CONCEPTUAL DESIGN, TESTING AND MANUFACTURING OF AN INDUSTRIAL TYPE ELECTRO-HYDRAULIC VACUUM SWEEPER SAHIN, Emre M.Sc., Department of Mechanical Engineering Supervisor : Prof. Dr. Kahraman ALBAYRAK Co-Supervisor: Prof. Dr. Bilgin KAFTANOGLU September 2011, 156 pages In this thesis, conceptual design, testing, development and manufacturing processes of the cleaning (elevator and fan system) and electro-hydraulic systems of an industrial type vacuum sweeper are presented. Thesis is financially supported by Ministry of Science, Industry and Technology (Turkey) and M&uuml / san A.S. (Makina &Uuml / retim Sanayi ve Ticaret A.S.) under the SAN-TEZ projects with numbers 00028.STZ.2007-1 and 00623.STZ.2010-1. The main purpose is to make critical design changes on existing fan system, designing a new elevator system and eventually obtaining efficient and powerful cleaning system. For design, Catia and SolidWorks softwares are used. Within the SAN-TEZ project, all CFD solutions were provided by Punto Engineering. Unlike many industrial type vacuum sweepers, new design will be electrically and electro-hydraulic controlled. All cleaning system of new &lsquo / M&Uuml / SAN Vacuum Sweeper&rsquo / will be activated by using hydraulic motors (traction system including hydraulic system is driven by the brushless DC electric motor as well) and the power of all these systems is supplied by batteries which are placed in the middle of the vehicle. Elevator and fan system can be considered as a group for a street sweeper for cleaning operations. Fan and elevator systems both gain an important place especially in cleaning operations due to lifting heavy and small particles from the ground. Fan system is used for sucking the small materials and dust by vacuum and elevator system is used to elevate heavier materials such stones, bottles, cans. Therefore, it is essential to design an efficient and powerful fan and elevator system for a street sweeper. The thesis work includes the design, development, supervision of manufacturing, simulation and testing of the cleaning (elevator and fan systems) and electro-hydraulic system of the street cleaners.

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior / Turbomáquinas são máquinas operacionais que transferem energia mecânica entre um rotor e um fluido. Estas máquinas têm muitas aplicações industriais. Um dos componentes de uma turbomáquina responsável pela transferência da energia, ou receber a rotação do eixo e transformar em energia de fluido em caso de bomba ou transferir a energia do fluido para o eixo em caso de uma turbina, é o impelidor ou rotor. O fenómeno da cavitação envolve escoamento bifásico: o líquido a ser bombeado e as bolhas de vapor que são formadas durante o processo de bombeamento. O processo de formação dessas bolhas é complexo, mas ocorre principalmente devido a presença de regiões de pressões muito baixas. O colapso dessas bolhas pode muitas vezes levar a deterioração do material, dependendo da intensidade ou da velocidade de colapso das bolhas. O principal objetivo deste trabalho foi estudar o comportamento hidrodinâmico do escoamento nos canais do impelidor de uma turbomáquina do tipo radial usando recursos de fluidodinâmica computacional (CFD). Uma abordagem Euler-Lagrange acoplada com o modelo da equação de Langevin foi empregada para estimar a trajetória das bolhas. Resultados das simulações mostram as particularidades de um escoamento líquido-bolha de vapor passando em um canal de geometria curva, fornecendo assim informações que podem nos ajudar na prevenção da cavitação nessas máquinas. / Turbomachines are operational machines that transfer mechanical energy between a rotor and a fluid. This type of machinery is employed in many industries. One of the main components of a turbomachine responsible for the energy transference, either receiving the rotation of the shaft and transforming it into fluid energy in the case of a pump or transferring energy from the fluid to the shaft in the case of a turbine, is the impeller or rotor. The cavitation phenomenon involves two-phase flow: the liquid to be pumped and the vapor bubbles which are formed during pumping. The formation process of these bubbles is complex, but occurs mainly due to the presence of regions of very low pressure. The collapse of the bubbles can often lead to a deterioration of the material, depending on the intensity or speed of bubbles collapse. The main objectives of this work was to study the hydrodynamic behavior of the flow in the impeller channels of a turbomachine (radial flow turbopump) using computational fluid dynamics (CFD resources). An Euler-Lagrange approach coupled with the Langevin equation model, was employed to estimate the bubbles tracking trajectory. Results of the simulations show the details of liquid-vapor bubble flow in a curved channel, providing insights that help us in the cavitation prevent of this machines.

The efficacy, reliability and versatility of the light emitting diode (LED) can outcompete most established light source technologies. However, they are particularly sensitive to high temperatures, which compromises their efficacy and reliability, undermining some of the technology s key benefits. Consequently, effective thermal management is essential to exploit the technology to its full potential. Thermal management is a well-established subject but its application in the relatively new LED lighting industry, with its specific constraints, is currently poorly defined. The question this thesis aims to answer is how can LED thermal management be achieved most effectively? This thesis starts with a review of the current state of the art, relevant thermal management technologies and market trends. This establishes current and future thermal management constraints in a commercial context. Methods to test and evaluate the thermal management performance of a luminaire system follow. The defined test methods, simulation benchmarks and operational constraints provide the foundation to develop effective thermal management strategies. Finally this work explores how the findings can be implemented in the development and comparison of multiple thermal management designs. These are optimised to assess the potential performance enhancement available when applied to a typical commercial system. The outcomes of this research showed that thermal management of LEDs can be expected to remain a key requirement but there are hints it is becoming less critical. The impacts of some common operating environments were studied, but appeared to have no significant effect on the thermal behaviour of a typical system. There are some active thermal management devices that warrant further attention, but passive systems are inherently well suited to LED luminaires and are readily adopted so were selected as the focus of this research. Using the techniques discussed in this thesis the performance of a commercially available component was evaluated. By optimising its geometry, a 5 % decrease in absolute thermal resistance or a 20 % increase in average heat transfer coefficient and 10 % reduction in heatsink mass can potentially be achieved . While greater lifecycle energy consumption savings were offered by minimising heatsink thermal resistance the most effective design was considered to be one optimised for maximum average heat transfer coefficient. Some more radical concepts were also considered. While these demonstrate the feasibility of passively manipulating fluid flow they had a detrimental impact on performance. Further analysis would be needed to conclusively dismiss these concepts but this work indicates there is very little potential in pursuing them further.

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior / Turbomáquinas são máquinas operacionais que transferem energia mecânica entre um rotor e um fluido. Estas máquinas têm muitas aplicações industriais. Um dos componentes de uma turbomáquina responsável pela transferência da energia, ou receber a rotação do eixo e transformar em energia de fluido em caso de bomba ou transferir a energia do fluido para o eixo em caso de uma turbina, é o impelidor ou rotor. O fenómeno da cavitação envolve escoamento bifásico: o líquido a ser bombeado e as bolhas de vapor que são formadas durante o processo de bombeamento. O processo de formação dessas bolhas é complexo, mas ocorre principalmente devido a presença de regiões de pressões muito baixas. O colapso dessas bolhas pode muitas vezes levar a deterioração do material, dependendo da intensidade ou da velocidade de colapso das bolhas. O principal objetivo deste trabalho foi estudar o comportamento hidrodinâmico do escoamento nos canais do impelidor de uma turbomáquina do tipo radial usando recursos de fluidodinâmica computacional (CFD). Uma abordagem Euler-Lagrange acoplada com o modelo da equação de Langevin foi empregada para estimar a trajetória das bolhas. Resultados das simulações mostram as particularidades de um escoamento líquido-bolha de vapor passando em um canal de geometria curva, fornecendo assim informações que podem nos ajudar na prevenção da cavitação nessas máquinas. / Turbomachines are operational machines that transfer mechanical energy between a rotor and a fluid. This type of machinery is employed in many industries. One of the main components of a turbomachine responsible for the energy transference, either receiving the rotation of the shaft and transforming it into fluid energy in the case of a pump or transferring energy from the fluid to the shaft in the case of a turbine, is the impeller or rotor. The cavitation phenomenon involves two-phase flow: the liquid to be pumped and the vapor bubbles which are formed during pumping. The formation process of these bubbles is complex, but occurs mainly due to the presence of regions of very low pressure. The collapse of the bubbles can often lead to a deterioration of the material, depending on the intensity or speed of bubbles collapse. The main objectives of this work was to study the hydrodynamic behavior of the flow in the impeller channels of a turbomachine (radial flow turbopump) using computational fluid dynamics (CFD resources). An Euler-Lagrange approach coupled with the Langevin equation model, was employed to estimate the bubbles tracking trajectory. Results of the simulations show the details of liquid-vapor bubble flow in a curved channel, providing insights that help us in the cavitation prevent of this machines.

A low-emissions power generator comprising a solid oxide fuel cell coupled to a gas turbine has been developed by Rolls-Royce Fuel Cell Systems. As part of the cycle, a fraction of the unreacted fuel (the off-gas) and oxidizer streams is reacted in a burner, which is the main source of pollutant formation. In this thesis a computational model of the burner has been developed which captures the formation of NOx and the oxidation of CO. This model gives accurate predictions at low computational cost, making it suitable for use as a design tool in future burner design optimization through parametric studies. A key factor in increasing computational efficiency was the development of a reduced H2/CO/N2 kinetic mechanism; from a starting mechanism of 30 species to 10 and 116 reactions to 6. The results of laminar opposed-flow diffusion flames have been used to validate the reduced mechanism. Several different turbulent combustion models have been evaluated by creating an interface between the reduced kinetic mechanism and the commercial CFD solver FLUENT. Comparison of model predictions with well-characterized turbulent syngas flames, which share a similar fuel composition to the experimental work conducted on the off-gas burner, shows acceptable agreement. These studies have demonstrated the sensitivity of modelling constants. Improved predictions were achieved by calibrating these constants and including radiative heat losses. Following suitable modification to reflect the predominantly laminar flow present in the current burner design, the relevant modelling approaches were applied to the off-gas burner. Comparison was made to previous detailed measurements, showing that the important trends of NOx and CO are captured in general. The model was extended to high pressure conditions, similar to those in the actual off-gas burner, with the emissions predictions within design limits. The outcome of this work is a fast, accurate design tool for CFD which has capabilities to simulate beyond the laminar burner studied here. It may be applied to more general types of off-gas/syngas burners where turbulence-chemistry interaction is expected to be more significant.

Since the very beginning of the development of computers they have been used to accelerate the knowledge gain in science and research. Today they are a core part of most research facilities. Especially in natural and technical sciences they are used to simulate processes that would be hard to observe in real world experiments. Together with measurements from such experiments, simulations produce huge amounts of data that have to be analyzed by researchers to gain new insights and develop their field of science.

Ventricle Assist Devices (VADs), which are typically either axial or centrifugal flow pumps implanted on the aortic arch, have been used to support patients who are awaiting cardiac transplantation. Success of the apparatus in the short term has led to long term use. Despite anticoagulation measures, blood clots (thrombi) have been known to form in the device itself or inside of the heart. The Ventricle Assist Devices supply blood flow via a conduit (cannula) implanted on the ascending aorta. Currently, the implantation angle of the VAD cannula is not taken into consideration. Since the VADs supply a significant amount of blood flow to the aorta, the implantation angle can greatly affect the trajectory of the formed thrombi as well as the cardiac flow field inside of the aortic arch. This study aims to vary the implantation angle of a pediatric Left Ventricle Assist Device (LVAD) through a series of computational fluid dynamics (CFD) software simulations focusing on the aortic arch and its branching arteries of a 20 kg pediatric patient in order to reduce the occurrence of stroke.

La Tesis Doctoral estudia el comportamiento de las emisiones de polvo generadas en las parvas ó sistemas de almacenamiento de minerales a la intemperie fundamentalmente en sistemas portuarios, en parques de centrales térmicas, cementeras y explotaciones mineras, para lograr la modelización del fenómeno de la puesta en suspensión de partículas sólidas y su propagación, evaluar las variables que en ello interfieren y recomendar las líneas de actuación para minimizar el impacto ambiental. Ha sido por tanto una investigación orientada a la definición de metodologías, modelos y técnicas con la intención de evaluar, simular y monitorizar las características de las nubes de polvo. En los estudios se emplearon las más importantes herramientas computacionales específicas y generales adaptadas al estudio tales como la Modelización-Animación en 3D, los Elementos Finitos (códigos MEF), los códigos numéricos (CFD4D) y los Elementos Discretos (PFC4D).

No description available.

Le prototypage virtuel des circuits pneumatiques de puissance, par exemple les circuits de freinage des véhicules industriels, constitue un enjeu important en raison de la complexité des écoulements en régime transsonique et des couplages entre les échelles locales et macroscopiques. Ces problèmes sont rencontrés lors de la conception, de la synthèse des commandes et de l'analyse des performances statiques et dynamiques de ces circuits et l'analyse. La mise au point des modèles numériques de ces systèmes induit des coûts et des temps importants par rapport à d'autres systèmes. La démarche proposée dans cette thèse repose sur la construction numérique de bases de données permettant de caractériser le comportement local et macroscopique d'un composant de circuit en fonction de la variation de certains paramètres physiques ou géométriques par rapport à un point de fonctionnement de référence. Les bases de données résultent de l'extrapolation de la solution des équations de Navier Stokes moyennées (RANS) pour le point de référence considéré obtenu à l'aide d’un logiciel de paramétrisation en mécanique des fluides (Turb’Opty). La contribution de cette thèse repose pour l'essentiel dans un travail d'analyse des solutions issues de la paramétrisation dans deux contextes différents: la tuyère De Laval et un élément "coude", des composants élémentaires de circuit. Nous avons montré que ces exemples "simples" conduisent déjà à des difficultés importantes en termes de paramétrisation du problème et du calcul des dérivées des champs aérodynamiques en raison de la taille du problème. Pour pallier cette difficulté, nous avons proposé de déraffiner le maillage et nous avons alors montré que cette démarche conduit parfois à déplacer ou à atténuer certains phénomènes (chocs). La deuxième contribution de ce travail repose sur l'évaluation de la qualité des solutions extrapolées, de leur domaine de validité et la construction des liens entre grandeurs locales et macroscopiques. Nous avons enfin proposé une démarche permettant de reconstruire la caractéristique en débit d'un composant à partir de la détermination de la solution extrapolée pour un nombre limité de points de référence. / Virtual prototyping pneumatic circuits for power transmission, for example braking circuits of trucks, is still a difficulty because of the complexity of the flow behavior in transonic conditions and of the coupling between local and macroscopic scales. These problems are met during system design, control synthesis and for static and dynamic performance analysis. Tuning accurate numerical models requires important costs and time when compared to other systems. The methodology proposed in this PhD thesis relies on numerically determining a data base that characterizes the local and macroscopic behavior of a circuit component according the variation from a reference point of some physical or geometrical parameters. The data bases are obtained from the extrapolation of the Mean Navier Stokes solution (RANS) for a given reference point with the help of a parametrization software dedicated to fluid mechanics (Turb'Flow). The main contribution of this thesis relies io the analysis of the solution obtained from the parametrization in two different cases: the De Laval nozzle and un "elbow" connecting element, which are elementary component in a circuit. We have shown that these two "simple" cases lead already to important difficulties in term of problem parametrization and calculation of the derivatives of the aerodynamic fields because of the problem dimension. In order to tackle this, we proposed to reduce the spatial discretization (mesh derefining) and we showed that this approach could sometimes lead to damp or move some phenomena (shocks). The second contribution of this work relies on evaluating the quality of the extrapolated solution and their validity domain, and on building links between local and macroscopic behavior. Finally, we proposed a method that allows the mass flow rate characteristic of a component to be determined from the calculation of the extrapolated solution issued from a limited number of reference points.