This last decade experienced a sudden increase of interest in the control of thermo-acoustic instabilities, in particular through the use of fuel modulation techniques. The primary goal of this research was to design, construct and characterize a high bandwidth proportional fuel injection system, which could be used to study the effect of specific levels of fuel modulation on the combustion process and the reduction of thermo-acoustic instabilities. A fuel injection system, incorporating the use of a closed loop piston and check valve, was designed to modulate the primary fuel supply of an atmospheric liquid-fueled swirl stabilized combustor operating at a mean volumetric fuel flow rate of 0.4 GPH. The ability of the fuel injection system to modulate the fuel was examined by measuring the fuel line pressure and the flow rate produced during operation. The authority of this modulation over the combustion process was investigated by examining the effect of fuel modulation on the combustor pressure and the heat release of the flame. Sinusoidal operation of the fuel injection system demonstrated: a bandwidth greater that 800 Hz, significant open loop authority (averaging 12 dB) with regards to the combustor pressure, significant open loop authority (averaging 33 dB) with regards to the unsteady heat release rate and an approximate 8 dB reduction of the combustor pressure oscillation present at 100 Hz, using a phase shift controller. It is possible to scale the closed loop piston and check valve configuration used to create the fuel injection system discussed in this work to realistic combustor operating conditions for further active combustion control studies. / Master of Science

The first part of this work focuses on control experiments performed on an unstable kerosene-fueled turbulent combustor. Using a phase shift controller and primary fuel modulation stability is successfully gained for a wide band of global equivalence ratios allowing the limitations of the control scheme to be characterized. It is shown that control signal saturation can significantly impact the ability of the control scheme to stabilize the system. Three different regions of controllability are defined based on the degree of saturation. A hysteresis behavior is also found to exist for the controller settings depending on whether stability is being maintained or realized for an unstable system. The second part of this work focuses on the impact that primary fuel modulation has on the fuel spray. Measurements for a simplex nozzle and an air-assist nozzle are taken under both static and dynamic operating conditions with a Phase Doppler Anemometry system. The dynamic modulation is found to significantly impact the spray properties of both nozzles. / Master of Science

High-bandwidth fuel modulation is currently one of the most promising methods for active combustion control. To attenuate the large pressure oscillations in the combustion chamber, the fuel is pulsed so that the heat release rate fluctuations damp the pressure oscillations in the combustor. This thesis focuses on the development and implementation of a high-bandwidth, proportional modulation system for liquid-fuel active combustion control. The throttle valve modulation system, discussed in this thesis, uses a 500-um piezoelectric stack coupled with an off-the-shelf valve. After comparing three other types of actuators, the piezoelectric stack was selected because of its compact size, bandwidth capabilities, and relatively low cost. Using the acoustic resonance of the fuel line, the system is able to achieve 128% pressure modulation, relative to the mean pressure, and is capable of producing more than 75% flow modulation at 115 Hz. Additionally, at 760 Hz the system produces 40% pressure modulation and 21% flow modulation with flow rates between 0.4 and 10 gph. Control authority was demonstrated on a single-nozzle kerosene combustor which exhibits a well-pronounced instability at ~115 Hz. Using the modulation system, the fundamental peak of the combustion instability was reduced by 30 dB, and the broadband sound pressure levels inside the combustor were reduced by 12 dB. However, the most important conclusion from the combustion control experiments was not the system?s accomplishments, but rather its inability to control the combustor at high global equivalence ratios. Our work indicates that having the ability to modulate a large percentage of the primary fuel is not always sufficient for active combustion control. / Master of Science

The thermodynamic conditions for the behaviour of silicon in the lower part of the blast furnace have been the focus of the thesis. More specifically, the influences of temperature, carbon activity, total gas pressure and Fe reoxidation on silicon have been studied. Calculations show that an increased temperature gives higher equilibrium ratio between silicon in hot metal and slag. Furthermore, laboratory reduction studies shows that the carbon activity in the cohesive zone increase with an increased reduction time. Increased carbon activity will increase the equilibrium silicon content in liquid metal. Equilibrium calculations based on tapped hot metal and slag shows that the equilibrium silicon content of the liquid metal phase is higher than measured at tapping. Around the raceway area the equilibrium silicon content is very high. The high equilibrium silicon content makes it important to differ between the conditions under operation and the conditions of samples taken out of the blast furnace before studied. The equilibrium silicon content is strongly correlated to the CO gas partial pressure. Often this partial pressure is changed during sampling and cooling of samples. At tapping the equilibrium partial pressure of CO has been calculated to higher values than the total gas pressure inside the blast furnace. Metal droplets found in tapped slags are probably formed by reduction of FeO. In the periphery part of the lower part of the blast furnace, it is believed that mainly FeO oxidises silicon in hot metal. It is not expected that the metal droplets in the slag is formed if FeO oxidises dissolved silicon. Instead, the iron droplets may form at reactions with gas, coke carbon or coal powder carbon. Around some droplets increased magnesium content has been found. This may be due to reactions with gaseous magnesium that, according to thermodynamic conditions, is easy to form. It has been reported that much FeO may be formed in the raceway area. The metal droplets may indicate how much FeO that reacts with other components than liquid iron. The iron found in metal droplets in the slag corresponds to between 0.02 and 0.2 wt-% FeO in the slag.

Uma nova metodologia para a criação de mapas base de injeção eletrônica de combustível para motores de combustão interna de ignição a centelha é apresentada e seu comportamento é comparado com os resultados fornecidos pela metodologia MVEM. A partir da utilização de equacionamentos da literatura, é feita uma modelagem do ciclo ideal Otto para um motor genérico alternativo monocilíndrico de 500 cm³ de volume deslocado. É modelada também uma válvula do tipo borboleta genérica de 0,06 m³ de diâmetro que opera tanto em regime subsônico quanto sônico. A pressão à jusante da borboleta é calculada para aberturas de 5° a 88,64°. Os modelos são acoplados a partir da vazão mássica de ar admitida, que é o parâmetro principal, sendo programados e simulados usando o programa comercial EES. O mapa base de pressão por abertura de borboleta por rotação resultante mostra o detalhe de descontinuidade pelo uso das equações de vazão mássica juntamente com a imposta pelas equações de coeficiente de descarga, implicando na mudança brusca de valores de pressão calculados para a região de abertura menor que 20%. O mapa de vazão mássica de combustível por rotação e por abertura de borboleta para uma razão estequiométrica de 14,67 também é gerado. Nele é possível observar a demanda por vazão mássica de combustível para cada rotação e abertura da válvula borboleta mostrando o caminho a ser seguido pelo motor para que seja atingida a vazão mássica necessária para obter-se a relação ar/combustível desejada. A metodologia proposta gera mapas base de combustível para módulos de injeção eletrônica. Os resultados são apresentados na forma de gráficos. O modelo produz resultados satisfatórios, reproduzindo o comportamento da válvula borboleta, comparado com a literatura. / A new methodology for EMS base maps to the internal combustion spark ignition engines is presented. Its behavior is compared with results from the MVEM methodology. From the technical literature an ideal Otto cycle for a generic reciprocating single cylinder engine with 500 cm³ of displaced volume. Also, throttle valve with a diameter of 0.06 m of diameter operating in subsonic and sonic flow regime is modeled. The downstream pressure is calculated for throttle openings of 5° to 88.64°. The models are coupled using the engine air mass flow rate as the main parameter, being programmed and simulated using a commercial EES software. The base map of pressure versus throttle opening and engine speed shows the discontinuity detail imposed from the mass flow and discharge coefficient equations, resulting into a abrupt change of pressure values calculated for an opening region less than 20%. The fuel mass flow versus revolutions per minute versus throttle valve opening for stoichiometric air fuel ratio of 14.67 is also generated. In such map it is possible to show the fuel mass flow demand for each rotation and throttle opening showing the path to be followed by the engine to reach the mass air flow needed to reach the target air fuel ratio. This methodology generates base fuel maps for electronic fuel injection modules. The results are presented in graph forms. The model presents satisfactory results that reproduce the throttle valve behavior, compared to the literature.

Uma nova metodologia para a criação de mapas base de injeção eletrônica de combustível para motores de combustão interna de ignição a centelha é apresentada e seu comportamento é comparado com os resultados fornecidos pela metodologia MVEM. A partir da utilização de equacionamentos da literatura, é feita uma modelagem do ciclo ideal Otto para um motor genérico alternativo monocilíndrico de 500 cm³ de volume deslocado. É modelada também uma válvula do tipo borboleta genérica de 0,06 m³ de diâmetro que opera tanto em regime subsônico quanto sônico. A pressão à jusante da borboleta é calculada para aberturas de 5° a 88,64°. Os modelos são acoplados a partir da vazão mássica de ar admitida, que é o parâmetro principal, sendo programados e simulados usando o programa comercial EES. O mapa base de pressão por abertura de borboleta por rotação resultante mostra o detalhe de descontinuidade pelo uso das equações de vazão mássica juntamente com a imposta pelas equações de coeficiente de descarga, implicando na mudança brusca de valores de pressão calculados para a região de abertura menor que 20%. O mapa de vazão mássica de combustível por rotação e por abertura de borboleta para uma razão estequiométrica de 14,67 também é gerado. Nele é possível observar a demanda por vazão mássica de combustível para cada rotação e abertura da válvula borboleta mostrando o caminho a ser seguido pelo motor para que seja atingida a vazão mássica necessária para obter-se a relação ar/combustível desejada. A metodologia proposta gera mapas base de combustível para módulos de injeção eletrônica. Os resultados são apresentados na forma de gráficos. O modelo produz resultados satisfatórios, reproduzindo o comportamento da válvula borboleta, comparado com a literatura. / A new methodology for EMS base maps to the internal combustion spark ignition engines is presented. Its behavior is compared with results from the MVEM methodology. From the technical literature an ideal Otto cycle for a generic reciprocating single cylinder engine with 500 cm³ of displaced volume. Also, throttle valve with a diameter of 0.06 m of diameter operating in subsonic and sonic flow regime is modeled. The downstream pressure is calculated for throttle openings of 5° to 88.64°. The models are coupled using the engine air mass flow rate as the main parameter, being programmed and simulated using a commercial EES software. The base map of pressure versus throttle opening and engine speed shows the discontinuity detail imposed from the mass flow and discharge coefficient equations, resulting into a abrupt change of pressure values calculated for an opening region less than 20%. The fuel mass flow versus revolutions per minute versus throttle valve opening for stoichiometric air fuel ratio of 14.67 is also generated. In such map it is possible to show the fuel mass flow demand for each rotation and throttle opening showing the path to be followed by the engine to reach the mass air flow needed to reach the target air fuel ratio. This methodology generates base fuel maps for electronic fuel injection modules. The results are presented in graph forms. The model presents satisfactory results that reproduce the throttle valve behavior, compared to the literature.

Uma nova metodologia para a criação de mapas base de injeção eletrônica de combustível para motores de combustão interna de ignição a centelha é apresentada e seu comportamento é comparado com os resultados fornecidos pela metodologia MVEM. A partir da utilização de equacionamentos da literatura, é feita uma modelagem do ciclo ideal Otto para um motor genérico alternativo monocilíndrico de 500 cm³ de volume deslocado. É modelada também uma válvula do tipo borboleta genérica de 0,06 m³ de diâmetro que opera tanto em regime subsônico quanto sônico. A pressão à jusante da borboleta é calculada para aberturas de 5° a 88,64°. Os modelos são acoplados a partir da vazão mássica de ar admitida, que é o parâmetro principal, sendo programados e simulados usando o programa comercial EES. O mapa base de pressão por abertura de borboleta por rotação resultante mostra o detalhe de descontinuidade pelo uso das equações de vazão mássica juntamente com a imposta pelas equações de coeficiente de descarga, implicando na mudança brusca de valores de pressão calculados para a região de abertura menor que 20%. O mapa de vazão mássica de combustível por rotação e por abertura de borboleta para uma razão estequiométrica de 14,67 também é gerado. Nele é possível observar a demanda por vazão mássica de combustível para cada rotação e abertura da válvula borboleta mostrando o caminho a ser seguido pelo motor para que seja atingida a vazão mássica necessária para obter-se a relação ar/combustível desejada. A metodologia proposta gera mapas base de combustível para módulos de injeção eletrônica. Os resultados são apresentados na forma de gráficos. O modelo produz resultados satisfatórios, reproduzindo o comportamento da válvula borboleta, comparado com a literatura. / A new methodology for EMS base maps to the internal combustion spark ignition engines is presented. Its behavior is compared with results from the MVEM methodology. From the technical literature an ideal Otto cycle for a generic reciprocating single cylinder engine with 500 cm³ of displaced volume. Also, throttle valve with a diameter of 0.06 m of diameter operating in subsonic and sonic flow regime is modeled. The downstream pressure is calculated for throttle openings of 5° to 88.64°. The models are coupled using the engine air mass flow rate as the main parameter, being programmed and simulated using a commercial EES software. The base map of pressure versus throttle opening and engine speed shows the discontinuity detail imposed from the mass flow and discharge coefficient equations, resulting into a abrupt change of pressure values calculated for an opening region less than 20%. The fuel mass flow versus revolutions per minute versus throttle valve opening for stoichiometric air fuel ratio of 14.67 is also generated. In such map it is possible to show the fuel mass flow demand for each rotation and throttle opening showing the path to be followed by the engine to reach the mass air flow needed to reach the target air fuel ratio. This methodology generates base fuel maps for electronic fuel injection modules. The results are presented in graph forms. The model presents satisfactory results that reproduce the throttle valve behavior, compared to the literature.

Orientador: Paulo Roberto Mei / Dissertação (mestrado) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecânica / Made available in DSpace on 2018-08-19T00:26:25Z (GMT). No. of bitstreams: 1 Belloto_HumbertoJesuino_M.pdf: 5308190 bytes, checksum: 1a5267190a7db08ed3b659370b64f95a (MD5) Previous issue date: 2011 / Resumo: O tubo de aço carbono com alto teor de manganês St52 (Norma DIN 1.0580) sem costura, com 8 mm de diâmetro externo e 3 mm de diâmetro interno, atualmente utilizado no sistema de combustível de motores eletrônicos a diesel com pressões de trabalho de até 1300 bar, apresentou problemas nos testes de durabilidade. O rompimento do tubo foi consequência das trincas internas originadas no processo de laminação, denominadas descontinuidades. O tubo de fabricação nacional, atualmente utilizado nos motores, foi comparado com um importado e os resultados dos testes encontrados determinaram qual deles teria maior vida à fadiga. São apresentados nesta dissertação o processo de fabricação do tubo com as suas vulnerabilidades, os testes de fadiga comparando as durabilidades dos tubos nacionais e importados, o efeito do processo de autofretagem e os ensaios metalográficos. Os resultados levaram a concluir que o tubo nacional não atende as solicitações de trabalho do motor e a solução imediata é a utilização do tubo importado. A recomendação para trabalhos futuros seria o estudo de melhoria no processo de laminação para diminuição do nível de descontinuidades internas tubos nacionais / Abstract: The carbon steel with high manganese in accordance with Din 1.0580 (St52) seamless 8 x 3 mm diameter has been used into fuel injection system of the electronic diesel king with pressure up to 1300 bar. This tube presented short life on durability tests due to inner cracks created during rolling process. The tube produced in Brazil and used nowadays in was compared with an imported one using a fatigue test. It is shown on this work the manufacturing tube process, the fatigue test applied to the national and imported tubes and the e effects. The results showed that the national tube does not meet the necessary requirements and the immediate solution is to use the imported one. It is recommended further used on the rolling process to reduce the internal roughness of the tubes produced in Brazil / Mestrado / Materiais e Processos de Fabricação / Mestre em Engenharia Mecânica

[ES] La inyección de combustible es, entre los temas de investigación de motores, una de las piezas críticas para obtener un motor eficiente. El papel es aún más significativo cuando se persigue una estrategia de inyección directa. La geometría interna y el movimiento de la aguja determinan el comportamiento del flujo del inyector, que se sabe que afecta enormemente al desarrollo externo del spray y, en última instancia, al rendimiento de la combustión dentro de la cámara. La conciencia sobre el cambio climático y los contaminantes ha ido creciendo, impulsando el esfuerzo en motores más limpios. En este sentido, los motores de gasolina tienen un margen más amplio para mejo- rar que los motores diesel. La evolución de los antiguos PFI a las modernas estrategias de inyección directa, que se utilizan en los motores de nueva generación, demuestra esta tendencia. Los sistemas GDI tienen el potencial de cumplir con las estrictas emisiones y aumentar el ahorro de combustible, sin embargo, todavía se enfrenta a muchos desafíos. Este trabajo implica el uso de dos inyectores, uno es una moderna tobera de GDI de investigación designada por el Engine Combustion Network (ECN), y el otro es una unidad de inyección de producción (PIU) con la misma tecnología y una geometría ligeramente diferente. Ambos equipos se someten a una completa caracterización (flujo interno y externo) que abarca las técnicas más avanzadas en diversas instalaciones experimentales. Además, se diseña y construye una nueva instalación para realizar experimentos en condiciones de evaporación instantánea (cuando la presión de vapor del combustible inyectado es superior a la presión del volumen de descarga). La instalación construida está diseñada para simular un ambiente de descarga en ciertas condiciones del motor en las que podrían producirse fenómenos de flash boiling. Así, debido a las propiedades típicas del combustible de gasolina, era un requisito operar con presiones de cámara de 0,2 a 15 bares. Además, la temperatura ambiente se controlaba mediante la implementación de una resistencia que puede calentar el gas ambiente. La instalación funciona en un bucle abierto, pudiendo renovar el volumen de gas entre las inyecciones. Por último, se construyeron tres amplios accesos ópticos para acomodar muchas técnicas de diagnóstico óptico como DBI, MIE, shadowgraphy o PDA, entre otros. Para la evaluación del flujo interno se determinó la geometría de las toberas y la orientación de los agujeros, el movimiento de la aguja y, por último, la caracterización del ratio de inyección (ROM) y el momento de inyección (ROI) de ambas toberas. La geometría de las toberas y la elevación de la aguja se midieron mediante técnicas avanzadas de rayos X en el Laboratorio Nacional de Argonne (ANL). Las mediciones de ROI y ROM se realizaron utilizando las instalaciones de CMT-Motores Térmicos siguiendo los conocimientos técnicos aplicados en los inyectores de gasóleo y adaptándolos a las toberas de GDI. El ROI nos permitió comparar las boquillas, cuyo número de orificios y geometría eran diferentes, aunque entregan aproximadamente la misma cantidad de combustible. Se ensayó la respuesta a condiciones típicas de motor como variaciones en la presión del rail, la presión de descarga, la temperatura del combustible, etc. Para el inyector de investigación "Spray G", se desarrolló un modelo 0-D de la velocidad de inyección que permite obtener la señal para diferentes condiciones y duración de la inyección, lo cual es útil para la calibración del motor y la validación del CFD. Además, para la caracterización de la ROM, se desarrolló la metodología de la técnica de deformación plástica para obtener la orientación del cono del spray y orientar adecuadamente los chorros de combustible para la medición de ROM. En el análisis hidráulico se combinaron los datos para estudiar los bajos valores del coeficiente de descarga y / [CA] La injecció de combustible és, entre els temes d'investigació de motors, una de les peces crítiques per a obtindre un motor eficient. El paper és encara més significatiu quan es persegueix una estratègia d'injecció directa. La geometria interna i el moviment de l'agulla determinen el comportament del flux de l'injector, que se sap que afecta enormement el desenvolupament extern de l'esprai i, en última instància, al rendiment de la combustió dins de la cambra. La consciència sobre el canvi climàtic i els contaminants ha anat creixent, impulsant l'esforç en motors més nets. En aquest sentit, els motors de gasolina tenen un marge més ampli per a millorar que els motors dièsel. L'evolució dels antics PFI a les modernes estratègies d'injecció directa, que s'utilitzen en els motors de nova generació, demostra aquesta tendència. Els sistemes GDI tenen el potencial de complir amb les estrictes emissions i aug- mentar l'estalvi de combustible, no obstant això, encara s'enfronta a molts desafiaments. Aquest treball implica l'ús de dos injectors, un és una moderna tovera de GDI d'investigació designada pel Engine Combustion Network (ECN), i l'altre és una unitat d'injecció de producció (PIU) amb la mateixa tecnologia i una geometria lleugerament diferent. Tots dos equips se sotmeten a una completa caracterització (flux intern i extern) que abasta les tècniques més avançades en diverses instal·lacions experimentals. A més, es dissenya i construeix una nova instal·lació per a realitzar experiments en condicions d'evaporació instantània (quan la pressió de vapor del combustible injectat és superior a la pressió del volum de descàrrega). La instal·lació construïda està dissenyada per a simular un ambient de descàrrega en certes condicions del motor en les quals podrien produir-se fenòmens de flash boiling. Així, a causa de les propietats típiques del combustible de gasolina, era un requisit operar amb pressions de cambra de 0,2 a 15 bars. A més, la temperatura ambient es controlava mitjançant la implementació d'una resistència que pot calfar el gas ambiente. La instal·lació funciona en un bucle obert, podent renovar el volum de gas entre les injeccions. Finalment, es van construir tres amplis accessos òptics per a acomodar moltes tècniques de diagnòstic òptic com DBI, MIE, shadowgraphy o PDA, entre altres. Per a l'avaluació del flux intern es va determinar la geometria de les toveres i l'orientació dels forats, el moviment de l'agulla i, finalment, la caracterització del ràtio d'injecció (ROM) i el moment d'injecció (ROI) de totes dues toveres. La geometria de les toveres i l'elevació de l'agulla es van mesurar mitjançant tècniques avançades de raigs X en el Laboratori Nacional de Argonne (ANL). Els mesuraments de ROI i ROM es van realitzar utilitzant les instal·lacions de CMT-Motores Térmicos seguint els coneixements tècnics aplicats en els injectors de gasoil i adaptant-los a les toveres de GDI. El ROI ens va permetre comparar els filtres, el nombre d'orificis dels quals i geometria eren diferents, encara que entreguen aproximadament la mateixa quantitat de combustible. Es va assajar la resposta a condicions típiques de motor com a variacions en la pressió del rail, la pressió de descàrrega, la temperatura del combustible, etc. Per a l'injector d'investigació "Esprai G", es va desenvolupar un model 0-D de la velocitat d'injecció que permet obtindre el senyal per a diferents condicions i duració de la injecció, la qual cosa és útil per al calibratge del motor i la validació del CFD. A més, per a la caracterització de la ROM, es va desenvolupar la metodologia de la tècnica de deformació plàstica per a obtindre l'orientació del con de l'esprai i orientar adequadament els dolls de combustible per al mesurament de ROM. En l'anàlisi hidràulica es van combinar les dades per a estudiar els baixos valors del coeficient de descàrrega i del coeficient d'àr / [EN] Fuel injection is among the engine research topics one of the critical pieces to obtain an efficient engine. The role is even more significant when a direct injection strategy is pursued. The internal geometry and pintle movement determine the injector flow behavior, which is known to hugely affect the external spray development and, ultimately, the combustion performance inside the chamber. Climate change and pollutants awareness has been growing, pushing forward the effort on cleaner engines. In this regard, gasoline en- gines have a wider margin to improve than diesel engines. The evolution from old Port Fuel Injectors to modern direct injection strategies, which are used in new generation engines, demonstrates this trend. GDI systems have the potential to comply with stringent emissions and increase fuel economy, however, it still faces many challenges. This work involves the use of two injectors, one is a modern research GDI nozzle appointed by the Engine Combustion Network (ECN), and the other is a production injector unit (PIU) with the same technology and slightly different geometry. Both hardware's undergo a complete characterization (internal and external flow) covering the state- of-the-art techniques in various experimental facilities. Furthermore, a new facility is designed and built to perform experiments under flash boiling conditions (when the fuel injected's vapor pressure is higher than the pressure in the discharge volume). The developed facility is designed to simulate a discharge ambient at certain engine conditions in which flash boiling phenomena could occur. Thus, due to typical gasoline fuel properties, it was a requirement to operate from chamber pressures from 0.2 bar to 15 bar. Also, the ambient temperature was controlled by implementing a resistor that can heat the ambient gas. The facility operates in an open loop, being able to renovate the gas volume between injections. Finally, three wide optical accesses were built to accommodate many optical diagnostic techniques such as DBI, MIE, shadowgraphy, or PDA, among others. For the internal flow description, it was determined the nozzles geometry and holes orientation, the pintle movement, and finally, the characterization of the rate of momentum (ROM) and rate of injection (ROI) of both nozzles. The nozzles geometry and needle lift were measured using advanced optical x-ray techniques at Argonne National Laboratory (ANL). The ROI and ROM measurements were performed using CMT-Motores Térmicos facilities follow- ing the know-how applied in diesel injectors and adapting it to GDI nozzles. The ROI allowed us to compare the nozzles, whose orifices number and geometry were different, although they deliver approximately the same amount of fuel. It was tested their response to typical boundary conditions such as rail pressure, discharge pressure, fuel temperature, etc. For the research nozzle "Spray G", it was developed a 0-D model of the rate of injection allowing to obtain the signal for different injection duration and conditions, which is useful in engine calibration and CFD validation. Furthermore, for the ROM characterization, the plastic deformation technique methodology was developed to obtain spray cone orientation and adequately guide the fuel jets for measuring ROM. The hydraulic analysis combined the data to study the low discharge coefficient and area coefficient values, which could result from low needle lift combined with novel hole designs in both nozzles that promote cavitation and air interaction from inside the orifice. In the external flow characterization, it was used the new developed vessel to study the external spray covering flash boiling conditions. It was employed four surrogate fuels to simulate different volatility properties of gasoline com- pounds and ultimately reproduce more extreme flashing conditions. It was used lateral visualization using DBI and Schlieren in addition to frontal MIE visualization. Some of t / Bautista Rodríguez, A. (2021). Study of the Gasoline Direct Injection Process under Novel Operating Conditions [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/167809 / TESIS

Recent imaging studies have provided a new conceptual model of the internal structure of direct injection diesel fuel jets as well as empirical correlations predicting jet development and structure. This information was used to create a diesel cycle simulation model using C language including compression, fuel injection and combustion, and expansion processes. Empirical relationships were used to create a new mixing-limited zero-dimensional model of the diesel combustion process. During fuel injection five zones were created to model the reacting fuel jet: 1) liquid phase fuel 2) vapor phase fuel 3) rich premixed products 4) diffusion flame sheath 5) surrounding bulk gas. Temperature and composition in each zone is calculated. Composition in combusting zones was calculated using an equilibrium model that includes 21 species. Sub models for ignition delay, premixed burn duration, heat release rate, and heat transfer were also included. Apparent heat release rate results of the model were compared with data from a constant volume combustion vessel and two single-cylinder direct injection diesel engines. The modeled heat release results included all basic features of diesel combustion. Expected trends were seen in the ignition delay and premixed burn model studies, but the model is not predictive. The rise in heat release rate due to the diffusion burn is over-predicted in all cases. The shape of the heat release rate for the constant volume chamber is well characterized by the model, as is the peak heat release rate. The shape produced for the diffusion burn in the engine cases is not correct. The injector in the combustion vessel has a single nozzle and greater distance to the wall reducing or eliminating wall effects and jet interaction effects. Interactions between jets and the use of a spray penetration correlation developed for non-reacting jets contribute to inaccuracies in the model.