This thesis is concerned with the study of parallel mixing of two dissimilar gases under compressible conditions in the confined environment. A number of numerical studies are reported in the literature for the compressible mixing of two streams of gases where (1) both the streams are of similar gases at the same temperatures, (2) both the streams are at different temperatures with similar gases, and (3) dissimilar gases are with nearly equal temperatures. The combination of dissimilar gases at large temperature difference, mixing under compressible conditions, as in the case of scramjet propulsion, has not been adequately addressed numerically. Also many of the earlier studies have used two dimensional numerical simulation and showed good match with the experimental results on mixing layers that are inherently three dimensional in nature. In the present study, both two-dimensional (2-d) and three dimensional (3-d) studies are reported and in particular the effect of side wall on the three dimensionality of the flow field is analyzed, and the reasons of the good match of two dimensional simulations with experimental results have been discussed. Both two dimensional and three dimensional model free simulations have been conducted for a flow configuration on which experimental results are available. In this flow configuration, the mixing duct has a rectangular cross section with height to width ratio of 0.5. In the upper part of the duct hydrogen gas at a temperature of 103 K is injected through a single manifold of two Ludweig tubes and in the lower part of the duct nitrogen gas at a temperature of 2436 K is supplied through an expansion tube, both the gases are at Mach numbers of 3.1 and 4.0 respectively. Measurements in the experiment are limited to wall pressures and heat flux. The choice of this experimental condition gives an opportunity to study the effect of large temperature difference on the mixing of two dissimilar gases with large molecular weights under compressible conditions. Both two dimensional and three dimensional model free simulations are carried out using higher order numerical scheme (4th order spatial and 2nd order temporal) to understand the structure and evolution of supersonic confined mixing layer of similar and dissimilar gases. Two dimensional simulations are carried out by both SPARK (finite difference method) and OpenFOAM (finite volume method based open source software that was specially picked out and put together), while 3D model free simulations are carried out by OpenFOAM. A fine grid structure with higher grid resolution near the walls and shear layer is chosen. The effect of forcing of fluctuations on the inlet velocity shows no appreciable change in the fully developed turbulent region of the flow. The flow variables are averaged after the attainment of statistical steady state established through monitoring the concentration of inert species introduced in the initial guess. The effect of side wall on the flow structure on the mixing layer is studied by comparing the simulation results with and without side wall. Two dimensional simulations show a good match for the growth rate of shear layer and experimental wall pressures. Three dimensional simulations without side wall shows 14% higher growth rate of shear layer than that of two dimensional simulations. The wall pressures predicted by these three dimensional simulations are also lower than that predicted using two dimensional simulations (6%) and experimental (9%) results in the downstream direction of the mixing duct. Three dimensionality of the flow is thought of as a cause for these differences. Simulations with the presence of side wall show that there is no remarkable difference of three dimensionality of the flow in terms of the variables and turbulence statistics compared to the case without side walls. However, the growth rate of shear layer and wall surface pressures matches well with that predicted using two dimensional simulations. It has been argued that this good match in shear layer growth rate occurs due to formation of oblique disturbances in presence of side walls that are considered responsible for the decrease in growth rate in 3-d mixing layers. The wall pressure match is argued to be good because of hindrance from side wall in the distribution of momentum in third direction results in higher wall pressure. The effect of dissimilar gases at large temperature difference on the growth rate reduction in compressible conditions is studied. Taking experimental conditions as baseline case, simulations are carried out for a range of convective Mach numbers. Simulations are also carried out for the same range of convective Mach numbers considering the mixing of similar gases at the same temperature. The normalized growth rates with incompressible counterpart for both the cases show that the dissimilar gas combination with large temperature difference shows higher growth rate. This result confirms earlier stability analysis that predicts increased growth rate for such cases. The growth rate reduction of a compressible mixing layer is argued to occur due to reduced pressure strain term in the Reynolds stress equation. This reduction also requires the pressure and density fluctuation correlation to be very near to unity. This holds good for a mixing layer formed between two similar gases at same temperature. For dissimilar gases at different temperatures this assumption does not hold well, and pressure-density correlation coefficient shows departure from unity. Further analysis of temperature density correlation factor, and temperature fluctuations shows that the changes in density occur predominantly due to temperature effects, than due to pressure effects. The mechanism of density variations is found to be different for similar and dissimilar gases, while for similar gases the density variations are due to pressure variations. For dissimilar gases density variation is also affected by temperature variations in addition to pressure variations. It has been observed that the traditional k-ε turbulence model within the RANS (Reynolds Averaged Navier Stokes) framework fails to capture the growth rate reduction for compressible shear layers. The performance of k-ε turbulence model is tested for the mixing of dissimilar gases at large temperature difference. For the experimental test case the shear layer growth rate and wall pressures show good match with other model free simulations. Simulations are further carried out for a range of convective Mach numbers keeping the mixing gases and their temperatures same. It has been observed that a drop in the growth rate is well predicted by RANS simulations. Further, the compressibility option has been removed and it has been observed that for the density and temperature difference, even for incompressible case, the drop in growth rate exists. This behaviour shows that the decrease in growth rate is mainly due to the interaction of temperature and species mass fraction on density. Also it can be inferred that RANS with k-ε turbulence model is able to capture the compressible shear layer growth rate for dissimilar gases at high temperature difference. The mixing of heat and species is governed by the values of turbulent Prandtl and Schmidt numbers respectively. These numbers have been observed to vary for different flow conditions, while affecting the flow field considerable in the form of temperature and species distribution. Model free simulations are carried out on an incompressible convective Mach number mixing layer, and the results are compared with that of a compressible mixing layer to study the effect of compressibility on the values of turbulent Prandtl / Schmidt numbers. It has been observed that both turbulent Prandtl and Schmidt numbers show an almost constant value in the mixing layer region for incompressible case. While, for a compressible case, both turbulent Prandtl and Schmidt numbers show a continuous variation within the mixing layer. However, the turbulent Lewis number is observed to be near unity for both incompressible and compressible cases. The thesis is composed of 8 chapters. An introduction of the subject with critical and relevant literature survey is presented in chapter 1. Chapter 2 describes the mathematical formulation and assumptions along with solution methodology needed for the simulations. Chapter 3 deals with the two and three dimensional model free simulations of the non reacting mixing layer. The effect of the presence of side wall is studied in chapter 4. Chapter 5 deals with the effect of compressibility on the mixing of two dissimilar gases at largely different temperatures. The performance of k-ε turbulence model is checked for dissimilar gases in Chapter 6. Chapter 7 is concerned with the effect of compressibility on turbulent Prandtl and Schmidt numbers. Finally concluding remarks are presented in chapter 8. The main aim of this thesis is the exploration of parallel mixing of dissimilar gases under compressible conditions for both two and three dimensional cases. The outcome of the thesis is (a) a finding that the presence of sidewall in a mixing duct does not make flow field two dimensional, instead it causes the formation of oblique disturbances and the shear layer growth rate is reduced, (b) that it has been shown that the growth rates of dissimilar gases are affected far more by large temperature difference than by compressibility as in case of similar gases, (c) that the growth rates of compressible shear layers formed between dissimilar gases are better predicted using k-εturbulence model and (d) that for compressible mixing conditions the turbulent Prandtl and Schmidt numbers vary continuously in the mixing layer region necessitating the use of some kind of model instead of assuming constant values.

Depuis quelques années, les modèles 0D trouvent un regain d'intérêt auprès des motoristes. En effet, ces modèles, fournissant aisément un comportement thermodynamique du moteur, peuvent être couplés avec des outils de contrôle moteur. Néanmoins, leur précision doit être augmentée, pour répondre aux enjeux technologiques actuels. Dans les moteurs à allumage commandé, la flamme turbulente prémélangée est modélisée comme un ensemble de flammelettes cohérentes entre elles. Cette approche généraliste nécessite un traitement particulier en proche paroi, motivé par une modification de la structure de flamme due aux couches limites thermique et cinématique. Ce présent travail propose des approches de modélisations 0D de la combustion, en proche paroi et dans la zone réactionnelle de la flamme. Pour modéliser la combustion en proche paroi, la flamme est scindée en une contribution en propagation libre, et une contribution en interaction avec les parois. Chaque contribution est divisée en une zone de transport, dans laquelle l'entraînement des gaz frais est décrit, et une zone de réaction, dans laquelle la réaction de combustion est modélisée. L'ajout d'une zone de réaction en interaction avec les parois permet de modéliser un gradient de température et une réaction de combustion ralentie en proche paroi. Pour modéliser la zone réactionnelle, une discrétisation de la flamme en N zones de réaction indépendantes est proposée. Une plage de fonctionnement moteur a été simulée avec nos approches de modélisation, afin de quantifier la variabilité des paramètres de calibration. Pour ce faire, les modèles sont calibrés sur chaque point de fonctionnement, par une méthode de minimisation de l'erreur quadratique moyenne sur la loi de dégagement d'énergie. Des corrélations aisées de paramètres de calibration peuvent être établies, en fonction de paramètres moteurs. Les résultats de simulations, obtenus à partir de ces corrélations, sont satisfaisants. / Recently, the interest for zero-dimensional models has increased. Indeed, these models provide easily the engines thermodynamic behavior and can be coupled with control tools. However, their accuracy must be improved to meet the current technological challenges. In the spark ignition engines, the premixed turbulent flame is modeled as a set of coherent flamelets. This approach requires special treatment near the walls, motivated by the modifications of the flame structure due to boundary layers. The present work proposes 0D modeling of combustion near the walls and in the reaction zone of the flame. To combustion model near the walls, the flame is divided into a free propagation contribution, and an interacting contribution with the walls. Each contribution is divided into a convective zone, wherein the entrainment of fresh gas is described, and a reaction zone, wherein the combustion reaction is modeled. Adding a reaction zone near the walls allows modeling a thermal gradient and a slower combustion reaction near the walls. To model the reaction zone, a flame discretization is made into several reaction zones. An engine operating range is simulated with our models, for quantifying the calibration parameters variability. To do this, models are calibrated on each operating point, by a method of minimization of the quadratic error on the heat released rate. Linear correlations can be found, depending on engines parameters. A good agreement between experimental data and simulation results is obtained with these parameters correlations.

L'augmentation continue des charges de fonctionnement des moteurs à allumage commandé a conduit à l'apparition d'une nouvelle forme de combustion anormale à bas régime sous la forme d'un pré allumage. Dans des conditions de pression et de température extrêmes, une auto-inflammation incontrôlée du mélange carburé peut en effet se produire avant l'allumage normal à la bougie et conduire à une seconde auto-inflammation de type cliquetis donnant naissance à des oscillations de pression inacceptables même pour les moteurs les plus robustes. Cette anomalie constitue donc une véritable limite au downsizing des moteurs et à l'augmentation de leurs performances spécifiques. Cette dernière forme de combustion anormale est bien plus critique que le cliquetis car son apparition est aléatoire, le plus souvent sporadique et généralement très violente. Ces caractéristiques fondamentales expliquent que de nouveaux outils et de nouvelles méthodologies d'analyse aient dû être développés pour mieux caractériser le processus d'auto-inflammation dans ces conditions extrêmes. Des méthodes statistiques avancées ont notamment été mises au point pour quantifier de manière fiable la fréquence d'apparition du pré allumage malgré son caractère aléatoire. En parallèle, un travail expérimental important a été réalisé pour mettre au point une méthodologie de réalisation de visualisations endoscopiques permettant de mieux analyser le processus de combustion, et d'identifier de manière plus précise les zones préférentielles d'apparition du pré allumage dans la chambre de combustion. Les impacts des paramètres fondamentaux régissant l'auto-inflammation (aérodynamique interne, thermique et chimie du mélange) ont d'abord été analysés sur un monocylindre de recherche. Le processus de combustion a ainsi été détaillé et l'hypothèse d'une auto-inflammation spontanée en phase gazeuse a également pu être abordée en parallèle de l'analyse expérimentale par une approche numérique RANS. Une étude plus approfondie a ensuite montré qu'il était possible qu'un pré allumage conduise à une auto-inflammation de type détonation, ce qui explique qu'un nombre réduit d'occurrences suffise à détériorer irrémédiablement le moteur. La versatilité du monocylindre a également permis de mettre en évidence la diversité des phénomènes qui pouvaient conduire au pré allumage et d'autres hypothèses que celle d'une auto-inflammation spontanée en phase gazeuse ont ainsi pu être formulées. Celles-ci ont finalement été testées sur un multicylindre en appliquant des méthodologies d'essais et d'analyse éprouvées sur monocylindre. Les investigations tournées vers l'impact des réglages moteur ont alors notamment confirmé que les impacts du carburant sur les parois de la chambre de combustion conduisaient à la formation de films liquides dont les caractéristiques locales pouvaient être favorables à une auto-inflammation. / The continuous increase of engine loads on SI engines has provoked the apparition of a new form of abnormal combustion at low engine speed in the guise of a pre-ignition. Under extreme conditions of pressure and temperature, an uncontrolled auto-ignition of the fresh mixture can happen well before the normal ignition at the spark and lead to a knocking-like second auto-ignition and to unacceptable pressure oscillations even for modern and robust engines. This anomaly constitutes thus a strong limit to the downsizing of gasoline engines and to the increase of their specific performance. This latter abnormal combustion is far more critical than knocking combustion since its apparition is random, most often sporadic and usually very violent. These fundamental characteristics explain that new tools and methodologies had to be developed to achieve a better characterization of the auto-ignition process under such extreme conditions. Advanced statistical methods have notably been defined to obtain a reliable quantification of the pre-ignition frequency despite its randomness. A significant work has simultaneously been realized to develop an experimental methodology dedicated to endoscopic visualizations allowing a better analysis of the combustion process and a more precise identification of the preferential areas of auto-ignition inside the combustion chamber. The impacts of fundamental parameters governing auto-ignition (the mixture's charge motion, thermal and chemical evolutions) have first been analyzed thanks to a research single cylinder engine. That way, the combustion process has been detailed and the hypothesis of a spontaneous auto-ignition of the gaseous mixture has also been tackled at the same time with the help of a numerical RANS approach. Then, a deeper analysis has showed that pre-ignition could lead to a developing detonation mode during the second auto-ignition, explaining so that a reduced number of events could cause irremediable damages. Thanks to the flexibility of the single cylinder engine, it has also been shown that a wide variety of phenomena could lead to pre-ignition and it has made possible the formulation of other hypotheses than a spontaneous auto-ignition of the gaseous mixture. These ones have finally been tested on a serial multi-cylinder engine with test and analysis methodologies validated on the single cylinder engine. The investigations focused on the impacts of settings have then confirmed that the fuel impacts on the liner and on the piston lead to the formation of liquid films whose local characteristics could be favorable to auto-ignition.

L’électroérosion (EE) est une technique d’usinage sans contact de matériaux conducteursd’électricité ; elle particulièrement bien adaptée à l’usinage de matériaux durs. Le principe consiste àcréer des décharges électriques érodantes entre un outil et une pièce à usiner, toutes deuximmergées dans un diélectrique. Dans cette thèse, nous avons étudié la miniaturisation de ceprocédé, la microélectroérosion (μEE), qui se présente comme un procédé complémentaire destechniques de micro-usinage mécanique, laser, ou encore des techniques issues de lamicrotechnologie du silicium (RIE, DRIE, LIGA). Toutefois, la résolution de la μEE est limitée.Dans ce travail, nous avons tout d’abord développé un procédé original d’élaboration de microoutilscylindriques en tungstène par gravure électrochimique. Celui-ci permet d’obtenir de manièrereproductible des micro-outils de diamètre 15 μm et de rapport hauteur sur diamètre supérieur à 50.Des micro-outils plus fins ont aussi été obtenus (jusqu’à 700 nm) mais avec des problèmes dereproductibilité. Par ailleurs, un prototype de machine de fraisage par μEE a été développé avec uneélectronique entièrement caractérisée. Des micro-canaux de 40 μm de largeur ont été obtenus dansl’acier d’inoxydable et 25 μm dans le titane ; une rugosité Ra de 86 nm a été atteinte dans des cavitésde 600 x 600 x 30 μm. Les limitations du dispositif expérimental ont aussi été mises en évidence.Dans la dernière partie de ce travail, nous avons procédé à l’étude des microdécharges et du microplasmas’établissant entre micro-outil et pièce à l’aide de caractérisations électriques. La résistanceet l’inductance des décharges ont été déterminées expérimentalement puis intégrées dans unmodèle permettant de prévoir la durée des impulsions de courant et leur intensité. Des pistes pourl’amélioration de la résolution d’usinage sont proposées en conclusion de ce travail. / Electro Discharge Machining (EDM) is a non-contact technique allowing machining of electricallyconductive materials; it is well adapted for the machining of hard materials. The principle is based onthe creation of eroding electrical discharges between a tool and a piece, both immersed in adielectric. In this thesis, we have the studied miniaturization of the process, called micro electrodischarge machining (μ-EDM), which is considered as a complementary technique of mechanical orlaser micro-machining techniques and silicon micro technology processes (RIE, DRIE, LIGA)..However, the resolution of μEDM is limited.In this work, we have firstly developed an original method for making tungsten micro-tools withcylindrical profile by electrochemical etching. This method allows the reproducible fabrication ofmicro-tool with 15-μm diameter. Thinner micro-tools were also obtained (down to 700 nm) withreproducibility problems. Furthermore, a prototype machine for milling μ-EDM was developed with afully characterized electronics. Micro channels were obtained respectively in stainless steel with awidth of 40μm and in titanium with a width of 25μm; a surface roughness Ra of 86 nm was achievedin 600 x 600 x 30 μm cavities. Besides, the limitations of the apparatus were highlighted. In the lastpart of this work, we have studied the micro-discharge and the micro-plasma between the micro-tooland the part with electrical characterization. The resistivity and the inductance of the sparks weremeasured and integrated in a numerical model in order to explain the duration of the microdischarges and their intensity. Solutions for improving the machining resolution are also discussed atthe end of this work.

The goal of this diploma thesis is to design and develop a system for collecting, processing and storing data from large IoT networks. The developed system introduces a complex solution able to process data from various IoT networks using Apache Hadoop ecosystem. The data are real-time processed and stored in a NoSQL database, but the data are also stored  in the file system for a potential later processing. The system is optimized and tested using data from IQRF network. The data stored in the NoSQL database are visualized and the system periodically generates derived predictions. Users are connected to this system via an information system, which is able to automatically generate notifications when monitored values are out of range.

Techniky rychlého slinování jako „Spark Plasma Sintering (SPS)“, „Flash Sintering“ (FS), „Selective Laser Sintering“ (SLS), „Induction Sintering“ (IS) a „Microwave Sintering“ (MS) jsou navrženy tak, aby účinně a předvídatelně kontrolovaly mikrostrukturu během slinovací proces. Spark Plasma Sintering jako jedna z nejmodernějších technik rychlého slinování a byla studována po celá desetiletí. V SPS má tři hlavní rysy: přímý ohřev elektrickým proudem, pulzní stejnosměrný elektrický proud a mechanický tlak. Mechanismy působení faktorů během SPS procesu však nejsou zatím jasně objasněny. Tato práce byla inspirována zvýšeným zájmem o techniky rychlého slinování a snahou o objasnění působení hlavních faktorů. Tato studie je rozdělena do čtyř částí: efekt elektromagnetického pole, efekt pulzního vzoru, tlakový efekt a přímý Joulův ohřev. Výsledky ukázaly, že elektromagnetické pole v SPS může být ignorováno, jak ukázaly simulace, a rovněž během experimentů nebyl nalezen žádný „efekt pole“. Na druhou stranu účinek pulzního vzoru byl významný, prášek TiO2 byl slinován pulzními vzory 12:2 a 10:9 s konstantním příkonem. Po aplikaci pulzního vzoru 10:9 došlo ke zvýšení velikosti zrna o jeden řád a ke zvýšení hustoty o 8%, zatímco množství spotřebované energie zůstalo konstantní. Při zahřátí s různými vzory pulzů se mění účinný výkon a kontaktní odpor indukovaný mechanickým pulsem, což jsou dva hlavní důvody, které vysvětlují měnící se energetickou účinnost. Vliv tlaku byl také významný, výsledky ukázaly, že použití tlaku při 900 ° C přineslo vysokou hustotu a malou velikost zrn, což vedlo k nejvyšší tvrdosti měřenou podle Vickerse. Interakce mezi tlakem a parami, vedoucí k rozdílné rychlosti přenosu páry v prvním slinovacím stupni, je považována za důvod pro rozdíly v mikrostruktuře, jako jsou mikropóry. Načasování mechanického tlaku může také podporovat difúzní mechanismy zhutňování během druhého slinovacího stupně, jako je difúze na hranicích zrn a mřížková difúze. Přímý ohřev, kdy se vede elektrický proud přímo skrz vzorek, vede k nízké měřené teplotě při slinování karbidu boru a jeho kompozitů, avšak teplota uvnitř vzorku je podstatně vyšší. Přidání slitiny titanu a křemíku do B4C významně zvýšilo finální hustotu, což byl hlavní důvod ovlivnění mechanických vlastností. Vzorek B4C + 1.0Ti (1 obj. % Ti slitiny) dosáhl nejvyšší tvrdosti 3628.5 ± 452.6 HV1 (16.2% vyšší než čistý B4C) s lomovou houževnatostí 2.11 ± 0.25 MPa m0.5. Zatímco při dopování křemíkem dosáhl vzorek B4C + 0.5Si (0.5 obj. % křemíku) nejvyšší tvrdosti 3524.6 ± 207.8 HV1 (o 13.0% vyšší než čistý B4C), vzorek B4C + 1.0Si dosáhl nejvyšší lomové houževnatosti 2.97 ± 0.03 MPa m0.5 (o 15.6% vyšší než čistý B4C). Velikost zrn kompozitů dotovaných titanem se oproti čistému karbidu boru byla o něco větší a mikrostruktura více nehomogenní. Naproti tomu se velikost zrn vzorků dotovaných křemíkem příliš nezměnila ve srovnání s velikostí zrn čistého karbidu boru. Sekundární fáze karbid křemíku byla dobře spojena s matricí karbidu boru a vykazovala pozitivní účinek jak na tvrdost, tak na lomovou houževnatost. Tato práce zkoumala vliv různých kontroverzních a nepopsaných aspektů na slinování keramických materiálů metodou Spark Plasma Sintering, což vedlo k lepšímu pochopení této techniky slinování.

This thesis deals with the influence of process parameters on the contamination level of powder materials produced by mechanical alloying (MA) technology. For this purpose austenitic stainless steel 316 L and equiatomic CoCrFeNi high-entropy alloy (HEA) were prepared by high-energy ball milling. Both materials were milled in argon and nitrogen atmospheres from 5 to 30 hours. Spark plasma sintering method (SPS) was then used for consolidation of chosen powder samples. Chemical analysis of contamination within MA was carried out using combustion analysers for determination of carbon, oxygen, and nitrogen contents after different lengths of milling. Also differences in chemical composition of powder and corresponding bulk samples were measured. The microstructure analysis using scanning electron microscopy (SEM) of both powder and bulk materials was executed with focus on oxide and carbide presence and dispersion. Increasing content of carbon with increasing milling time was observed across all measured samples. This contamination is attributed to using milling vial made of tool steel AISI D2 (containing 1,55 wt. % of carbon). Increase of carbon content within consolidation using SPS was also observed. Milling of specimens using N2 as milling atmosphere caused higher contamination level in both AISI 316 L and HEA compared to milling in argon.

[pt] As projeções para as próximas décadas indicam que os combustíveis tradicionais, derivados do petróleo, associados à utilização de biocombustíveis nos motores de combustão interna continuarão sendo a principal fonte de propulsão dos veículos. Isto justifica as intensas pesquisas por todo o Mundo, para atender aos desafios de aumento de eficiência e redução de emissões de poluentes. As modelagens dos combustíveis comerciais, que possuem centenas de componentes, e dos processos de combustão em motor são, hoje, desafios reais. Também carecem estudos sistemáticos para compreender melhor como os diferentes componentes de combustíveis interagem em mistura e influenciam os parâmetros de combustão e desempenho nos motores. No presente trabalho, realizaram-se seleção de componentes e ensaios experimentais em motor comercial para identificar formulações reduzidas representativas de gasolinas comerciais brasileiras. Concluiu-se que formulações compostas de n-heptano, iso-octano, tolueno e etanol podem ser utilizadas para modelagem de gasolinas oxigenadas. Implementaram-se metodologias para avaliar a influência dos componentes nas propriedades dos combustíveis e parâmetros de combustão e desempenho do motor, identificando os potencias de cada componente e seus grupos químicos. Com dados experimentais de pressão no cilindro desenvolveu-se modelagem para se calcular a velocidade de propagação de chama no motor, bem como foram obtidas relações para calculá-la a partir da velocidade de chama laminar do combustível na condição padrão. Estas relações possuem como parâmetros de entrada o Reynolds de admissão, pressão e temperatura dos gases não queimados na câmara de combustão. Os resultados reúnem informações e metodologias que poderão ser usadas em várias etapas do processo de desenvolvimento de combustíveis para diferentes aplicações. / [en] For the next decades it is expected that the fossil fuels and bio-fuels usage in internal combustion engines remains to be the main source for vehicular propulsion. This justifies the intense worldwide research and development to comply with the challenges of increasing efficiency and emissions reduction. The modeling of commercial fuels and engine combustion processes presents great challenges. There is also the need to better understand how different fuel components interact and influence engine combustion and performance parameters. In the present work, components selection and engine dynamometer tests were done to identify representative surrogate fuels for commercial Brazilian gasoline. It was concluded that formulations of n-heptane, iso-octane, toluene and ethanol can be used to model oxygenated gasolines. Methodologies were implemented to evaluate the influence of the fuel components on fuel properties and several engine combustion and performance parameters. The potentials of each component and corresponding chemical group were identified. Using in cylinder pressure measurements it was developed a methodology to calculate flame propagation velocity in a commercial engine. Further, mathematical modeling was developed to calculate this combustion parameter, based on fuel laminar flame velocity at standard condition. The relations were designed considering the intake Reynolds number, temperature and pressure of the unburned gases inside the cylinder. The results put together informations and methodologies that can be used in several steps of the fuel development process for different applications.

This master thesis deals with ignition systems which are used in cars vehicles with gas engines and also with setting of the best moment of ignition of gasoline-air mixture in cylinders of engine. Ways of gas injection at diesel engines and their control systems are also described in this thesis. Next chapter deals with control unit and describes main actions which are necessary for today’s motor vehicles. As illustration is used example of succession of actions which are necessary for calculation and setting regular value of pre-ignition. At the end is shown animation, which can be used for practice lessons in a subject Automobile Electric and Electronic Systems as a example. It will simplify understanding of described activities which are all accomplished by central control unit. For purposes of laboratory lessons is in this thesis also discussed measuring of engine performance with changes of parameter of central control unit.

The diploma thesis focuses on the problems of electric power precipitators. Due to their current dominant position, the work concentrates on the sources of single phase transformers operating at the frequency of 50 Hz controlled by thyristors. The first part describes the electrostatic precipitator and its principle. This is followed by a brief insight into the proposal for an electrostatic precipitator. The work also explains the high voltage source that is divided into a transformer with a rectifier and into a control box with power circuits and control circuits that provide the power supplied by a transformer. The work also offers an explanation of the HV source system that operates at different conditions. The last part suggests a proposal for cooling cabinet including thyristors, for power line control box resources, for a supply line and a line to the transformer.