Cooling of electronic components is one of the most important issues concerned in the electronic industry for design of equipment. Maintaining the temperature of an electronic device within its safe operating temperature limits is essential to operate the equipment safely with proper functionality. According to the Arrhenious law of failure rate, for a device with activation energy 0.65eV, every 10°C increase in temperature doubles the failure rate. Recent miniaturisation of components and high device heat dissipation rates lead to high heat fluxes, which cause temperature rise. Hence, there is an increasing need for research to achieve high heat removal rates and optimal design. Several cooling techniques are used for cooling of electronics based on the application and cooling rate requirements. Air-cooling of electronics has a wide range of applications due to its greater reliability, simplicity, easy maintenance, low cost, easy availability of coolant (air), and light weight. Air-cooling is also free from boiling and dripping problems. Air-cooling is used in applications such as avionics, cooling of personal computers, cooling of data centers, and in automobile electronics. In a typical electronic cooling application, cooling fluid is driven by the combination of external pressure forces and buoyancy forces. Based on the relative contribution of these forces towards the total driving force, the cooling techniques can be categorized as forced, natural or mixed convection cooling. However, in many of the electronic cooling situations, such as in the applications with very high heat fluxes, tall Printed Circuits Boards (PCBs) with low forced convection velocity, and in large scale applications such as data centers, the contributions of the buoyancy forces and external pressure forces for the total driving force are comparable, which results in a mixed convection situation. In the present study, mixed convection in vertical channels heated with five heating configurations, which represent typical electronic cooling applications, is studied numerically. The five different heating configurations are channels with flush-mounted continuous heater, flush-mounted strip heaters, flush-mounted square block heaters, protruding rib heaters and protruding square heaters. The first three configurations are categorised as flush-mounted heating configurations and the latter two configurations are categorised as protruded heating configurations. One of the channel walls represents the substrate on which the heaters are mounted and the heat sources represent the heat generating electronic components. Heat transfer under steady state conditions is considered in the study. The study includes laminar as well as turbulent heat transfer. For a systematic study of mixed convection, an analytical or semi-analytical formulation is desirable for a simplified model, as it can highlight the effect of relevant non-dimensional parameters on the heat transfer characteristics of a system. The results of a simplified model can be used for benchmarking the results of practical situations. Hence, before numerically solving the governing equations for mixed convection in channels, mixed convection boundary layer flows over a heated vertical plate is considered for study. Perturbation technique is used to solve the boundary layer equations with non-isothermal boundary conditions. The perturbation analysis is carried out for an arbitrarily variation of wall temperature or heat flux. Subsequently, the results are extended to find heat transfer rates in the cases of power-law variation of temperature and heat flux, as special cases. It is always required to design a cooling system to remove maximum possible amount of heat, keeping the device temperature within its safe operating limits. Hence, optimization of heat transfer in boundary layers is attempted, whose results can be used as guidelines to achieve optimal heat transfer in practical situations of channels with continuous as well as discrete heating. Similarity analysis is used for the optimization of heat distribution in boundary layer flows. In the similarity analysis, in the search of optimal heat transfer from the plate, the boundary layer equations are solved for various power-law heat flux variations and the appropriate power-law variation of optimal heat transfer is found. Similarly, the heat flux variation for optimal heat transfer is found for the cases of natural and forced convection, as they are the limiting cases of mixed convection. In the numerical part of the study, the generalised three-dimensional governing equations for the five heating configurations considered for the study are solved numerically with appropriate boundary conditions. Separation of natural, forced and mixed convection regimes is carried out in all the heating configurations using a criterion based on individual contributions of pressure force and buoyancy force towards the total driving force for the fluid movement. Heat transfer characteristics are studied in laminar as well as turbulent regimes in terms of parameters such as Grashof number, Reynolds number, Nusselt number, maximum temperature of heaters, pressure drop across the channel, and so on. The influence of conjugate effects on the heat transfer characteristics is studied by varying the substrate thermal conductivity. A systematic comparison of various effects such as the effect of discrete heating in plain channels, effect of discrete heating in channels with heated ribs, and the effect of three-dimensional protrusions on heat transfer, is achieved. The parameters in the individual configurations, which affect heat transfer, are explored for better cooling solutions. Optimal heat distribution among the heaters to minimise the temperature of the hottest heater for a given total amount of heat generation in the channel is found for all the channel configurations, which are heated either continuously or discretely. In the process of finding the optimal heat distribution among heaters, guidelines are taken from the optimal heat distribution in boundary layer flows. Compared to usual optimization approaches such as genetic algorithm, the present physics based optimisation procedure requires fewer runs to arrive at the optimal distribution. The fluid flow characteristics in all the three configurations with flush-mounted heaters are found to be similar. However, heat transfer characteristics in channels with flush-mounted square heaters differ from those in the other two flush-mounted channel configurations. Hot spots with higher temperatures are found at heater locations in channels with flush-mounted square heaters. The effect of substrate follows the same trend in all the flush-mounted configurations. At lower thermal conductivities, the maximum temperature decreases sharply with increasing thermal conductivity. However, at higher conductivities, the influence reduces. In all the flush-mounted configurations, heat transfer will not be influenced by substrate thermal conductivity increment at conductivities more than 150 times the fluid thermal conductivity. The fluid flow and heat transfer characteristics in channels with protruded heaters differ significantly from those in channels with flush-mounted heaters. The protrusions in the channels interact with the fluid flow and make it different from that of smooth channels. In turn, the protrusions affect heat transfer characteristics in the channels. The influence of the protrusions on the heat transfer and locations of hot spots in the domain is examined. Effect of thermal conductivity in channels with protruded square heaters is similar to that in channels with flush-mounted heaters. However, conductivity in channels with protruded rib heaters affects the heat transfer in a wider range of conductivities than in the other heating configurations. Unlike in the other configurations, at low thermal conductivities, maximum temperature does not drop sharply with increase of conductivity. In channels with protruded square heaters, staggering arrangement of heaters results in higher heat transfer rates than those with in-line heater arrangement. In all the configurations, pressure drop is found to be independent of Grashof number in the range of heat dissipation rates considered in the study. Heat transfer rates in turbulent region are much higher than the heat transfer rates in laminar regime. However, the pressure drops encountered are also high in the turbulent regime. Turbulent heat transfer results in a more uniform temperature distribution in channels. The cooling performances of the individual configurations are compared. For a given pressure drop the cooling performances decreases in the order of flush-mounted strip heating, protruded square heating, flush-mounted square heating, protruded rib heating. For a given inlet fluid flow rate, the cooling performances decreases in the order of protruded rib heating, protruded square heating, flush-mounted square heating, flush-mounted strip heating. However, for a given inlet fluid flow rate, the pressure drop increases in the order of increasing cooling performance.

A stacked microchannel heat sink was developed to provide efficient cooling for microelectronics devices at a relatively low pressure drop while maintaining chip temperature uniformity. Microfabrication techniques were employed to fabricate the stacked microchannel structure, and experiments were conducted to study its thermal performance. A total thermal resistance of less than 0.1 K/W was demonstrated for both counter flow and parallel flow configurations. The effects of flow direction and interlayer flow rate ratio were investigated. It was found that for the low flow rate range the parallel flow arrangement results in a better overall thermal performance than the counter flow arrangement; whereas, for the large flow rate range, the total thermal resistances for both the counter flow and parallel flow configurations are indistinguishable. On the other hand, the counter flow arrangement provides better temperature uniformity for the entire flow rate range tested. The effects of localized heating on the overall thermal performance were examined by selectively applying electrical power to the heaters. Numerical simulations were conducted to study the conjugate heat transfer inside the stacked microchannels. Negative heat flux conditions were found near the outlets of the microchannels for the counter flow arrangement. This is particularly evident for small flow rates. The numerical results clearly explain why the total thermal resistance for counter flow arrangement is larger than that for the parallel flow at low flow rates. In addition, laminar flow inside the microchannels were characterized using Micro-PIV techniques. Microchannels of different width were fabricated in silicon, the smallest channel measuring 34 mm in width. Measurements were conducted at various channel depths. Measured velocity profiles at these depths were found to be in reasonable agreement with laminar flow theory. Micro-PIV measurement found that the maximum velocity is shifted significantly towards the top of the microchannels due to the sidewall slope, a common issue faced with DRIE etching. Numerical simulations were conducted to investigate the effects of the sidewall slope on the flow and heat transfer. The results show that the effects of large sidewall slope on heat transfer are significant; whereas, the effects on pressure drop are not as pronounced.

En vue de leur refroidissement, les parois de chambres de combustion aéronautiques sont perforées de trous à travers lesquels de l’air plus froid est injecté. La paroi est ainsi refroidie par convection et un film isolant est créé en surface chaude (film cooling). Cette thèse a pour objectif d’utiliser les possibilités de la fabrication additive pour proposer de nouvelles solutions architecturées qui permettraient d’augmenter les échanges de chaleur internes et d’obtenir ainsi de meilleures efficacités de refroidissement.La première approche consiste à élaborer de nouveaux designs de plaques multiperforées par Electron Beam Melting (EBM) et Selective Laser Melting (SLM) aux limites de résolution des procédés. Les architectures sont caractérisées en microscopie, en tomographie X et en perméabilité. Des simulations aérothermiques permettent de mettre en évidence l’effet de ces nouveaux designs sur l’écoulement et les échanges de chaleur, et de proposer des voies d’amélioration de la géométrie.La deuxième approche consiste à élaborer de façon simultanée une pièce architecturée par EBM, avec des zones denses et poreuses. A partir d’analyse d’images associée à une cartographie EBSD grand champ, il est possible de remonter aux mécanismes de formation du matériau poreux et de relier la perméabilité et la porosité aux paramètres procédé. Afin de favoriser le film cooling, il pourrait être avantageux que les zones microporeuses soient orientées dans le sens de l’écoulement. Pour ce faire, un nouveau procédé dénommé Magnetic Freezing, où des poudres métalliques forment une structure orientée par un champ magnétique, est mis au point.Les diverses solutions développées durant cette thèse sont testées sur un banc aérothermique. Les essais montrent qu’elles offrent un refroidissement plus efficace et plus homogène que la référence industrielle. Enfin, de premiers tests en combustion sur l’une des structures retenues, plus légère et plus perméable que la référence, montrent qu’il s’agit d’une solution aussi efficace à un débit traversant donné, et donc a priori plus efficace à une surpression donnée. / Combustion chamber walls are perforated with holes so that a cooling air flow can be injected through them. The wall is cooled by convection and an insulating film is created on the hot surface (film cooling). This PhD thesis aims to use the possibilities of additive manufacturing to provide new architectured solutions that could enhance the internal heat exchanges, and lead to a higher cooling effectiveness.The first approach is to develop new designs of multiperforated walls by Electron Beam Melting (EBM) and Selective Laser Melting (SLM) used at the resolution limits of the processes. They are characterized by microscopy, X-ray tomography and permeability tests. Some aerothermal simulations help understanding the effects of these new designs on the flow and on heat exchanges. These results lead to a geometry adaptation.The second approach is to simultaneously manufacture an architectured part with dense and porous zones by EBM. Thanks to image analysis combined with large field EBSD, it is possible to investigate the mechanisms leading to the porous zones and to link them to permeability and porosity. The film cooling effect could be favoured by the orientation of pores towards the cooling flow. Therefore, a new powder-based manufacturing process named Magnetic Freezing, where metallic powders organize into an oriented structure thanks to a magnetic field, is developed.The various solutions studied during this thesis are tested on an aerothermal bench. They all show a more efficient and homogeneous cooling than the industrial reference. Some first tests on one of the selected solutions are performed on a combustion bench. This lighter and more permeable structure proves to be a solution as efficient as the industrial reference at a given flow rate. It should therefore be a more efficient solution for a given overpressure.

Made available in DSpace on 2016-06-02T20:09:08Z (GMT). No. of bitstreams: 1 1646.pdf: 3878244 bytes, checksum: 1b913364f7458c2e95fc16bda01f835e (MD5) Previous issue date: 2007-08-01 / Financiadora de Estudos e Projetos / This research focuses the evaporative cooling by water aspersion on wavy cement fiber tiles in the city of São Carlos, SP, seeking to use it to reduce the buildings heat gains. A theoretical model was developed, based on classic equations of fluids mechanic, applied to iterative calculations of heat flows on the tile superior surface, considered as control surface. In the work development, this model was progressively adjusted to experimental data obtained in a test cell, exposed to the local climatic conditions, with the monitoring of superficial temperatures of both faces in two tiles, one maintained dry and other under intermittent aspersion of water. The research results indicated that, despite of still being susceptible to improvement, the theoretical model already presents quite satisfactory approach with the measured data. Applying a statistical adjustment to the proposed model of iterative heat flows calculation, it was obtained a correlation coefficient between measured and estimated temperatures of 0,999 and a standard deviation of 0,35 ºC. During the experiments, the average evaporative heat flow was 409 W/m2. Theaverage water volume evaporated was 0,7 l/(m².h), corresponding to an average difference of temperatures among the compared tiles of 5,12 K, for the daylight period. Due to the growing need of energy consumption reduction, this procedure seems to be a good option to reduce buildings thermal load, if compared to conventional air conditioning systems / Esta pesquisa enfoca a refrigeração evaporativa por aspersão de água sobre telhas onduladas de fibrocimento, na cidade de São Carlos, SP, visando sua utilização para redução dos ganhos de calor em edificações. Um modelo teórico foi desenvolvido, baseado em equações clássicas da mecânica dos fluidos, aplicadas em cálculos iterativos dos fluxos de calor sobre a superfície superior da telha, considerada como superfície de controle. No desenvolvimento do trabalho, este modelo foi progressivamente ajustado a dados experimentais obtidos em uma célula de teste, exposta às condições climáticas locais, sendo monitoradas temperaturas superficiais de ambas as faces em duas telhas, uma mantida seca e outra sob aspersão intermitente de água. Os resultados da pesquisa indicaram que, apesar de ainda ser passível de aprimoramento, o modelo teórico já apresenta aproximação bastante satisfatória com os dados medidos. Aplicando-se um ajuste estatístico ao modelo proposto de cálculo iterativo dos fluxos de calor, obteve-se um coeficiente de correlação entre temperaturas medidas e estimadas de 0,999 e um desvio padrão de 0,35 ºC. Durante os experimentos, o fluxo médio de calor por evaporação foi de 409 W/m2. O volume médio de água evaporado foi de 0,7 l/(m².h), correspondendo a uma diferença média de temperaturas entre as telhas comparadas, para o período diurno, de 5,12 K. Frente à crescente necessidade de redução de consumo de energia, esta parece uma boa opção para redução da carga térmica dos edifícios, se comparada aos sistemas convencionais de condicionamento de ar

Made available in DSpace on 2014-10-09T12:55:30Z (GMT). No. of bitstreams: 0 / Made available in DSpace on 2014-10-09T14:07:16Z (GMT). No. of bitstreams: 0 / Tese (Doutoramento) / IPEN/T / Instituto de Pesquisas Energeticas e Nucleares - IPEN-CNEN/SP

Com base em um modelo fenomenológico e a partir de dados experimentais obtidos numa planta piloto, foi obtida uma correlação entre o desempenho de uma torre de resfriamento em função das principais variáveis de processo: fluxos mássicos do gás e da água pela torre, e temperatura de entrada da água. Os resultados apresentaram boa consistência, comparados com os da literatura. A metodologia desenvolvida pode, com relativa facilidade, ser aplicada para torres de resfriamento industriais, pois se baseia em medidas de variáveis, factíveis em termos práticos. Efetuou-se também um estudo paralelo com base em modelagem e simulações matemáticas do comportamento de uma torre de resfriamento de água em condições severas, com temperatura da água de alimentação superior a 50°C. Constatou-se que o coeficiente de transporte de massa na torre de resfriamento aparentemente não é afetado. / Cooling towers are widely used in many industrial and utility plants and its thermal performance is of vital importance. In the present work, using a phenomenological model and by experiments carried on over a pilot installation, the mass transfer coefficient dependence of air and water flow rates and inlet cooling water temperature is determined. The approach proposed may be useful in addition for characterization of industrial cooling towers since it depends on temperature and flow rate measurement usually available in typical plants. A parallel study concerning high mass transfer rate theory is accomplished. Through mathematical modeling and simulations based on this study no influence is detected on the mass transfer coefficient in the cooling tower, operating under harsh conditions with inlet water temperature up to 90°C.

Made available in DSpace on 2014-10-09T12:55:30Z (GMT). No. of bitstreams: 0 / Made available in DSpace on 2014-10-09T14:07:16Z (GMT). No. of bitstreams: 0 / Foi desenvolvida uma técnica de medida de nível em vasos de pressão usando sondas térmicas resfriadas internamente por um fluido e análise dos dados experimentais com Redes Neurais Artificiais (RNA´s). Esse novo conceito de sondas térmicas foi testado em uma Bancada Experimental para Testes de Sondas de Nível (BETSNI) com duas seções de testes, ST1 e ST2. Dois projetos distintos de sondas foram construídos: Sonda de Tubos Concêntricos e Sonda de Tubo U. Um Sistema de Aquisição de Dados (SAD) foi montado para registrar os dados experimentais. Testes foram realizados tanto para condições de nível nas seções de testes em estado estacionário quanto para transientes. Os dados experimentais de temperatura e de nível obtidos foram usados para compor tabelas de treinamento e de verificação usadas para implementar RNA´s no programa RETRO-05, que simula um Perceptron de Múltiplas Camadas com Retropropagação. As análises mostraram que a técnica pode ser aplicada para medir o nível em vasos de pressão. As análises mostraram ainda que a técnica é aplicável para um número menor de entradas de temperatura que o inicialmente previsto no projeto das sondas e é robusta, aplicando-se mesmo quando ocorre a perda de alguma informação de temperatura. Dados experimentais disponíveis na literatura referentes a uma sonda térmica aquecida eletricamente também foram usados nas análises com RNA´s, produzindo bons resultados. Os resultados das análises indicaram que a técnica é eficaz e robusta, podendo ser aprimorada e aplicada para medidas de nível em vasos de pressão. / Tese (Doutoramento) / IPEN/T / Instituto de Pesquisas Energeticas e Nucleares - IPEN-CNEN/SP

My thesis deals with the design of an experimental emergency cooling device of the reactor pressure vessel (RPV). It consists of two parts, the theoretical one and practical one. Different molten corium cooling methods in terms of their efficiency and comparison are introduced in the theoretical part. The design of an experimental emergency cooling device, which incorporates a model channel past the reactor pressure vessel , is presented in the practical part. The cooling device consists of a model channel past the reactor pressure vessel, condensator, which takes away the heat generated by the reactor pressure vessel and the pump of a secondary loop. Next, thermal and hydraulic calculations are given in this section. The conclusion is devoted to the evaluation of particular cooling technologies and their comparison in terms of nuclear and technical safety.

This diploma thesis deals with producing and using low temperatures in home brewing processes. The introductory part describes technological process of brewing beer, followed by a design of a primary fermentation vessel and next an aging vessel. In the next step a suitable wort chiller is designed. All the equipment is designed to be able to run on batteries or a solar photovoltaic panel.

Die Kühlung thermisch hoch belasteter Bauteile wird häufig mit Kühlverfahren realisiert, die auf dem Prinzip des Massetransports durch die Bauteilwand beruhen. Neben der Film- und Transpirationskühlung gehört die Effusionskühlung zu diesen Verfahren und basiert auf einer Reihe oder einem Raster von Bohrungen. Dieser Ansatz ermöglicht sowohl den Abtransport von Wärme aus dem Bauteil als auch die Ausbildung eines schützenden Kühlmittelfilms auf der Bauteiloberfläche. Viele Autoren beschäftigten sich in ihren Arbeiten mit den Auswirkungen der Filmkühlung auf den Wärmeübergang an der Bauteilwand und definierten einen Filmkühlwirkungsgrad, der die Effektivität der Kühlung widerspiegelt. Auch die Freistrahlen aus Effusionskühlbohrungen wurden mit diesen Mitteln untersucht und eine Vielzahl unterschiedlicher Einflussgrößen auf den Filmkühlwirkungsgrad identifiziert. Dazu gehören insbesondere geometrische Bedingungen, wie z.B. der Bohrungswinkel, das Verhältnis von Länge zu Durchmesser der Bohrung und die Austrittsgeometrie der Bohrungen. In späteren Beiträgen analysierten verschiedene Autoren die Einflüsse der Turbulenz sowie der Stoffwerte von Kühlmittel und Hauptströmung. Dabei kamen meist Luft und seltener Kohlendioxid oder Stickstoff als Kühlmittel zum Einsatz. In den letzten Jahren wurde das Verhalten des Kühlmittelstrahls vor allem numerisch untersucht. Dabei beschränkte sich das Berechnungsgebiet oftmals auf das direkte Umfeld der Effusionskühlbohrung und die Identifikation und Beschreibung auftretender Wirbelstrukturen. Der Bereich weiter stromab der Bohrung blieb oft unberücksichtigt. Die vorliegende Arbeit verfolgt den Ansatz, den Kühlmittelstrahl in der Hauptströmung zu beobachten. Das wird durch die Verwendung von Helium und Argon als Kühlmittel möglich, denn diese Gase können in der Luftströmung detektiert werden. Durch eine in zwei Richtungen bewegliche Kombisonde wird Gas aus der Grenzschicht abgesaugt und die Konzentration des Kühlmittels bestimmt. Die so an diskreten Punkten stromab der Effusionskühlbohrung erhaltenen Konzentrations- und Geschwindigkeitsprofile ermöglichen die Verfolgung des Kühlmittelstrahls und dessen Wechselwirkungen mit der Hauptströmung. Für eine vergleichende Analyse der gemessenen Profile entstand ein empirisches Verfahren zur Systematisierung der gesamten Messdaten. Die Definition einer mittleren Kühlmittelkonzentration innerhalb einer zweckmäßig festgelegten Höhe über der Wand und eines normierten Einblasparameters, der das Verhältnis der molaren Massen von Kühlmittel und Hauptströmung berücksichtigt, sind der Kern des empirischen Verfahrens. Für Vergleiche mit der Literatur erfolgte die Berechnung eines Filmkühlwirkungsgrads auf Basis der Massebilanz in der Grenzschicht und der mittleren Kühlmittelkonzentration. Während der Datenauswertung zeigte sich, dass der Bohrungswinkel einen geringen Einfluss auf die mittlere Kühlmittelkonzentration hat und so ein Bohrungswinkel von 30° ein guter Kompromiss zwischen Herstellungsaufwand und Kühlwirkung ist. Kühlmedien mit geringer molarer Masse und hoher spezifischer Wärmekapazität sollten bevorzugt werden, da deren Kühlwirkung hoch, der Einfluss auf die Grenzschicht aber gering ist. / The cooling of thermally heavily loaded components is commonly performed by injecting a mass flow through the component’s wall into the hot flow, which is called Film cooling. The main goal is to form a coolant film to reduce the hot side heat transfer and to absorb thermal energy in order to protect the component’s wall. There are different techniques available called film cooling, transpiration cooling and effusion cooling. By applying transpiration cooling, the cooling fluid is injected through a porous material into the hot gas flow. Unfortunately, these porous materials do not have the physical strength required to work within gas turbines. If the injection is done with a row or a pattern of holes so the cooling film is renewed at certain positions, the cooling technique is called effusion cooling. Film cooling means the injection of fluid through a slot without renewing the film. Many authors analyze the effect of the film or effusion cooling on the wall temperature, the heat transfer coefficient or the cooling effectiveness. Many influencing factors were identified, such as the length to diameter relation, the hole’s alignment, fluid properties as well as turbulence and vortices. Recent works use numerical simulations to investigate the turbulent flow and vortex development in the near field of the injection hole. Due to the complexity of the simulation, the effects far downstream area were not covered by these simulations. This work investigates the behavior of the cooling jet within the boundary layer above the wall. Therefore a foreign gas (Helium, Argon) was injected as coolant into a cross flow and a pitot probe was used to get gas samples out of the boundary layer and the coolant gas fraction was measured. The measured concentration was empirically systematized by comparative data analysis. Therefore, a mean concentration within a certain height above the wall was calculated. Also a normed blowing rate was used to include the molar masses of coolant and cross flow. With this mean concentration a cooling effectiveness is calculated based on a balance model and compared to the results in the literature. As a result of the data evaluation, the hole’s angle was found to have a minor influence on the mean coolant concentration. An angle of about 30° is a good compromise between production effort and cooling efficiency. Also coolant fluids with a low molar mass and high specific heat capacity should be preferred because of their low impact on the boundary layer.