaft engines is in scenarios where high power and reliability are required within a small envelope of requirements for size and weight. Most helicopter, marine, and auxiliary power units applications take advantage of turboshaft configurations. In fact, the turboshaft plays a workhorse role in the aviation industry as much as it is does for industrial power generation. While conventional turbine jet propulsion is achieved through thrust generated by a hot and fast exhaust stream, turboshaft engines creates shaft power that drives one or more rotors on the vehicle. -
TEST for VESSEL STATUS Lozman V. City Of
CASE COMMENT IF IT LOOKS LIKE A VESSEL: THE SUPREME COURT’S “REASONABLE OBSERVER” TEST FOR VESSEL STATUS Lozman v. City of Riviera Beach, 133 S. Ct. 735 (2013) David R. Maass∗ What is a vessel? In maritime law, important rights and duties turn on whether something is a vessel. For example, the owner of a vessel can limit his liability for damages caused by the vessel under the Limitation of Shipowners’ Liability Act,1 and an injured seaman who is a member of the crew of a vessel can claim remedies under the Jones Act.2 Under the general maritime law, a vendor who repairs or supplies a vessel may acquire a maritime lien over the vessel.3 In these and other areas, vessel status plays a crucial role in setting the limits of admiralty jurisdiction. Clear boundaries are important because with admiralty jurisdiction comes the application of substantive maritime law—the specialized body of statutory and judge-made law that governs maritime commerce and navigation.4 The Dictionary Act5 defines “vessel” for purposes of federal law. Per the statute, “[t]he word ‘vessel’ includes every description of watercraft or other artificial contrivance used, or capable of being used, as a means of transportation on water.”6 The statute’s language sweeps broadly, and courts have, at times, interpreted the statute to apply even to unusual structures that were never meant for maritime transport. “No doubt the three men in a tub would also fit within our definition,” one court acknowledged, “and one probably could make a convincing case for Jonah inside the whale.”7 At other times, however, courts have focused on the structure’s purpose, excluding structures that were not designed for maritime transport.8 In Stewart v. -
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. -
Wankel Powered Time to Climb World Record Attempt
Wankel powered time to climb world record attempt Presentation at Aero Expo, Friedrichshafen, Germany April 19th, 2018 by Paul Lamar Several years ago an American rotor head by the name of Russ MacFarlane living in Newcastle Australia decided to build a Mazda rotary powered world record attempt time to climb aircraft. Russ was a long time subscriber to the Rotary Engine News Letter. A used flying Harmon Rocket home built aircraft was purchased and the Lycoming engine and instruments were removed and sold. The aircraft is very similar to a Van's RV4 with longer landing gear and shorter wings. Dan Grey, owner of Aviation FX in Santa Paula California was chosen to finish the project and get it flying. I was the project engineer. Dan is a 787 captain for UAL. The Wankel rotary has a much better power to weight ratio and power to size ratio than any automotive piston engine. It is also far more robust and will withstand ungodly amounts of turbo boost with out structural failure. Up to 100 inches of Mercury manifold pressure is possible. That translates to almost 1000 HP for an all aluminum turbo two rotor weighing less than 200 pounds. That is about four HP per pound of engine weight. Most aircraft engines are about one HP per pound of weight or worse. Any piston engine operating at aircraft power levels has a limited life. That is the reason for a TBO. The moving parts are magnafluxed for cracks at TBO. The cracks are caused by reversing stress on the crankshaft, connecting rods, pistons and valve parts. -
Positive Displacement Reciprocating Pump Fundamentals— Power and Direct Acting Types
POSITIVE DISPLACEMENT RECIPROCATING PUMP FUNDAMENTALS— POWER AND DIRECT ACTING TYPES by Herbert H. Tackett, Jr. Reciprocating Product Manager James A. Cripe Senior Reciprocating Product Engineer Union Pump Company; A Textron Company Battle Creek, Michigan and Gary Dyson Director of Product Development - Aftermarket Union Pump, A Textron Company A Trading Division of David Brown Engineering, Limited Penistone, Sheffield ABSTRACT Herbert H. Tackett, Jr., is Reciprocating Product Manager for Union Pump Company, This tutorial is intended to provide an understanding of the in Battle Creek, Michigan. He has 39 years fundamental principles of positive displacement reciprocating of experience in the design, application, and pumps of both power and direct acting types. Topics include: maintenance of reciprocating power and • A definition and overview of the pump types—Including the direct acting pumps. Prior to Mr. Tackett’s differences between single acting and double acting pumps, how current position in Aftermarket Product both types work, where they are used, and how they are applied. Development, he served as R&D Engineer, Field Service Engineer, and new equipment • Component options—Covers aspects of valve designs and when order Engineer, in addition to several they should be used; describes the various stuffing box designs positions in Reciprocating Pump Sales and Marketing. He has been available with specific reference to their function and application, a member of ASME since 1991. and points out the differences between plungers and pistons and their selection criteria. • Specification criteria and methodology—What application James A. Cripe currently is a Senior information is needed by pump suppliers to correctly size and Reciprocating Product Engineer assigned supply appropriate equipment? to the New Product Development Team for Union Pump Company, in Battle Creek, • Additional topics—Volumetric and mechanical efficiency, net Michigan. -
Small Scale ORC Plant Modeling with the Amesim Simulation Tool: Analysis of Working Fluid and Thermodynamic Cycle Parameters Influence
Available online at www.sciencedirect.com ScienceDirect Energy Procedia 81 ( 2015 ) 440 – 449 69th Conference of the Italian Thermal Engineering Association, ATI 2014 Small scale ORC plant modeling with the AMESim simulation tool: analysis of working fluid and thermodynamic cycle parameters influence. M. Antonelli*, A. Baccioli, M. Francesconi, P. Psaroudakis, L. Martorano Università di Pisa, D.E.S.Te.C., Largo Lucio Lazzarino, Pisa 56122, Italy Abstract ORC plant transient modeling is an actual issue for the correct assessment of the size of the various components of the system especially when unpredictable fluctuations of the inlet thermal flux are to be considered. This work shows the modeling procedure of a small scale (10-50 kW) Waste Heat Recovery ORC plant which uses an innovative expansion device derived from a Wankel engine. The numerical model here presented was developed with the simulation tools AMESim and simulates the transient behavior of such a small scale system in all its main components: preheater, evaporator, expansion device and condenser. The aims of this work were to evaluate the suitability of the Wankel-derived mechanism to ORC systems and to establish its optimal working conditions for the employment in a low-grade heat recovery system. The application of several working fluids as well as of various operating conditions are presented in this paper. The analysis of the transient response of the plant is also presented with a particular attention to start up operations. © 20152015 Published The Authors. by Elsevier Published Ltd. This by E islse anvier open Ltd access. article under the CC BY-NC-ND license (Peerhttp://creativecommons.org/licenses/by-nc-nd/4.0/-review under responsibility of the Scientific).