Dissertations / Theses on the topic 'Engine system'
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Romanov, Artyom. "Rocket Engine System Analysis : Vinci Engine Turbines Analysis, Volvo Aero Corp." Thesis, Linköping University, Linköping University, Linköping University, Applied Thermodynamics and Fluid Mechanics, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17766.
Full textMajor part of the current work describes the development of the update methodology for onedimensional code (TML) currently used at Volvo Aero Corporation during turbine design process. The methodology is then applied and tried out in a general engine analysis (GESTPAN).
Mahmoud, Osama Esmail. "An intelligent engine condition monitoring system." Thesis, University of Newcastle Upon Tyne, 2009. http://hdl.handle.net/10443/1665.
Full textWatson, Veronica. "Basic system configuration in search engine." Xavier University / OhioLINK, 2008. http://rave.ohiolink.edu/etdc/view?acc_num=xavier1545566567119888.
Full textDriscoll, Robert B. "Investigation of Sustained Detonation Devices: the Pulse Detonation Engine-Crossover System and the Rotating Detonation Engine System." University of Cincinnati / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1459155478.
Full textNorouzi, Shahrouz. "Interaction of diesel type fuels and engine fuel system components in compression ignition engines." Thesis, University of Birmingham, 2014. http://etheses.bham.ac.uk//id/eprint/5369/.
Full textZhang, Kai. "Air charge system emulation for diesel engine." Thesis, University of Bath, 2010. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.521014.
Full textXu, Jingbo. "GRAPE : parallel graph query engine." Thesis, University of Edinburgh, 2017. http://hdl.handle.net/1842/28927.
Full textDietrich, Hans. "Vergleich des Kreiskolbenmotors System NSU-Wankel mit dem Hubkolbenmotor." Doctoral thesis, Saechsische Landesbibliothek- Staats- und Universitaetsbibliothek Dresden, 2013. http://nbn-resolving.de/urn:nbn:de:bsz:14-qucosa-115035.
Full textFrick, Peyton M. "A hydraulic actuated thermal management system for large displacement engine cooling systems." Connect to this title online, 2007. http://etd.lib.clemson.edu/documents/1193080466/.
Full textSjöstrand, Johan. "A communication system for a pluggable game engine." Thesis, Linköping University, Department of Electrical Engineering, 2007. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-8361.
Full textThis thesis documents the development of a communication system that is part of a pluggable game engine for a course in advanced game programming. It covers some techniques and problems in network game programming, a description of the developed system and an example of how the system is used in a demo of the game engine.
Colic, Dalibor, and Jakob Norin. "CONTROL STRATEGY AND MODELING FOR ENGINE OIL SYSTEM." Thesis, Mälardalens högskola, Akademin för innovation, design och teknik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-55030.
Full textGräsberg, Pontus. "IC-Engine Source Characterisation and exhaust system simulations." Thesis, KTH, Marcus Wallenberg Laboratoriet MWL, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-299411.
Full textFör att kunna modellera ljudtrycket som avges från ett avgassystem behöver man kunna beskriva källan. Källan i form av en bränslemotor kan linjärt beskrivas som en källstyrka och en källimpedans. En bränslemotor kan dock ha en akustisk ickelinjär del vilket medför att källan kan vara beroende utav vilken last i form av ljuddämpare den är kopplad till. Första delen av detta arbete undersöker genom motorsimuleringar i GT-Power hur lasten påverkar källkarakteristiken. Den andra delen av arbetet kombinerar källkarakteristiken med simuleringar av ljuddämparen och jämför olika metoder för att få ljudtrycket vid utloppet av avgassystemet. Den första metoden för detta är direkt simulering av ljuddämparen i COMSOL Multiphysics där källkarakteristiken inkluderas och den andra metoden är transfermatris baserad. Det testas också hur känsligt ljudtrycket vid utloppet av ljuddämparen är för variationer i impedansen. För källkarakteristiken används fem laster per uträkning och slutsatsen dras att lasten i form av röret mellan motor och ljuddämpare samt ljuddämparen bör vara så lik som möjligt det riktiga systemet. Utöver det dras slutsatsen att en liten variation i det kopplande rörets längd ger bättre resultat och att en variation mellan största och minsta röret på 100 mm ger bra resultat. Till sist dras slutsatsen att för varvtal över 1000 RPM är källkarakteristiken tillräckligt stabil för att ge stabila resultat vid utloppet av ljuddämparen, medans under 1000 RPM kan det vara stabilt nog men här är validering viktigare.
Lius, Andreas. "Single cylinder research engine multi-spark ignition system." Thesis, KTH, Maskinkonstruktion (Inst.), 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-232371.
Full textIn this project, a 5-cylinder SI port-injected engine is converted to single cylinder operation by deactivating four of the cylinders. A concept generation process resulted in four different concepts where one of them was chosen to be implemented. Previous setups have been used before where cylinders have been deactivated by drilling holes in the piston.Unwanted compression work for the deactivated cylinders is minimized by allowing ventilation to the atmosphere. The inlet valves are removed and the inlet guides plugged. A modified intake connects the deactivated cylinders to the atmosphere. To manage the oil in the deactivated cylinders which otherwise would be combusted is routed to a manifold and finally a catch tank. With this setup, the rotating assembly is untouched thereby retaining the stock engine balance.A capacitive ignition system where the spark energy can be altered during operation is implemented. The ignition system is comprised of two separate ignition units and coils which is connected to the same spark plug. This setup allows full control of when the second spark is released when operated in a multi-spark mode. The system has been designed to minimize the time from spark demand to spark initiation. This is to prepare for future use where an experimental control algorithm will be used which doesn’t use traditional look-up tables.In an initial stage, the fuel and spark will be controlled by an aftermarket engine control unit. The system is installed using the standard sensors on the engine. The control unit can alter relevant parameters during operation using a graphical user interface. The system incorporates closed-looped lambda and knock control for safe operation. The stock exhaust gas recirculation system is incorporated with the engine control unit.Auxiliary units and other components not necessary for single operate are removed. The engine is also prepared to accommodate a high-pressure pump for future direct injection.
Höglund, Filip. "Knock Detection in a Two-Stroke Engine to be Used in the Engine Management System." Thesis, Linköpings universitet, Fordonssystem, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-104681.
Full textSides, Steve P. (Steve Paul) 1963. "Driving robust jet engine design through metrics." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/88331.
Full textFleming-Dahl, Arthur. "A chaotic communication system with a receiver estimation engine." Diss., Georgia Institute of Technology, 1998. http://hdl.handle.net/1853/15651.
Full textCATY, Fabien. "DESIGN OF SECONDARY AIR SYSTEM AND THERMAL MODELS FOR TRIPLE SPOOL JET ENGINES." Thesis, KTH, Kraft- och värmeteknologi, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-98875.
Full textRowles, Craig M. 1962. "System integration analysis of a large commercial aircraft engine." Thesis, Massachusetts Institute of Technology, 1999. http://hdl.handle.net/1721.1/9753.
Full text10912289
Includes bibliographical references (p. 93-94).
In this thesis we develop and demonstrate a method, called a System Integration Analysis, to produce a comprehensive understanding of the activities Integrated Product Teams (IPTs) perform in designing and developing a large complex product or system. The methodology is applied to an existing product or system whose physical architecture can be partitioned into comparable sections, or chunks, as the IPTs who design and develop it. Its goal is to identify specific integrative mechanisms to better align the Integrated Product Development (IPD) process and the organization with the product architecture. These mechanisms are then developed into specific recommendations in consideration of a strategic and tactical framework for achievement of the desired future state of the organization and its IPD process. Implementation of the initiatives is directed to a comprehensive change process defined to address the cultural, structural, and political reality of the company. The methodology uses two distinct applications of a Design Structure Matrix, and several complimentary approaches to the analysis of the data. The methodology is demonstrated with a world-class commercial high bypass-ratio turbofan engine, the Pratt & Whitney PW4098. This product is a derivative design of an existing configuration, or family of engines. Recommendations based upon the PW4098 application include specific interface management and system integration improvements, a minor organizational re-alignment, stronger discipline management, and clearly defined roles and responsibilities of key players.
by Craig M. Rowles.
S.M.
Holmeros, Linus. "Data acquisition system for rocket engine hot fire testing." Thesis, KTH, Maskinkonstruktion (Inst.), 2009. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-99495.
Full textECAPS has developed a unique propellant with a rocket engine which can be used to control satellites and replace Hydrazin which today is the most common fuel onboard on satellites. Hydrazin is extremely toxic and cancerogenic. The new propellant offers 6 % better specific impulse and 30 % better density impulse compared to hydrazine. ECPAS´s propellant also provides significant lower risks for both man and environment. The report includes a literature study about rocket engines which can be used on satellites and how the test environment is arranged where ECAPS develops their engines. The rocket engine is first generally described and then complemented a theoretical derivation of common concepts. For further development of new rocket engines the present engine test system has too few sensor channels and limited sampling capability (2 kHz). The operator interface and software can be upgraded and the number of channels needs to increase. This report treats the implementation of a new test system which is written in Labview 8.6 and has improved for example performance, stability and interface. The sampling frequency is now 10 kHz on 24 channels with a margin for up to 40 channels, alarm functions exists on both temperature and multiple choice sensors, the user interface is logic and more ergonomic together with increased traceability for different types of tests which are saved in unique logs.
Valenti, Carlo Alberto. "Development of a control system for an aeronautical engine." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2019.
Find full textWu, Xiongnan Newman. "A Compositional Automation Engine for Verifying Complex System Software." Thesis, Yale University, 2019. http://pqdtopen.proquest.com/#viewpdf?dispub=13851930.
Full textFormal verification is the only known way of building bug-free or hacker-proof programs. However, due to its prohibitive associated costs, formal verification has rarely been considered as an option in building robust large-scale system software. Practical system software normally consists of highly correlated interdependent subsystems, with complex invariants that need to be globally maintained. To reason about the correctness of a program, we not only need to show that the program in consideration satisfies the invariants and the specification, but also prove that the invariants cannot be accidentally broken by other parts of the system, e.g., via pointer manipulation. Furthermore, we often have some snippet of code that temporarily breaks the invariants, and re-establishes them later, which could make reasoning of such code more complex. Even worse, many complex system software contains device drivers to work with the devices, which brings a major challenge of handling device interrupts; and consists of multiple threads running on multiple CPUs concurrently. This forces us to further reason about arbitrary interactions and interleaved executions among different devices, interrupts, and programs running on different CPUs, which could quickly make the verification task intractable.
In this dissertation, we present a compositional, and powerful automation engine for effectively verifying complex system software. It is compositional because it solely focuses on providing strong automation support for verifying functional correctness properties of C source programs, while taking the memory isolation and invariant properties as given, and separately provide a systematic approach for guaranteeing the isolation among different in-memory data, and proving invariants, completely at the logical level. The engine also contains a novel way of representing devices and drivers, and simulation-based approach for turning the low-level interrupt model into an equivalent abstract model which is suitable for reasoning about interruptible code. Furthermore, the engine provides a new way of representing concurrently shared states into a sequence of external UO events and allows us to verify concurrent programs as if they were sequential and provided a separate logical framework to effectively reason about interleaved executions. This very modular design allows us to be able to reason about each aspect of the system separately, and while each of the reasoning tasks looks unbelievably simple, we could combine all the proofs to obtain proofs of properties about complex system software. An OS kernel is a typical example of complex low-level system software with highly interdependent modules. To illustrate the effectiveness of our approach, using all the tools, we have developed a fully verified feature-rich operating system kernel with machine-checkable proof in the Coq proof assistant.
Liu, Chunmeni 1970. "Dynamical system modeling of a micro gas turbine engine." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/9249.
Full textAlso available online at the MIT Theses Online homepage
Includes bibliographical references (p. 123).
Since 1995, MIT has been developing the technology for a micro gas turbine engine capable of producing tens of watts of power in a package less than one cubic centimeter in volume. The demo engine developed for this research has low and diabtic component performance and severe heat transfer from the turbine side to the compressor side. The goals of this thesis are developing a dynamical model and providing a simulation platform for predicting the microengine performance and control design, as well as giving an estimate of the microengine behavior under current design. The thesis first analyzes and models the dynamical components of the microengine. Then a nonlinear model, a linearized model, and corresponding simulators are derived, which are valid for estimating both the steady state and transient behavior. Simulations are also performed to estimate the microengine performance, which include steady states, linear properties, transient behavior, and sensor options. A parameter study and investigation of the startup process are also performed. Analysis and simulations show that there is the possibility of increasing turbine inlet temperature with decreasing fuel flow rate in some regions. Because of the severe heat transfer and this turbine inlet temperature trend, the microengine system behaves like a second-order system with low damping and poor linear properties. This increases the possibility of surge, over-temperature and over-speed. This also implies a potentially complex control system. The surge margin at the design point is large, but accelerating directly from minimum speed to 100% speed still causes surge. Investigation of the sensor options shows that temperature sensors have relatively fast response time but give multiple estimates of the engine state. Pressure sensors have relatively slow response time but they change monotonically with the engine state. So the future choice of sensors may be some combinations of the two. For the purpose of feedback control, the system is observable from speed, temperature, or pressure measurements. Parameter studies show that the engine performance doesn't change significantly with changes in either nozzle area or the coefficient relating heat flux to compressor efficiency. It does depend strongly on the coefficient relating heat flux to compressor pressure ratio. The value of the compressor peak efficiency affects the engine operation only when it is inside the range of the engine operation. Finally, parameter studies indicate that, to obtain improved transient behavior with less possibility of surge, over-temperature and over-speed, and to simplify the system analysis and design as well as the design and implementation of control laws, it is desirable to reduce the ratio of rotor mechanical inertia to thermal inertia, e.g. by slowing the thermal dynamics. This can in some cases decouple the dynamics of rotor acceleration and heat transfer. Several methods were shown to improve the startup process: higher start speed, higher start spool temperature, and higher start fuel flow input. Simulations also show that the efficiency gradient affects the transient behavior of the engine significantly, thereby effecting the startup process. Finally, the analysis and modeling methodologies presented in this thesis can be applied to other engines with severe heat transfer. The estimates of the engine performance can serve as a reference of similar engines as well.
by Chunmei Liu.
S.M.
Ramirez-de-Arellano, Luis G. (Luis Guillermo) 1970. "Engine production system in the US defense aircraft industry." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/50530.
Full textSharad, Kittur Rohan. "Heavy-Duty Spark-Ignited Single Cylinder Engine Fueling System." Thesis, KTH, Maskinkonstruktion (Inst.), 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-232481.
Full textMost of the fundamental research in internal combustion engines is driven by the ever-increasing stringency of emissions regulations along with the need for increased fuel economy. The proposed ban on diesel vehicles in several cities around the world combined with extensive availability, has made natural gas a promising substitute even for heavy-duty applications. The high hydrogen-to-carbon ratio of methane, the major component of natural gas, makes it attractive from an emissions reduction perspective. CO2 emissions from natural gas combustion are particularly low. However, the low cetane number and high activation energy required to ignite natural gas, requires spark-ignition.In a research setting, it is often advantageous to have a single cylinder engine. The main benefit is the ability to study phenomena without adverse interactions which multi-cylinder operation may cause. This is especially important for gas-exchange studies. Quicker replacement of parts and lower fuel consumption are secondary benefits.The focus of this thesis was the implementation of a flexible fueling system for a single cylinder spark-ignited engine. The engine is a Scania 9-liter spark-ignited engine modified for single cylinder operation. Flexibility in terms of charge homogeneity, selective intake port filling and provisions for liquid fuel direct injection have been provided. For ease of use, the engine is controlled by an aftermarket engine control unit with a graphical user interface for configuration. Safety considerations when mixing gaseous fuels and air well upstream of the intake ports have been implemented.
Sastry, Sudeep. "A Thermoacoustic Engine Refrigerator System for Space Exploration Mission." Case Western Reserve University School of Graduate Studies / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=case1301588899.
Full textBucknell, Roger John. "Control system for a gasoline engine including dual spark." Thesis, University of Hertfordshire, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.314566.
Full textSwift, Stuart John. "Applicability of hybrid methods in engine control system design." Thesis, University of Cambridge, 2009. https://www.repository.cam.ac.uk/handle/1810/265493.
Full textSandvik, Joel Emil. "Scaling an Optimization Engine for a Decision Support System." Thesis, Mittuniversitetet, Avdelningen för informations- och kommunikationssystem, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:miun:diva-20441.
Full textMoro, Mike, and Paul J. Friedman. "An Integrated Real-Time Turbine Engine Flight Test System." International Foundation for Telemetering, 1990. http://hdl.handle.net/10150/613817.
Full textNew developments and modifications to existing gas turbine engines require qualification through extensive ground testing followed by flight testing. An increasing work load necessitates productivity improvements in the test platform utilization and the telemetry ground station. This paper addresses the application of a compatible family of commercial offthe-shelf telemetry systems for quick-look to ensure data integrity on board the Boeing 720 test platform, and a distributed architecture ground station to serve multiple engineering disciplines through the use of an acquisition subsystem serving data to independent color graphics workstations via an Ethernet local area network.
Hague, Douglas C. (Douglas Charles) 1967. "Description of a turbofan engine product development process." Thesis, Massachusetts Institute of Technology, 2001. http://hdl.handle.net/1721.1/29164.
Full textIncludes bibliographical references (p. 123-125).
This research explores what requirements are necessary for the development of a turbofan engine and how they evolve through the product development cycle. This work utilizes a parameter-based design structure matrix (DSM) to define the interfaces and interdependencies present in a large commercial aircraft propulsion system. The DSM was developed from the system level to the module level allowing one to examine the assumptions made throughout the entire life cycle of the product. The work utilizes the system-level DSM to show the similarities between the turbofan engine product development process (PDP) and the software spiral product development process. This work examines the parameter-based DSM in each of the design phases and attempts to understand the assumptions made in each phase and how the assumptions change as the product proceeds through the development cycle. By examination of the DSM, it was found that program goals and requirements lead to an initial set of design parameters. These design parameters are then iterated until a satisfactory product defamation is developed. Each stage concludes with the integration and testing of that stages work. In all stages risk management occurs and with the necessary revision of the program plan for subsequent stages (not in the system-level DSM). The work shows that the PDP for a turbofan engine can be viewed as a spiral process. The thesis then suggests that, in general, the current industry practices for the development of complex physical systems have similarity to the spiral framework for development of software.
by Douglas C. Hague.
S.M.
Moy, Habs M. (Habs Mern) 1967. "Commercial gas turbine engine platform strategy and design." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/88328.
Full textFollen, Kenneth. "A System Dynamics Modeling Methodology for Compressible Fluid Systems with Applications to Internal Combustion Engines." The Ohio State University, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=osu1281971505.
Full textMcCauley, Bob. "Expert Systems in Data Acquisition." International Foundation for Telemetering, 1987. http://hdl.handle.net/10150/615229.
Full textIn an Independent Research and Development (IR&D) effort, the Telemetry Systems Operation (TSO) of Computer Sciences Corporation (CSC) sought to determine the feasibility of using Artificial Intelligence (AI) techniques in a real-time processing environment. Specifically, the use of an expert system to assist in telemetry data acquisition processing was studied. A prototype expert system was implemented with the purpose of monitoring F15 Vertical Short Take Off and Landing (VSTOL) aircraft engine tests in order to predict engine stalls. This prototype expert system was implemented on a Symbolics 3670 symbolic processor using Inference Corporation's Artificial Reasoning Tool (ART) expert system compiler/generator. The Symbolics computer was connected to a Gould/SEL 32/6750 real-time processor using a Flavors, Inc. Bus Link for real-time data transfer.
Assanis, Dennis N. "A computer simulation of the turbocharged turocompounded diesel engine system for studies of low heat rejection engine performance." Thesis, Massachusetts Institute of Technology, 1985. http://hdl.handle.net/1721.1/15089.
Full textMICROFICHE COPY AVAILABLE IN ARCHIVES AND ENGINEERING.
Bibliography: leaves 135-140.
by Dionissios Nikolaou Assanis.
Ph.D.
Boulanger, Yves. "A microprocessor system for internal combustion engine PV diagram analysis /." Thesis, McGill University, 1988. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=61266.
Full textThe pressure signal is unstable over successive cycles. Consequently, pressure must be averaged over several consecutive cycles to produce valid data.
Due to instrumentation problems the data obtained was insufficient to allow the development of diagnostics. The investigation reported in this work is thus limited to the development of a microprocessor-based system for the acquisition of pressure-volume data on high speed, spark ignition internal combustion engines.
Several instrumentation problems were identified and solutions applied or proposed. The information presented here can form the basis for further research on the original project.
Johansson, Thomas. "System analysis of a diesel engine with VGT and EGR." Thesis, Linköping University, Department of Electrical Engineering, 2005. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-5438.
Full textTo fulfil emission requirements specified by environment demands, such as Euro 4 and Euro 5, there is a need to utilize engines based on technologies such as Variable Turbine Geometry (VGT) and Exhaust Gas Recirculation (EGR). A model of an engine using VGT and EGR was created by Ph.D student Johan Wahlström at Linköping University. This thesis evaluates Wahlström's model and shows how it successfully describes the engine and its behaviour. The thesis also confirms theories about the occurrens of non.minimum phase behaviour in different transfer functions, e.g. from VGT signal to the mass flow through the compressor.
An interesting phenomenon when applying VGT and EGR is a nonlinearity leading to, for example, that the same pressure in the intake manifold can occur for two different VGT signals. Such phenomenon can cause problems when designing a control system. Furthermore, this nonlinearity also results in a replacement of the nonminimum phase behaviour with an overshoot when a large (above 80%) VGT control signal is used.
This thesis also provides a linearized model, which describes the engine satisfactory. The linearization results in transfer functions with two zeros and three poles, whose locations do not change much when varying engine speed and load (except at high load and low engine speed). This fact will most likely make it possible to utilize just a few different linearizations for all speeds and loads. However, altering VGT and EGR positions greatly affect the transfer functions. Thus, several linearizations are probably needed to cover all operating points.
When designing a future control system a good strategy is to utilize a decoupled system since the model has strong cross-connections. Another solution would be to apply multi dimensional control strategy, e.g. LQ-theory.
Austin, Paul Baden. "Towards a file system for a scalable parallel computing engine." Thesis, University of York, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.304159.
Full textBai, Mo, and Mahabaleshwar Sagar Parampalli. "Accelerated Engine Suspension Load Prediction and Exhaust System Displacement Simulation." Thesis, KTH, Maskinkonstruktion (Inst.), 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-218029.
Full textI dagens konkurrensutsatta bilindustri försöker de flesta företag att göra sina nya mönster och funktioner implementerbara i sina produkter för att vara före sina konkurrenter. I det preliminära konstruktionsstadiet av CEVT-fordon förbrukar dynamisk simulering dock en stor tid beroende på komplexiteten hos den dynamiska modellen och simuleringsinställningarna. Det är fördelaktigt och möjligt att förkorta simuleringstiden. Denna avhandling fokuserar på att minska den dynamiska simuleringstiden i ADAMS / Car i motorupphängningens tidiga utvecklingsstadium. Med hjälp av bakgrundsstudier och erfarenheter från CEVT’s personal provades fem olika sätt att minska simuleringstiden, samtidigt som simuleringsresultatens noggrannhet kontrollerades. Varje metod användes separat i simuleringen för att studera effekten på resultatens noggrannhet. I slutet kombineras alla metoder i simuleringen för att få bästa möjliga simuleringstid utan att förlora noggrannhet. Genom att kombinera de fem metoderna reducerades den totala dynamiska simuleringstiden till 61% och variationen i utmattningsskadans resultat av varje motorupphängningskomponent kontrollerades inom 30%. Dynamisk modellering av ett avgassystem ingår också i denna avhandling, vilket ger referensdata för framtida förpackningsdesign av avgassysteme
Anzalone, Thomas M. "Heat transfer characteristics of a fluidized bed : stirling engine system." The Ohio State University, 1989. http://rave.ohiolink.edu/etdc/view?acc_num=osu1291128389.
Full textKorres, Michael. "Cylinder Pressure Sensor based Engine Combustion and Fuel System Diagnostics." Thesis, KTH, Fordonsdynamik, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-203351.
Full textAlmeida, Fernando Jorge Gonçalves, and João Pedro Brás da Cruz. "Cooling System Analysis." Master's thesis, 2012. http://hdl.handle.net/10316/20538.
Full textABSTRACT This master thesis report describes the behavior of a cooling system based on the power consumption and power losses during the velocity range. The thesis is a report of the behavior of the cooling system to understand were we having more needs to cold down the system. It was used a excel sheet to describe the values of power, losses and efficiencies of the various components of the cooling. With the excel sheets built we studied various cases in the system to show the points more important to take care with the cooling system. Continuing the study, it was showed the power consumptions of the cooling system and also the heat dissipation capacity. The objective included in this thesis is to show that in the regular cooling systems the use of the engine's velocity to move the fan and the coolant pump is not the best choice. Could be currently the less expensive one,but not the best one. This thesis didn’t have the objective to find a solution for a perfect cooling system, but a good report of the problems of the actual cooling systems and where we should spend more time to improve them. This is just a preparatory work for a new work.
Lin, Hsin-Chuan, and 林信傳. "Design and Verification for Engine Management System of EFI Scooter Engines." Thesis, 2007. http://ndltd.ncl.edu.tw/handle/zvyx3r.
Full text國立臺北科技大學
車輛工程系所
95
The purpose of this thesis is to develop an engine management system (EMS) for scooter engine to improve fuel consumption and exhaust emissions. The proposed EMS is consisted of engine operation mode switch, fuel injection, ignition, and idle speed control (ISC) strategies. The engine operation mode switch strategy is used to judge current state of the engine, such as key on, run, idle, fuel cut off, etc. the fuel injection control strategy is designed to control the injection duration and start injection angle based on engine operation conditions, such as engine speed, intake manifold pressure, etc. The ignition control strategy is utilized to control the magnetization time and ignition timing at optimal operating points. The ISC strategy is employed to control the airfuel ratio, carbon deposition, ambient pressure compensation, ignition timing, etc. The Motortron is used as a hardware ECU for developing ECU-based rapid-prototype system and for designing engine control strategy. The MATLAB/Simulink Model-Based is employed as a control strategy development platform. Finally, the Mototune is utilized as an engine calibration tool to regulate the injection and ignition control parameters at engine dynamomoter and chassis dynamomoter. The preliminary experimental results show that the vehicle acceleration, fuel consumption and engine performance of the proposed algorithm including transient and steady state tests are close to the original performance of the scooter.
施翔耀. "Engine-Hanger System for Scooters." Thesis, 1997. http://ndltd.ncl.edu.tw/handle/50644629679868787814.
Full text國立中山大學
機械工程研究所
85
Engine-hanger system is an important mechanism for the riding safety and comfort of scooters. The purpose of this research is develop a systematic design process for the allocation of engine-hanger systems to increase the comfort. First, the conceptual design of the configurations of engine-hanger systems is done by a systematic structural synthesis method, an atlas of engine-hanger systems with six and eight links is successfully constructed. Next, the balancing design of a single cylinder engine is accomplished. Then, the new balance position of the engine-hanger system under a load is determined by the principle of virtual work. Based on the concepts of orthogonality theory and virtual center of percussion, four feasible design concepts of the engine-hanger system of scooters are proposed. Finally, a multi-body modeling is proposed to simulate the engine-hanger system of scooters, and the dynamic response and acceleration of the seat are analyzed. Refer to hanger rotation analysis and acceleration analysis of the seat, the performance of design works is analyzed and compared. In this study, we can obtain potential arrangement design of Engine-Hanger System.
Peng, Yu-Wen, and 彭郁文. "Development of Torque-Based Engine Management System for Range Extender Engine." Thesis, 2012. http://ndltd.ncl.edu.tw/handle/f942n7.
Full text國立臺北科技大學
車輛工程系所
100
Due to the energy crisis , an Electric Vehicle with Range Extender is regarded as the solution of short distance of the electric vehicle , this thesis would like to develop a range extender engine which has Semi-direct Injection (SDI) system and uses cheaper liquified petroleum gas (LPG) as the fuel . A torque-based engine control system described in the thesis uses a control demand to control and satisfy torque requirement. This torque demand is the result of power management strategy, so the engine management system must include the function of receiving and achieving the torque demand. This thesis uses a SDI engine and keeps it in lean-burn to find the best ignition timing, excess air ratio and the engine map, than finds 2 best operating point of the engine: The first is the point which has high torque and lowest fuel consumption; the other one is considerate of noise vibration harshness , so a lower speed and torque is the second operating point. The thesis also use an engine model by Matlab/Simulink to simulate the control strategy, finally the verification of the algorithm by engine experiment. The result shows that the torque-based engine control algorithm makes the engine run at the best operating point steadily, which opens up potential for improvement high efficiency and reduction in fuel consumption
Narayanaswamy, Kushal. "DI-HCCI engine control system development." 2006. http://www.library.wisc.edu/databases/connect/dissertations.html.
Full textSu, Chien-Ying, and 蘇建穎. "Stirling engine geothermal power generation system." Thesis, 2011. http://ndltd.ncl.edu.tw/handle/52816170358246455557.
Full text萬能科技大學
工程科技研究所
100
Because the world of excessive use of fossil fuels, and excessive use of fossil fuels produce carbon dioxide and the greenhouse effect as a result of climate change a serious problem, therefore, the development of green energy is very urgent, geothermal is a natural green energy, the use of geothermal for power generation is the future research direction. In this paper, we actually produce a large size of the Stirling engine, geothermal generators, field testing, access to important information when the actual operation and experience, as well as related results can be used for solar power. The low temperature difference Stirling engine, the choice of materials and design have a lot of flexibility, so we can optimize as much as possible, so it has some potential for development, the low temperature difference Stirling engine can be used In the heat pipe-based solar power, can also be used in geothermal power generation. Stirling engine geothermal power compared to other models, the existing geothermal power generation technology, there are many advantages, can be high for the spa water temperature is not the case, you can smoothly, so the Stirling engine used in geothermal power is a good choice. We actually design a Stirling engine, a large-scale geothermal power, and geothermal valley in Beitou a month field test, the experimental results confirmed that a Stirling engine, geothermal generators, able to meet our design requirements, according to the experimental test results, our laboratory has also produced a smaller temperature difference Stirling engine, plus we use a modified hot tube, round container and improved heat dissipation, maintaining the temperature difference Stirling engine, quite good.
Chen, Jian-Syong, and 陳建雄. "Design Optimization of Engine Mount System." Thesis, 2013. http://ndltd.ncl.edu.tw/handle/58762526145545146963.
Full text國立宜蘭大學
機械與機電工程學系碩士班
101
In this research, ADAMS engineering software was used to create the power model of automobile engine mount system. The vibration reduction analysis for an original engine mount system was performed to calculate the vibration modes and the corresponding frequencies. The energy distribution was calculated as well. The major optimization purpose was to have the torque roll axis approach the elastic axis. Based on the dynamic simulation analysis, two optimization steps for engine mount system were performed. After optimization, full automobile model with 13 degrees of freedom was created to calculate the reaction force at idle condition. After optimization, the torque roll axis was consistent with elastic axis and the decoupling level in system principle direction was significantly increased, the vibration frequencies were decreased, and the reaction force was reduced at idle condition. Keywords: Engine Mount System, Decoupling, Torque Roll Axis, Elastic Roll Axis
林佳明. "Expert system maintenance for aircraft engine." Thesis, 2010. http://ndltd.ncl.edu.tw/handle/80356305251572340768.
Full text建國科技大學
自動化工程系暨機電光系統研究所
98
Generally the maintenance crew compare the malfunction symptoms with fault isolation items of the technical manual to do the engine examination, but, many of the malfunctions are unpredictable and can not be found in the design, and this kind of service needs experienced specialized engineer to provide the domain knowledge. In this study, the virtual configuration of the aircraft engine cold section was chose as object of the study, according to the aircraft engine, 80% malfunctions can be classified as gas path, and based on the existing maintenance of experience and information, rule-based knowledge and case-based knowledge has built. The occurrence of all failure and results compile its own regular pattern. By using software into knowledge base, a combination of artificial intelligence expert system technology to speed up the diagnostic process has been developed. Therefore by this software, it can achieve convenient and rapid fault diagnosis and improve the quality of aircraft maintenance to ensure flight safety.
Schneidewend, Dan. "A custom digital engine control system." 1992. http://catalog.hathitrust.org/api/volumes/oclc/25896872.html.
Full textTypescript. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references (leaves 33-34).
Sue, Yanren, and 蘇筵壬. "Optimization Control Study of Engine Management System for Direct InjectionCommon Rail Diesel Engine." Thesis, 2011. http://ndltd.ncl.edu.tw/handle/16151218503116481064.
Full text大葉大學
機械與自動化工程學系
99
The main purpose of this study is to establish a simulation and analysis methodology for multi-cylinder four-stroke direct-injection common-rail diesel engine management system and to verify the dynamic performance response. The hardware and software of the engine control were combined to display real-time performance parameters with the engine control parameter tuning and multi-objective optimization rules and to verify the engine performance by dynamometer experiments. This study has built the search program for multi-cylinder four-stroke common rail direct injection diesel engine multi-objective goal attainment optimization control parameters. The fuel consumption and pollution of vehicle driving cycle was converted into engine torque and speed by using the real vehicle parameters. Several key points were sorted from the corresponding map data for steady state estimation measurement. The selected key points control parameters were changed to reduce the overall exhaust emissions. Simulation module and combustion analysis models were used to explore injection pressure, injection timing and the injection duration of engine management system. Engine torque, speed and the relationship between the response of pollutants in the exhaust were optimized and compared with the baseline engine measurement data. Real-time display and record of the engine hardware and software parameters, and control parameters under different engine operating conditions were measured. The engine combustion heat release and its rate were calculated by using engine combustion pressure data and validated with combustion analyzer under different engine operating conditions. The dynamic relationship between control and the response data can be used as future reference for developing of engine management systems. By experimental design and multi-objective optimization search, the experiments time and expanse can be reduced and the efficiency of engine parameters calibration and adjustment can thus be improved.