No description available.

An examination of various methods for mass flow rate measurements was undertaken to evaluate their applicability for measuring refrigerant R-134a two-phase mass flow in refrigeration and air-conditioning equipment. An experimental apparatus was constructed to generate the required two-phase flow conditions. A turbine and a venturi flowmeter were used together with either a capacitance transducer or a gamma densitometer to determine the two-phase mass flow rate. The time-averaged void fraction was measured using a capacitance transducer and a gamma densitometer. Their measurements were in good agreement. Hence, for mass flow rate measurements, the capacitance transducer was used as the void fraction meter because of its ease of operation. A number of models were used to combine the output of either the turbine flowmeter or the venturi flowmeter, with the void fraction measurement to estimate the mass flow rate. It was found that, within the range of experimental data tested in the present work, the venturi flowmeter, in conjunction with Chisholm's model, provided the best agreement with the experimental results. / Thesis / Master of Engineering (MEngr)

The main objective of this study is to explore the complex fluid flow phenomena that result in the generation of a high frequency noise in counterbalance valves through an experimental and numerical investigation of the flow. Once the influence of the different components involved in noise generation is established, a secondary objective is the introduction of design modifications that eliminate the undesired effect without altering the operation envelope or the performance of the valve. A hydraulic test bench was used to carry out an experimental investigation of the noise generation process. A computer based data acquisition system was used to record pressure fluctuations, flowrates and hydraulic oil temperatures in a production valve under a variety of operational conditions. Extensive experimental measurements and numerical modeling lead to the hypothesis that noise generation is the result of an acoustic resonance triggered by shear layer instability at the valve inlet. The pressure gradients developed when the shear layer entrains the stagnant fluid in the valve main cavity cause the layer to become unstable and oscillate. The oscillation frequency will depend on a great number of factors such as valve geometry, pressure and velocity gradients and the density and viscosity of the fluid. It is postulated that the observed noise is generated when this frequency matches one of the resonant frequencies of the valve cavity. The proposed mechanism is theoretically poorly understood and well beyond simplified analysis, its accurate numerical simulation is computational very intensive requiring sophisticated CFD codes. The numerical investigation was carried out using STAR–CCM+, a commercially available CFD code featuring 3-D capabilities and sophisticated turbulence modeling. Streamline, pressure, velocity-vector and velocity-scalar plots were obtained for several valve configurations using steady and unsteady state flow simulations. An experimental and numerical analysis of an alternative valve geometry was carried out. Experimental results demonstrated a greatly reduced instability range. The numerical analysis of the unsteady behavior of the shear-layer streamlines for both valves yielded results that were compatible with the experimental work. The results of this investigation promise a great positive impact on the design of this type of hydraulic valves.

Cette thèse est consacrée à l'étude des écoulements de gaz raréfiés à travers divers micro-conduits de type circulaire et rectangulaire dans des conditions isotherme et stationnaire. L'objectif de la thèse est de contribuer à l'étude de l'interaction gaz-surface notamment en déterminant le coefficient d'accommodation de la quantité de mouvement pour différent matériaux de surface (Or, Silice, Acier inoxydable et Sulfinert) associés à différents types de gaz (hélium, azote, argon et dioxyde-de-carbone). Afin d'atteindre cet objectif, on adopte un triple point de vue : expérimental, théorique et numérique. L'aspect expérimental est réalisé par des mesures de débit massique à travers les micro-conduits, en utilisant la méthode dite « à volume constant ». L'aspect théorique original est développé à travers une nouvelle approche basée sur la résolution de l'équation de Stokes. Cette approche a permis d'écrire une expression analytique de débit massique en régime de glissement, qui prenne en compte les effets bidimensionnels dans une section de conduit rectangulaire. Cette approche complètement explicite, est conduite au deuxième ordre. Enfin l'aspect numérique permet de calculer le débit massique, en régimes transitionnel et moléculaire libre, en résolvant numériquement l'équation cinétique BGK linéarisée. La comparaison des mesures de débit massique avec l'équation analytique, en régime de glissement, ou avec les calculs numériques, en régimes transitionnel et moléculaire libre, nous a permis de déduire des coefficients de glissement et les coefficients d'accommodation correspondant à chaque couple gaz-surface dans tous les régimes de raréfaction. / This thesis is devoted to the study of rarefied gas flows through micro-channels of various cross sections (circular and rectangular) under isothermal and stationary conditions. The objective of this thesis is to contribute to the study of gas-surface interaction by determining the tangential momentum accommodation coefficient for different surface materials (gold, silica, stainless steel and Sulfinert) and associated to various gases (helium, nitrogen, argon and carbon-dioxide). To achieve this goal three aspects are considered: experimental, theoretical and numerical. The experimental aspect is considered by measuring the mass flow rate through microchannels using the constant volume technique. The theoretical aspect is considered by the development of a new approach based on the Stokes equations. This approach yields to the analytical expression of the mass flow rate in the slip regime, which takes into account the second order effects. The last aspect, numerical, is considered by the numerical simulations of the mass flow rate in the transitional and free molecular flow regimes by solving the linearized BGK kinetic model. The comparison between the measured mass flow rates and the analytically expressions in the slip regime or with the results of numerical simulations in the transitional and free molecular regimes enabled to deduce the tangential momentum accommodation coefficients corresponding to each pair gas-surface in all flow regimes.

Cette thèse de doctorat porte sur l'étude et la réalisation d'une plateforme de pesage dynamique pour véhicule roulant basée sur un concept d'intégration de la charge. Ce concept est mis en œuvre en vue de pouvoir minimiser la taille et l'encombrement de ce type de dispositif tout en effectuant des pesées présentant des caractéristiques métrologiques acceptables. Nous démontrons tout d'abord au travers de la réalisation d'un prototype et de plusieurs campagnes d'essais, la faisabilité de la méthode utilisée. Nous évaluons dans un deuxième temps les performances présentées par le prototype lors du pesage de véhicules légers roulant jusqu'à des vitesses de 35km/h. Une étude est ensuite menée sur les jauges de déformation piézorésistives et les jauges piézoélectriques réalisées en couches épaisses grâce à des techniques de sérigraphie. Nous caractérisons ces transducteurs avec pour objectif leur utilisation dans des dispositifs de pesage en remplacement des jauges de déformation classiques à filaments métalliques. / This PhD thesis is devoted to the study and implementation of a weigh-in-motion platform for vehicle based on a concept of integration of load. This concept is used to minimize the size of this kind of device while performing weighings with acceptable results. First, we show thanks to a protoype and several test campagns, the feasability of the method used. In a second time, we evaluate the performances of the prototype in terms of precision and repeatability with the dynamic weighing of vehicles at speeds up to 35km/h. A study is finally conducted on thick-film piezoresitive strain gauges and piezoelectric gauges manufacturing by a screen-printing process with cermet and polymer pastes. We characterize these tranducers with the goal of used them as an alternative of conventional foil strain gauges.

The aim of the project was to get familiar with the environment of ANSYS CFX, create several models of fans and synchronous machine model in Autodesk inventor, create model of cooling medium flow through the machine with these fans and evaluation of results. Firstly the thesis describes the synchronous machine itself, losses of the machine, the flow of power of synchronous machine and methods of its cooling. Next the thesis describes each kind of heat transfer, laminar and turbulent flow. The thesis also refers of kind of the fans and the program used to calculate the flow Ansys CFX, including the method that Ansys used to calculate. The work describes the individual modification of fans and setting of calculation in ANSYS. Then displays the results of the analysis these fans for different numbers of fan blades and for modification of the fan. Then the thesis analyzes selected modifications due to changing speed. In the last chapter shows the analysis of flow in the machine with three different fans. In particular, there is shown the mass flow rate, pressure and its distribution on areas for evaluation.

La diminution de la cylindrée ou le downsizing du moteur est potentiellement l'une des stratégies les plus efficaces pour améliorer la consommation de carburant et diminuer les émissions polluantes. Dans le domaine de la suralimentation, la simulation est limitée par les caractéristiques de fonctionnement des turbines fournies par les constructeurs. Une extrapolation précise et fiable des cartographies turbine est donc l’objectif de cette thèse. Une étude expérimentale sur une turbine radiale d’un turbocompresseur est effectuée avec différentes techniques pour mesurer la cartographie turbine la plus large possible. Les mesures sont effectuées sur un banc turbocompresseur classique avec différentes températures d'entrée turbine. Puis une technique de gavage en entrée et en sortie compresseur est testée. Le compresseur est ensuite remplacé par un autre compresseur à roue inversée qui peut aider la turbine à tourner et même l’entrainer. Les débits les plus faibles et même les débits négatifs sont mesurés. Un banc turbine électromécanique a également été développé, mais n’a pas pu donner de résultats satisfaisants à cause de problèmes techniques mais des évolutions à venir restent prometteuses. Les diverses techniques expérimentales testées ont aussi permis de mesurer le rendement isentropique de la turbine et le rendement mécanique du turbocompresseur. Finalement, plusieurs modèles d’extrapolation des courbes caractéristiques turbine ont été testés et confrontés aux résultats expérimentaux. / Engine downsizing is potentially one of the most effective strategies being explored to improve fuel economy and reduce emissions. In the field of turbocharging,simulation is limited by the operating characteristics of turbines supplied by the manufacturers. An accurate and precise extrapolation of the turbine performance maps is the main aim of this study. An experimental study was done on a radial turbine of a turbocharger with different techniques to measure the wider turbine performance map possible. Measurements were done on a classic turbocharger test bench with different turbine inlet temperatures. Then air was blown to the compressor inlet and exit: it is the compressor “gavage”. The compressor is then replaced with another one with are versed rotor: this compressor can help the turbine turn and even drive it itself. The lowest mass flow rates are measured even the negative ones. An electromechanical turbine test bench was developed but did not work correctly because of technical problems but future developments are promising. The various experimental techniques used allowed also the measurement of the turbine isentropic efficiency and the turbocharger mechanical efficiency. Finally, many extrapolation models of the turbine performance maps were tested and compared to the experimental results.

The labyrinth seal is a non-contact annular type sealing device used to reduce the internal leakage of the working fluid which is caused by the pressure difference between each stage in a turbomachine. Reducing the leakage mass flow rate of the working fluid through the labyrinth seal is desirable because it improves the efficiency of the turbomachine. The carry-over coefficient, based on the divergence angle of the jet, changed with flow parameters with fixed seal geometry while earlier models expressed the carry-over coefficient solely as a function of seal geometry. For both compressible and incompressible flows, the Reynolds number based on clearance was the only flow parameter which could influence the carry-over coefficient. In the case of incompressible flow based on the simulations for various seal geometries and operating conditions, for a given Reynolds number, the carry-over coefficient strongly depended on radial clearance to tooth width ratio. Moreover, in general, the lower the Reynolds number, the larger is the divergence angle of the jet and this results in a smaller carry-over coefficient at lower Reynolds numbers. However, during transition from laminar to turbulent, the carry-over coefficient reduced initially and once the Reynolds number attained a critical value, the carry-over coefficient increased again. In the case of compressible flow, the carry-over coefficient had been slightly increased if radial clearance to tooth width ratio and radial clearance to tooth pitch ratio were increased. Further, the carry-over coefficient did not considerably change if only radial clearance to tooth width ratio was decreased. The discharge coefficient for compressible and incompressible flows depended only on the Reynolds number based on clearance. The discharge coefficient of the tooth in a single cavity labyrinth seal was equivalent to that in a multiple tooth labyrinth seal indicating that flow downstream had negligible effect on the discharge coefficient. In particular, for compressible fluid under certain flow and seal geometric conditions, the discharge coefficient did not increase with an increase in the Reynolds number. It was correlated to the pressure ratio, Pr. Moreover, it was also related to the fact that the flow of the fluid through the constriction became compressible and the flow eventually became choked. At low pressure ratios (less than 0.7), Saikishan’s incompressible model deviated from CFD simulation results. Hence, the effects of compressibility became significant and both the carry-over coefficient compressibility factor and the discharge coefficient compressibility factor needed to be considered and included into the leakage model. The carry-over coefficient compressibility factor, phi, had two linear relationships with positive and negative slopes regarding the pressure ratios. This result was not associated with the seal geometry because the seal geometry ratios for each instance were located within the nearly same ranges. Further, the phi-Pr relationship was independent of the number of teeth regardless of single and multiple cavity labyrinth seals. The discharge coefficient compressibility factor, psi, was a linear relationship with pressure ratios across the tooth as Saikishan predicted. However, in certain flow and seal geometric conditions, Saikishan’s model needed to be modified for the deviation appearing when the pressure ratios were decreased. Hence, a modified psi-Pr relationship including Saikishan’s model was presented in order to compensate for the deviation between the simulations and his model.

No description available.

[ES] En un contexto de creciente preocupación por el calentamiento global y de políticas energéticas internacionales, en el cual los sistemas de climatización de los edificios suponen una parte importante del consumo energético global, los sistemas de bombas de calor son considerados como opciones muy interesantes debido a su alta eficiencia y por ser fuentes de energía renovables. En este sentido, una caracterización precisa de estos equipos es de vital importancia con el objetivo de mejorar su diseño y, en aquellos casos dónde este tipo de unidades se integren como parte de sistemas más complejos, implementar estrategias de control eficientes. En este contexto, esta tesis doctoral se centra en el modelado de bombas de calor con el fin de obtener modelos que permitan conocer con precisión el desempeño global de estas unidades en todo el rango de trabajo. En la primera parte del trabajo, se han realizado numerosos ensayos experimentales utilizando un nuevo prototipo de bomba de calor dual, obtenidos dentro del marco de trabajo del proyecto europeo GEOTeCH. Debido a la tipología hibrida de esta unidad, los resultados experimentales obtenidos incluyen datos de desempeño para las principales tecnologías de bombas de calor: las bombas de calor aerotérmicas y geotérmicas. Haciendo uso de toda esta información experimental, esta primera parte del trabajo se centra en obtener modelos polinómicos para la predicción del consumo eléctrico y las capacidades de calefacción y refrigeración en función de las variables externas a la unidad. Dichas variables son fáciles de obtener y suelen medirse en instalaciones reales. Por tanto, estos modelos caracterizan a la bomba de calor como un único componente, simplificando su implementación en modelos globales de sistemas más complejos donde se instalan estas unidades. Además, seleccionado un enfoque empírico para el modelado, en esta parte también se analizan algunos aspectos relevantes, como los términos a incluir en el polinomio, o cómo conformar las matrices experimentales de ensayo necesarias, es decir, cuántos puntos experimentales realizar y dónde situarlos en el rango de operación. Por último, la segunda parte de la tesis doctoral está dedicada a modelar uno de los componentes principales en estas unidades, el compresor. En este caso, el desarrollo de una extensa base de datos que incluye numerosos ensayos calorimétricos de las dos principales tecnologías de compresores, pistón y scroll, ha permitido el análisis detallado de las superficies de respuesta del consumo eléctrico y el caudal másico de refrigerante en función de las temperaturas de evaporación y condensación. A partir de esta información y siguiendo un enfoque similar al utilizado previamente, en esta segunda parte se revisan los modelos incluidos en la norma actual de caracterización de compresores, el estándar AHRI 540 (2020), para comprobar si son adecuados o si, por el contrario, debemos utilizar otro tipo de expresiones polinómicas. También se analizan en profundidad cuestiones críticas como el número de puntos necesarios para caracterizar cada tecnología de compresor, dónde situarlos en el dominio experimental, cómo evitar un posible sobreajuste del modelo minimizando problemas de extrapolación o interpolación, o cómo extrapolar los resultados para predecir con otros refrigerantes u otras condiciones de aspiración. / [CA] En un context de creixent preocupació per l'escalfament global i de polítiques energètiques internacionals, en el qual els sistemes de climatització dels edificis suposen una part important del consum energètic global, els sistemes de bombes de calor són considerats com a opcions molt interessants a causa de la seva alta eficiència i perquè són fonts d'energia renovables. En aquest sentit, una caracterització precisa d'aquests equips és de vital importància amb l'objectiu de millorar el seu disseny i, en aquells casos on aquest tipus d'unitats s'integren com a part de sistemes més complexos, implementar estratègies de control eficients. En aquest context, aquesta tesi doctoral se centra en el modelat de bombes de calor per obtenir models que permitisquen conèixer amb precisió el funcionament d'aquestes unitats a tot el rang de treball. A la primera part del treball, s'han realitzat nombrosos assajos experimentals utilitzant un nou prototip de bomba de calor dual, obtinguts dins del marc de treball del projecte europeu GEOTeCH. A causa de la tipologia hibrida d'aquesta unitat, els resultats experimentals obtinguts inclouen dades de funcionament per a les principals tecnologies de bombes de calor: les bombes de calor aerotèrmiques i geotèrmiques. Fent ús de tota aquesta informació experimental, aquesta primera part del treball se centra a obtenir models polinòmics per a la predicció del consum elèctric i les capacitats de calefacció i refrigeració en funció de les variables externes a la unitat. Aquestes variables són fàcils d'obtenir i se solen mesurar en instal·lacions reals. Per tant, aquests models caracteritzen la bomba de calor com un únic component, simplificant-ne la implementació en models globals de sistemes més complexos on s'instal·len aquestes unitats. A més, seleccionat un enfocament empíric per al modelatge, en aquesta part també s'analitzen alguns aspectes rellevants, com els termes a incloure al polinomi, o cóm conformar les matrius experimentals d'assaig necessàries, és a dir, quants punts experimentals realitzar i on situar-los al rang d'operació. Per acabar, la segona part de la tesi doctoral està dedicada al modelat d'un dels components principals d'aquestes unitats, el compressor. En aquest cas, el desenvolupament d'una extensa base de dades que inclou nombrosos assajos calorimètrics de les dues principals tecnologies de compressors, pistó i scroll, ha permès l'anàlisi detallat de les superfícies de resposta del consum elèctric i el cabal màssic de refrigerant segons les temperatures d'evaporació i de condensació. A partir d'aquesta informació i seguint un enfocament similar a l'utilitzat prèviament, en aquesta segona part es revisen els models inclosos a la norma actual de caracterització de compressors, l'estàndard AHRI 540 (2020), per comprovar si són adequats o si, per contra, cal utilitzar un altre tipus d'expressions polinòmiques. També s'analitzen en profunditat qüestions crítiques com el nombre de punts necessaris per caracteritzar cada tecnologia de compressor, on situar-los al domini experimental, cóm evitar un possible sobreajust del model minimitzant problemes d'extrapolació o interpolació, o cóm extrapolar els resultats per predir amb altres refrigerants o altres condicions d'aspiració. / [EN] In a context of global warming concerns and global energy policies, in which heating and cooling systems in buildings account for a significant amount of the global energy consumption, heat pump systems are widely considered as a really interesting option for enabling high efficiency and also for being renewable energy sources. In this sense, an accurate characterization of these units is of vital importance to improve their design and implement efficient control strategies, when the unit is integrated in more complex systems. Against this background, this PhD thesis focuses on heat pump modelling in order to create map-based models able to accurately characterize the global performance of these units for the entire working range. In the first part of this work, many experimental tests have been obtained for a new Dual Source Heat Pump prototype tested in the framework of the European project GEOTeCH. Due to the dual typology, the experimental results include performance data for the two main heat pump technologies: Air Source Heat Pumps and Ground Source Heat Pumps. By using all this experimental information, this first part focuses on obtaining empirical polynomial models capable of accurately predicting energy consumption and heating and cooling capacities as a function of external variables. Such variables are easy to measure and are usually recorded in real installations. Therefore, these models characterize the heat pump as a single component, simplifying its implementation in global models of more complex systems where these units are installed. Furthermore, selecting the empirical model approach, this part also includes some critical aspects, such as how to obtain the best polynomial expression, or how to perform the required experimental test matrices, i.e., how many tests should be conducted and where in the operating range. Finally, the second part of this PhD thesis is dedicated to modelling one of the main components of these units, the compressor. In this case, the development of an extensive database including numerous calorimetric tests on the two main compressor technologies, reciprocating and scroll compressors, has allowed the detailed analysis of the response surfaces of their performance parameters, i.e., the energy consumption and mass flow rate as a function of the evaporation and condensation temperatures. Using this information, and following an approach similar to that used in the first part, this second part reviews the models included in the current compressor characterization standard, the AHRI 540 (2020), in order to check whether they are appropriate or, on the contrary, whether we should use of other types of polynomial expression. Critical issues such as the number of points needed to characterize each compressor technology, where to place them in the experimental domain, how to prevent possible overfitting in the model adjustment to minimize extrapolation or interpolation problems, or how to extrapolate results for predicting other refrigerant or suction conditions, are discussed in depth. / I would like to acknowledge the financial support that has made this PhD thesis possible. The doctoral fellowship FPU15/03476 was founded by “Ministerio de Educación, Cultura y deporte” inside the program “Formación de Profesorado Universitario”, and the GEOTeCH project (No 656889) founded by the European Union under the “Horizon 2020 Framework Programme for European Research and Technological Development” / Marchante Avellaneda, J. (2023). Study of Response Surface Models for the characterization of the performance in Refrigeration Equipments and Heat Pumps [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/192653