HIGH INJECTION PRESSURE IMPINGING DIESEL SPRAY CHARACTERISTICS AND SUBSEQUENT SOOT FORMATION IN REACTING CONDITIONS

The spray impingement in diesel engines attracts the attention of engine researchers in recent decades as the physical size of the engine is reduced. Due to the spray impingement, the atomization, vaporizing and air-fuel mixing quality is altered compared to a free spray. For emission control, soot is one of the major particulate emissions from diesel combustion and its formation in an impinged spray is worthy to be investigated. Firstly, to understand the impinged spray characteristics, the experiments for both non-vaporizing and reacting conditions were conducted in a constant volume combustion vessel. The impinged spray was captured by a high-speed camera and the instantaneous spray propagation distance and rate were obtained. For a better understanding, the microscopic behavior of the spray propagation, the curvature of the impinged spray was calculated and a relationship between local fuel distribution and soot formation was found. After that, the apparent heat release rate from an impinge spray combustion and the heat flux through the impingement were analyzed. The apparent heat release rate was obtained by the internal chamber pressure and the heat flux was measured by heat flux probes embedded in the impinging plate. Then, the soot formation of an impinged spray was both studied from experiments and simulations. In the experiments, the natural luminosity mainly due to the incandescence of soot particles was captured by the high-speed camera. A computational fluid dynamics (CFD) approach was adopted to quantitatively study the soot formation in terms of absolute soot mass and soot mass fractions in the vicinity of the wall. In the last, the film formation under different ambient temperatures, impinging distances, and oxygen concentration was investigated in terms of film area and thickness. The impact of film formation on the soot outcomes was then investigated by comparing the rate of film vaporization and soot formation. To summarize, the main goal of this dissertation is going to benefit the understanding of the impinged spray in reacting diesel-relevant engine conditions. From experiments, a global view of soot formation in an impinged spray was analyzed and the mechanism of soot formation was further revealed by the CFD simulations

Computational study on the non-reacting flow in Lean Direct Injection gas turbine combustors through Eulerian-Lagrangian Large-Eddy Simulations

[ES] El principal desafío en los motores turbina de gas empleados en aviación reside en aumentar la eficiencia del ciclo termodinámico manteniendo las emisiones contaminantes por debajo de las rigurosas restricciones. Ésto ha conllevado la necesidad de diseñar nuevas estrategias de inyección/combustión que operan en puntos de operación peligrosos por su cercanía al límite inferior de apagado de llama. En este contexto, el concepto Lean Direct Injection (LDI) ha emergido como una tecnología prometedora a la hora de reducir los óxidos de nitrógeno (NOx) emitidos por las plantas propulsoras de los aviones de nueva generación. En este contexto, la presente tesis tiene como objetivos contribuir al conocimiento de los mecanismos físicos que rigen el comportamiento de un quemador LDI y proporcionar herramientas de análisis para una profunda caracterización de las complejas estructuras de flujo de turbulento generadas en el interior de la cámara de combustión. Para ello, se ha desarrollado una metodología numérica basada en CFD capaz de modelar el flujo bifásico no reactivo en el interior de un quemador LDI académico mediante enfoques de turbulencia U-RANS y LES en un marco Euleriano-Lagrangiano. La resolución numérica de este problema multi-escala se aborda mediante la descripción completa del flujo a lo largo de todos los elementos que constituyen la maqueta experimental, incluyendo su paso por el swirler y entrada a la cámara de combustión. Ésto se lleva a cabo través de dos códigos CFD que involucran dos estrategias de mallado diferentes: una basada en algoritmos de generación y refinamiento automático de la malla (AMR) a través de CONVERGE y otra técnica de mallado estático más tradicional mediante OpenFOAM. Por un lado, se ha definido una metodología para obtener una estrategia de mallado óptima mediante el uso del AMR y se han explotado sus beneficios frente a los enfoques tradicionales de malla estática. De esta forma, se ha demostrado que la aplicabilidad de las herramientas de control de malla disponibles en CONVERGE como el refinamiento fijo (fixed embedding) y el AMR son una opción muy interesante para afrontar este tipo de problemas multi-escala. Los resultados destacan una optimización del uso de los recursos computacionales y una mayor precisión en las simulaciones realizadas con la metodología presentada. Por otro lado, el uso de herramientas CFD se ha combinado con la aplicación de técnicas de descomposición modal avanzadas (Proper Orthogonal Decomposition and Dynamic Mode Decomposition). La identificación numérica de los principales modos acústicos en la cámara de combustión ha demostrado el potencial de estas herramientas al permitir caracterizar las estructuras de flujo coherentes generadas como consecuencia de la rotura de los vórtices (VBB) y de los chorros fuertemente torbellinados presentes en el quemador LDI. Además, la implementación de estos procedimientos matemáticos ha permitido tanto recuperar información sobre las características de la dinámica de flujo como proporcionar un enfoque sistemático para identificar los principales mecanismos que sustentan las inestabilidades en la cámara de combustión. Finalmente, la metodología validada ha sido explotada a través de un Diseño de Experimentos (DoE) para cuantificar la influencia de los factores críticos de diseño en el flujo no reactivo. De esta manera, se ha evaluado la contribución individual de algunos parámetros funcionales (el número de palas del swirler, el ángulo de dichas palas, el ancho de la cámara de combustión y la posición axial del orificio del inyector) en los patrones del campo fluido, la distribución del tamaño de gotas del combustible líquido y la aparición de inestabilidades en la cámara de combustión a través de una matriz ortogonal L9 de Taguchi. Este estudio estadístico supone un punto de partida para posteriores estudios de inyección, atomización y combus[CA] El principal desafiament als motors turbina de gas utilitzats a la aviació resideix en augmentar l'eficiència del cicle termodinàmic mantenint les emissions contaminants per davall de les rigoroses restriccions. Aquest fet comporta la necessitat de dissenyar noves estratègies d'injecció/combustió que radiquen en punts d'operació perillosos per la seva aproximació al límit inferior d'apagat de flama. En aquest context, el concepte Lean Direct Injection (LDI) sorgeix com a eina innovadora a l'hora de reduir els òxids de nitrogen (NOx) emesos per les plantes propulsores dels avions de nova generació. Sota aquest context, aquesta tesis té com a objectius contribuir al coneixement dels mecanismes físics que regeixen el comportament d'un cremador LDI i proporcionar ferramentes d'anàlisi per a una profunda caracterització de les complexes estructures de flux turbulent generades a l'interior de la càmera de combustió. Per tal de dur-ho a terme s'ha desenvolupat una metodología numèrica basada en CFD capaç de modelar el flux bifàsic no reactiu a l'interior d'un cremador LDI acadèmic mitjançant els enfocaments de turbulència U-RANS i LES en un marc Eulerià-Lagrangià. La resolució numèrica d'aquest problema multiescala s'aborda mitjançant la resolució completa del flux al llarg de tots els elements que constitueixen la maqueta experimental, incloent el seu pas pel swirler i l'entrada a la càmera de combustió. Açò es duu a terme a través de dos codis CFD que involucren estratègies de mallat diferents: una basada en la generación automàtica de la malla i en l'algoritme de refinament adaptatiu (AMR) amb CONVERGE i l'altra que es basa en una tècnica de mallat estàtic més tradicional amb OpenFOAM. D'una banda, s'ha definit una metodologia per tal d'obtindre una estrategia de mallat òptima mitjançant l'ús de l'AMR i s'han explotat els seus beneficis front als enfocaments tradicionals de malla estàtica. D'aquesta forma, s'ha demostrat que l'aplicabilitat de les ferramente de control de malla disponibles en CONVERGE com el refinament fixe (fixed embedding) i l'AMR són una opció molt interessant per tal d'afrontar aquest tipus de problemes multiescala. Els resultats destaquen una optimització de l'ús dels recursos computacionals i una major precisió en les simulacions realitzades amb la metodologia presentada. D'altra banda, l'ús d'eines CFD s'ha combinat amb l'aplicació de tècniques de descomposició modal avançades (Proper Orthogonal Decomposition and Dynamic Mode Decomposition). La identificació numèrica dels principals modes acústics a la càmera de combustió ha demostrat el potencial d'aquestes ferramentes al permetre caracteritzar les estructures de flux coherents generades com a conseqüència del trencament dels vòrtex (VBB) i dels raigs fortament arremolinats presents al cremador LDI. A més, la implantació d'estos procediments matemàtics ha permès recuperar informació sobre les característiques de la dinàmica del flux i proporcionar un enfocament sistemàtic per tal d'identificar els principals mecanismes que sustenten les inestabilitats a la càmera de combustió. Finalment, la metodologia validada ha sigut explotada a traves d'un Diseny d'Experiments (DoE) per tal de quantificar la influència dels factors crítics de disseny en el flux no reactiu. D'aquesta manera, s'ha avaluat la contribución individual d'alguns paràmetres funcionals (el nombre de pales del swirler, l'angle de les pales, l'amplada de la càmera de combustió i la posició axial de l'orifici de l'injector) en els patrons del camp fluid, la distribució de la mida de gotes del combustible líquid i l'aparició d'inestabilitats en la càmera de combustió mitjançant una matriu ortogonal L9 de Taguchi. Aquest estudi estadístic és un bon punt de partida per a futurs estudis de injecció, atomització i combustió en cremadors LDI.[EN] Aeronautical gas turbine engines present the main challenge of increasing the efficiency of the cycle while keeping the pollutant emissions below stringent restrictions. This has led to the design of new injection-combustion strategies working on more risky and problematic operating points such as those close to the lean extinction limit. In this context, the Lean Direct Injection (LDI) concept has emerged as a promising technology to reduce oxides of nitrogen (NOx) for next-generation aircraft power plants In this context, this thesis aims at contributing to the knowledge of the governing physical mechanisms within an LDI burner and to provide analysis tools for a deep characterisation of such complex flows. In order to do so, a numerical CFD methodology capable of reliably modelling the 2-phase nonreacting flow in an academic LDI burner has been developed in an Eulerian-Lagrangian framework, using the U-RANS and LES turbulence approaches. The LDI combustor taken as a reference to carry out the investigation is the laboratory-scale swirled-stabilised CORIA Spray Burner. The multi-scale problem is addressed by solving the complete inlet flow path through the swirl vanes and the combustor through two different CFD codes involving two different meshing strategies: an automatic mesh generation with adaptive mesh refinement (AMR) algorithm through CONVERGE and a more traditional static meshing technique in OpenFOAM. On the one hand, a methodology to obtain an optimal mesh strategy using AMR has been defined, and its benefits against traditional fixed mesh approaches have been exploited. In this way, the applicability of grid control tools available in CONVERGE such as fixed embedding and AMR has been demonstrated to be an interesting option to face this type of multi-scale problem. The results highlight an optimisation of the use of the computational resources and better accuracy in the simulations carried out with the presented methodology. On the other hand, the use of CFD tools has been combined with the application of systematic advanced modal decomposition techniques (i.e., Proper Orthogonal Decomposition and Dynamic Mode Decomposition). The numerical identification of the main acoustic modes in the chamber have proved their potential when studying the characteristics of the most powerful coherent flow structures of strongly swirled jets in a LDI burner undergoing vortex breakdown (VBB). Besides, the implementation of these mathematical procedures has allowed both retrieving information about the flow dynamics features and providing a systematic approach to identify the main mechanisms that sustain instabilities in the combustor. Last, this analysis has also allowed identifying some key features of swirl spray systems such as the complex pulsating, intermittent and cyclical spatial patterns related to the Precessing Vortex Core (PVC). Finally, the validated methodology is exploited through a Design of Experiments (DoE) to quantify the influence of critical design factors on the non-reacting flow. In this way, the individual contribution of some functional parameters (namely the number of swirler vanes, the swirler vane angle, the combustion chamber width and the axial position of the nozzle tip) into both the flow field pattern, the spray size distribution and the occurrence of instabilities in the combustion chamber are evaluated throughout a Taguchi's orthogonal array L9. Such a statistical study has supposed a good starting point for subsequent studies of injection, atomisation and combustion on LDI burners.Belmar Gil, M. (2020). Computational study on the non-reacting flow in Lean Direct Injection gas turbine combustors through Eulerian-Lagrangian Large-Eddy Simulations [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/159882TESI

Internal flow and spray characteristics of an outwards opening pintle-type gasoline-injector

The focus of the present study was on the spray characterization of an outwards opening pintle-type injector to be used for spray-guided direct injection spark-ignition (DISI) engines. This spray-guided approach requires excellent spray performance and stability over a wide range of operating conditions. To achieve these goals it is necessary to have a good understanding of the internal nozzle flow and its link with the spray characteristics. In particular, the knowledge of the in-nozzle two-phase flow structure (air entrainment and cavitation), the spray development (spray angle, penetration and recirculation zones) and droplets velocity and size distribution is essential. Therefore, this study was planned and carried out in three main phases: The first phase of the investigation was focused on a comprehensive study of the internal flow of the injector in order to understand not well-clarified flow/spray phenomena such as the longitudinal string formation and the spray-to-spray variation (flapping) which play a very important role in the behaviour of the overall spray-guided DISI system. To overcome the problems related to the small dimension of the injector and its optical accessibility, an enlarged transparent model about 23 times the real size injector was manufactured. Quantitative flow analysis performed with the Laser Doppler Velocimetry (LDV) technique was matched with 3D Mie scattering visualization to provide full information about the internal flow behaviour and allow correlation of the flow upstream and downstream of the nozzle exit. The flow between the needle guide and the nozzle seat in the enlarged injector consisted of four liquid jets and four pairs of unstable counter rotating vortices which were found to be responsible for the tangential oscillation of the flow downstream of the nozzle exit. The emerging hollow cone spray exhibited a string type structure similar to that of the real size injector with the string spacing depending on the flow velocity. The origin of these strings has been attributed to the formation of a two-phase flow inside the nozzle due to flow separation just upstream of the nozzle exit giving rise to air entrainment in the form of small bubbles. The presence of these bubbles in the nozzle outlet was correlated with the exiting flow and the formation of large longitudinal strings. The initiation and development of cavitation at the nozzle seat was also identified and was found to enhance the spray breakup and droplet atomisation. The second part of the investigation was focused on the spray characterization of the real size injector by 3D Mie scattering visualization and a parametric study of the velocity field and droplet size by Phase Doppler Anemometry (PDA), Particle Image Velocimetry (PIV) and LDV measurements. The post processed data have characterised the string-to-string velocity a droplet size distribution as a function of injection and backpressure, injection duration, chamber temperature and pintle needle lift. An alternative arrangement set up made it possible to overcome problems associated with the signal attenuation due to the high spray density and also allow characterisation of the internal and external spray recirculations where ignition takes place. By introducing very low velocity atomized water mist against the spray, the velocity field of the air entrainment around the nozzle exit of the injector was measured and showed the flow development during the spray injection process which may influence the string instability and contribute to the primary droplet break up phenomenon. Validation of the results concerning recirculation and air entrainment was obtained by a PIV investigation. The performance of three prototype pintle-type injectors having different nozzle exit designs was investigated and, in particular, the interaction of the spray with the in-cylinder flow was observed by mounting the injectors in an optical engine and visualizing the effects of the injection and engine parameters on the spray stability, spray angle variation and spray flow recirculation. Overall, the classification of the three prototypes has shown that the Inward Seal Band positive step design produced the most robust spray angle which is ideally suited for stratified fuel mixture formation in spray-guided configurations for DISI engines which offer promise for outstanding efficiency and reduced C02 emissions, approaching the levels of passenger car diesels

Laser induced incandescence and high speed imaging in hydra optical diesel engine

The aim of this thesis is to investigate ways to reduce soot emission from compression ignition engines by investigating the combustion processes within the diesel engine. The approach is to include computational and experimental work. In order to investigate the trade-off between the amount and stratification of the premixing and the consequent rate of pressure rise, and in particular the effects of changing the autoignition properties of the fuel blend, a multizone code capable of representing the ignition of a premixed charge consequent on multiple injection of fuel is presented. As part of this investigation, this thesis began the process of looking into the potential of gasoline fuel. Experimentally, investigations of soot distribution were carried out in an optically-accessed single cylinder “Hydra” engine. The soot was visualized using high speed imaging and laser induced incandescence in the optical engine to look at the effect of injection pressure on combustion luminosity and soot distribution. An extensive parametric study was carried out on the Hydra engine to look at the effect of engine load, injection timing and pressure, number of injections, intake temperature and combustion phasing. High speed imaging was carried out to measure injection tip penetration and soot luminosity as a function injection pressure. The combustion luminosity was studied, with proper orthogonal decomposition (POD) analysis, at different injection pressures. It was found that increase of injection pressure decreases combustion luminosity. The technique of laser induced incandescence (LII) was used to visualize the soot. As a preliminary to the use of the LII in the engine, fundamental work on the technique itself was carried out at Heriot-Watt University to isolate the radiative emission component of heat loss from the soot and measure the complex refractive index of soot. Results on soot particle sizes were compared to scanning electron micrograph of the soot collected. The LII measurement was found to be much larger, due to the high signal to noise ratio and the bias towards detection of larger particles. The investigation also showed that the soot agglomerates could undergo micro-explosions on being exposed to laser irradiance. It is speculated that the soot molecules become ionized and mutually repel each other.Open Acces

高圧横風気流中で平板に衝突する燃料噴霧の特性

広島大学(Hiroshima University)博士(工学)Doctor of Engineeringdoctora

Numerical simulations of stationary and transient spray combustion for aircraft gas turbine applications

Le développement des turbines à gaz d’aviation actuelles et futures est principalement axé sur la sécurité, la performance, la minimisation de la consommation de l’énergie, et de plus en plus sur la réduction des émissions d’espèces polluantes. Ainsi, les phases de design de moteurs sont soumises auxaméliorations continues par des études expérimentales et numériques. La présente thèse se consacre à l’étude numérique des phases transitoires et stationnaires de la combustion au sein d’une turbine à gaz d’aviation opérant à divers modes de combustion. Une attention particulière est accordée à la précision des résultats, aux coûts de calcul, et à la facilité de manipulation de l’outil numérique d’un point de vue industriel. Un code de calcul commercial largement utilisé en industrie est donc choisi comme outil numérique. Une méthodologie de Mécanique des Fluides Numériques (MFN) constituée de modèles avancés de turbulence et de combustion jumelés avec un modèle d’allumage sous-maille, est formulé pour prédire les différentes phases de la séquence d’allumage sous différentes conditions d’allumage par temps froid et de rallumage en altitude, ainsi que les propriétés de la flamme en régime stationnaire. Dans un premier temps, l’attention est focalisée sur le régime de combustion stationnaire. Trois méthodologies MFN sont formulées en exploitant trois modèles de turbulence, notamment, le modèle basé sur les équations moyennées de Navier-Stokes instationnaires (URANS), l’adaptation aux échelles de l’écoulement (SAS), et sur la simulation aux grandes échelles (LES). Pour évaluer la pertinence de l’incorporation d’un modèle de chimie détaillée ainsi que celle des effets de chimie hors-équilibre, deux différentes hypothèses sont considérées : l’hypothèse de chimie-infiniment-rapide à travers le modèle d’équilibre-partiel, et l’hypothèse de chimie-finie via le modèle de flammelettes de diffusion. Pour chacune des deux hypothèses, un carburant à une composante, et un autre à deux composantes sont utilisés comme substituts du kérosène (Jet A-1). Les méthodologies MFN résultantes sont appliquées à une chambre de combustion dont l’écoulement est stabilisé par l’effet swirl afin d’évaluer l’aptitude de chacune d’elle à prédire les propriétés de combustion en régime stationnaire. Par la suite, les rapports entre le coût de calcul et la précision des résultats pour les trois méthodologies MFN formulées sont explicitement comparés. La deuxième étude intermédiaire est dédiée au régime de combustion transitoire, notamment à la séquence d’allumage précédant le régime de combustion stationnaire. Un brûleur de combustibles gazeux, muni d’une bougie d’allumage, et dont la flamme est stabilisée par un accroche-flamme, est utilisé pour calibrer le modèle MFN formulé. Ce brûleur, de géométrie relativement simple, peut aider à la compréhension des caractéristiques d’écoulements réactifs complexes, en l’occurrence l’allumabilité et la stabilité. La méthodologie MFN la plus robuste issue de la précédente étude est reconsidérée. Puisque le brûleur fonctionne en mode partiellement pré-mélangé, le modèle de combustion paramétré par la fraction de mélange et la variable de progrès est adopté avec les hypothèses de chimie-infiniment-rapide et de chimie-finie, respectivement à travers le modèle de Bray-Moss-Libby (BML) et un modèle de flammelettes multidimensionnel (FGM). Le modèle d’allumage sous-maille est préalablement ajusté via l’implémentation des propriétés de la flamme considérée. Par la suite, le modèle d’allumage est couplé au solveur LES, puis successivement aux modèles BML et FGM. Pour évaluer les capacités prédictives des méthodologies résultantes, ces dernières sont utilisées pour prédire les évènements d’allumage résultant d’un dépôt d’énergie par étincelles à diverses positions du brûleur, et les résultats sont qualitativement et quantitativement validés en comparant ceux-ci à leurs homologues expérimentaux. Finalement, la méthodologie MFN validée en configuration gazeuse est étendue à la combustion diphasique en la couplant au module de la phase liquide, et en incorporant les propriétés de la flamme de kérosène dans le modèle d’allumage. La méthodologie MFN résultant de cette adaptation, est préalablement appliquée à la chambre de combustion étudiée antérieurement, pour prédire la séquence d’allumage et améliorer les prédictions antérieures des propriétés de la flamme en régime stationnaire. Par la suite, elle est appliquée à une chambre de combustion plus réaliste pour prédire des évènements d’allumage sous différentes conditions d’allumage par temps froid, et de rallumage en altitude. L’aptitude de la nouvelle méthodologie MFN à prédire les deux types d’allumage considérés est mesurée quantitativement et qualitativement en confrontant les résultats des simulations numériques avec les enveloppes d’allumage expérimentales et les images d’une séquence d’allumage enregistrée avec une caméra infrarouge.The development of current and future aero gas turbine engines is mainly focused on the safety, the performance, the energy consumption, and increasingly on the reduction of pollutants and noise level. To this end, the engine’s design phases are subjected to improving processes continuously through experimental and numerical investigations. The present thesis is concerned with the simulation of transient and steady combustion regimes in an aircraft gas turbine operating under various combustion modes. Particular attention is paid to the accuracy of the results, the computational cost, and the ease of handling the numerical tool from an industrial standpoint. Thus, a commercial Computational Fluid Dynamics (CFD) code widely used in industry is selected as the numerical tool. A CFD methodology consisting of its advanced turbulence and combustion models, coupled with a subgrid spark-based ignition model, is formulated with the final goal of predicting the whole ignition sequence under cold start and altitude relight conditions, and the main flame trends in the steady combustion regime. At first, attention is focused on the steady combustion regime. Various CFD methodologies are formulated using three turbulence models, namely, the Unsteady Reynolds-Averaged Navier-Stokes (URANS), the Scale-Adaptive Simulation (SAS), and the Large Eddy Simulation (LES) models. To appraise the relevance of incorporating a realistic chemistry model and chemical non-equilibrium effects, two different assumptions are considered, namely, the infinitely-fast chemistry through the partial equilibrium model, and the finite-rate chemistry through the diffusion flamelet model. For each of the two assumptions, both one-component and two-component fuels are considered as surrogates for kerosene (Jet A-1). The resulting CFD models are applied to a swirl-stabilized combustion chamber to assess their ability to retrieve the spray flow and combustion properties in the steady combustion regime. Subsequently, the ratios between the accuracy of the results and the computational cost of the three CFD methodologies are explicitly compared. The second intermediate study is devoted to the ignition sequence preceding the steady combustion regime. A bluff-body stabilized burner based on gaseous fuel, and employing a spark-based igniter, is considered to calibrate the CFD model formulated. This burner of relatively simple geometry can provide greater understanding of complex reactive flow features, especially with regard to ignitability and stability. The most robust of the CFD methodologies formulated in the previous configuration is reconsidered. As this burner involves a partially-premixed combustion mode, a combustion model based on the mixture fraction-progress variable formulation is adopted with the assumptions of infinitely-fast chemistry and finite-rate chemistry through the Bray-Moss-Libby (BML) and Flamelet Generated Manifold (FGM) models, respectively. The ignition model is first customized by implementing the properties of the flame considered. Thereafter, the customized ignition model is coupled to the LES solver and combustion models based on the two above-listed assumptions. To assess the predictive capabilities of the resulting CFD methodologies, the latter are used to predict ignition events resulting from the spark deposition at various locations of the burner, and the results are quantitatively and qualitatively validated by comparing the latter to their experimental counterparts. Finally, the CFD methodology validated in the gaseous configuration is extended to spray combustion by first coupling the latter to the spray module, and by implementing the flame properties of kerosene in the ignition model. The resulting CFD model is first applied to the swirl-stabilized combustor investigated previously, with the aim of predicting the whole ignition sequence and improving the previous predictions of the combustion properties in the resulting steady regime. Subsequently, the CFD methodology is applied to a scaled can combustor with the aim of predicting ignition events under cold start and altitude relight operating conditions. The ability of the CFD methodology to predict ignition events under the two operating conditions is assessed by contrasting the numerical predictions to the corresponding experimental ignition envelopes. A qualitative validation of the ignition sequence is also done by comparing the numerical ignition sequence to the high-speed camera images of the corresponding ignition event

Multihole injectors for direct-injection gasoline engines

High-pressure multi-hole nozzles, carrying a Diesel-derived technology, are believed to be promising Fuel Injection Equipment (FIE) for Direct-Injection (DI) Spark Ignition (SI) gasoline engines. Having explored thoroughly swirl pressure atomisers and their spray behaviour, multi-hole nozzles represent the second-generation injectors. Thus, complete investigation of multi-hole nozzle flow, spray characteristics and their engine performance is a vital part of development of future DI gasoline engines. The internal nozzle flow of an enlarged transparent multi-hole injector was investigated for different flow rates and needle lifts under steady state flow conditions. High-resolution CCD camera and high speed digital video systems were employed to visualize the nozzle flow patterns and cavitation development. The images identified the onset of cavitation in multi-hole gasoline nozzles and revealed the transition from pre-film to film stage cavitation. Cavitation strings were also visualized inside the injection hole that could extend to the needle face. However, these structures are highly unstable and directly affected by needle lift and cavitation number, although it appeared to be independent of the Re, in a behaviour similar to that of multi-hole diesel injectors. The sprays from various high-pressure multi-hole nozzle designs injected into a high-pressure/temperature constant-volume chamber have been visualised and quantified in terms of droplet velocity and diameter with a two-component phase-Doppler Anemometry (PDA) system at injection pressures up to 200bar and chamber pressures varying from atmospheric to 12bar. The overall spray angles relative to the axis of the injector were found to be almost independent of injection and chamber pressure, a significant advantage relative to swirl pressure atomisers. Within the measured range, the effect of injection pressure on droplet size was rather small while the increase in chamber pressure from atmospheric to 12bar resulted in much smaller droplet velocities, by up to fourfold, and larger droplet sizes by up to 40%. The effect of chamber temperature on multi-hole sprays confirmed the expected trends that dictate smaller droplet size distributions as temperature rise from 50 to 90 and 120°C. Additionally, multiple-injection proved to have similar dependencies to the single injection with certain operating limits. Laser-induced fluorescence has been mainly used to characterise the two-dimensional fuel vapour concentration inside the cylinder of a multi-valve twin-spark ignition engine equipped with high-pressure multi-hole injectors. The effects of injection timing, in-cylinder charge motion and injector tip layout have been quantified. The flexibility in nozzle design of the multi-hole injectors has proven to be a powerful tool in terms of matching overall spray cone angle and number of holes to specific engine configurations. Injection timing was found to control spray impingement on the piston and cylinder wall, thus contributing to quick and efficient fuel evaporation. Multipleinjection performed well under certain operating conditions and proved to be a powerful tool in the hands of engine manufacturers. It was confirmed that in-cylinder charge motion plays a major role in engine's stable operation by assisting in the transportation of the air-fuel mixture towards the ignition locations (i.e. spark-plugs) in the way of a uniformly distributed charge or by preserving stratification of the charge depending on operating mode of the engine

Combustion characteristics of alternative liquid fuels

Envisaged application of biodiesel in gas turbine engines or furnaces requires extensive tests on the deflagration properties of biodiesel. The laminar flame speeds of Palm Methyl Esters (PME) and blends of PME with conventional fuels are determined using the jet-wall stagnation flame configuration. The same technique is also used to measure the laminar flame speed of diesel, Jet-A1, n-heptane, acetone, methane and methane/acetone. The spray atomization characteristics of a plain-jet airblast atomizer are investigated using a phase Doppler anemometry (PDA) under non-reacting conditions. The droplet size and velocity distribution of biodiesels are compared to conventional fuels. For spray combustion investigations, a generic gas turbine-type combustor is developed to compare the spray flame established from PME, rapeseed methyl esters (RME), diesel, Jet-A1 and biodiesel blends. The spray droplet characteristics in the flame and the flow field in the combustor are investigated. Chemiluminescence imaging of OH* and CH* are applied to capture the global flame structure and heat release region. Flame spectroscopy and long bandpass filtered imaging at > 550 nm are performed to evaluate the tendency of soot formation. In general, biodiesels exhibit flame shapes and spray droplet characteristics that are comparable to conventional fuels. In spite of the higher fuel specific consumption, the emission of NOx is found to be lower for biodiesels compared to conventional fuels. The results show that biodiesels can potentially be used as alternative fuels for gas turbine operation

Study of the Gasoline Direct Injection Process under Novel Operating Conditions

[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 tBautista 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/10251/167809TESI

Spray atomization of alternative fuels in medium speed diesel engines

Until today, the diesel engine is still the most important power source for heavy duty road & rail transport, marine, genset and agriculture applications. The decreasing reserves of fossil fuels, the strict emission regulations, the greenhouse effect, the increasing energy demand and fuel prices are all strong drivers for research into the use of alternative fuels in internal combustion engines. Potential alternative fuels for this application are straight vegetable oils and animal fats. Several manufacturers of medium speed diesel engines show interest. However, due to the difference in fuel properties problems due to the lack of knowledge still exists and engine modifications are required. The study focused on the understanding of the behavior of the fuel during injection in the engine. This was realized through both experimental and numerical work. For the experimental work, a constant volume combustion chamber, equipped with a medium speed diesel injection system, was developed and baptized as the Ghent University Combustion Chamber I (a.k.a. GUCCI). The setup allows the simulation of engine-like conditions and enables several optical diagnostics. Several boundary conditions were carefully analyzed and finally the influence of straight oil on the injection system and atomization were investigated in cold pressurized ambients. The numerical part consisted of the implementation of a spray model as sub-model for an engine simulation tool. The behavior of the model was evaluated for different commonly used diesel and biodiesel surrogates. The conclusions were used to make suggestions for oil surrogates. In a final step, the vaporizing spray model was validated with experiments that were conducted in the constant volume combustion chamber at the Technical University of Eindhoven. The setup conditions were taken as determined by the internationally established engine combustion network (ECN), making the results useful for comparison with similar setups and research at other institutions