Dans le domaine du renforcement et/ou de la réparation des structures en béton armé par des matériaux composites à l'aide de la méthode du collage extérieur au moyen d'un adhésif époxy, une des préoccupations de la communauté scientifique est l'intégrité structurelle de ce système dans le cas d'incendie dans lequel la haute température est une caractéristique essentielle et peut atteindre jusqu'à 1200°C. Ce travail de recherche est axé sur le comportement thermomécanique à très haute température des matériaux composites [un composite à base de polymère carbone/ époxy (Carbon Fiber Reinforced Polymer- CFRP), un composite textile/ mortier cimentaire (Textile Reinforced Concrete- TRC) et un adhésif à base d'époxy]. L'évolution des propriétés mécaniques et d'autres aspects mécaniques de ces matériaux composites avec la température a été caractérisée. Une nouvelle procédure expérimentale concernant la mesure de la déformation de l'éprouvette à l'aide du capteur laser est développée et validée. Une étude numérique et expérimentale a été réalisée dans le but de déterminer principalement la température à la rupture des joints « composite/ adhésif/ composite » sous les sollicitations mécaniques et thermiques. L'efficacité de la protection thermique de deux isolants [PROMASPRAY®T (produit commercial de la société PROMAT] et Isolant A (produit développé par le LGCIE site Tusset) a aussi été étudiée dans cette thèse. Enfin, une approche numérique, à l'aide du logiciel ANSYS, est utilisée afin de déterminer, de façon préliminaire et approximative, à l'échelle matériau, les propriétés thermiques des matériaux (composite textile/ mortier cimentaire -TRC et Isolant A) / In the area of the strengthening and/or the reparation of reinforced concrete structures with composites by means of the external bonding method using an epoxy adhesive, one of the preoccupation of the scientific community is the structural integrity of this system in the event of fire in which the high temperature is the essential feature et can reach up to 1200°C. This research focuses on the thermo-mechanical behavior of composite materials [carbon/epoxy adhesive composite (or carbon fiber reinforced polymer (CFRP), textile/cementitious mortar composite (or textile reinforced concrete (TRC)] and an epoxy-based adhesive. The evolution of mechanical properties and other mechanical aspects of these materials with the temperature has been characterized. A new experimental procedure concerning the measurement of sample strain by the laser sensor is developed and validated. An experimental and numerical study has been realized in order to mainly determine the temperature at the failure of "composite/adhesive/composite" joints under thermal and mechanical loadings. The effectiveness of the thermal protection of two insulators [PROMASPRAY®T (a commercial product of the PROMAT company and the insulator A (product developed by the LGCIE site Tuset)] has also been investigated in this PhD thesis. Finally, a numerical approach, using ANSYS software, is used to determine, in the preliminary and approximate way, at material scale, thermal properties of the materials [the textile reinforced concrete (TRC) and the insulator A]

Les composites Carbone/Carbone (C/C), largement utilisés à hautes températures dans des environnements oxydants, sont sensibles à l'oxydation dès 400°C. Deux voies sont envisagées pour accroître la tenue à l'oxydation de ces matériaux. La première est de renforcer la force de la liaison fibre/matrice en modifiant les propriétés de surface des fibres de carbone. La seconde voie d 'étude consiste à remplacer une partie de la matrice carbone par un oxyde. L'introduction d'une nouvelle phase conduit à la création de nouvelles interfaces dans les matériaux. L'ensemble des résultats obtenus à partir des caractérisations physico-chimiques et macroscopiques des matériaux élaborés permettent alors de répondre à la problématique qui est de connaître le rôle des interfaces dans les propriétés macroscopiques de composites C/C. / C/C composites are widely used as structural parts in oxiding environment. Yet, they become very sensitive to air oxidation for temperature higher than 400°C. This work proposed two methods to improve their oxidation resistance :(i) the fiber/matrix bond is increased by modifying the properties of the carbon fiber surface, and (ii) a fraction of the carbon matrix is substitued by an oxide phase.Introduction of new constituants leads to the creation of new material interfaces. Thus, the influence of the interfaces on the macroscopic properties of the composite is evaluated by physico-chemical and macroscopic characterizations.

Dans le domaine de l'électronique de puissance, la gestion thermique de l'intégration des puces en silicium au sein du système global constitue un problème clé. La chaleur dissipée par les composants électriques est évacuée vers l’extérieur à travers un drain thermique, généralement en cuivre, qui est brasé sur le substrat céramique. Cette étude est consacrée à l'élaboration de drains thermiques adaptatifs en matériaux composites cuivre allié/fibres de carbone (FC) qui combinent une bonne conductivité thermique et un CTE proche de celui du substrat. Dans ce type de matériau, la liaison interfaciale renfort/matrice doit être forte afin d'optimiser le transfert des propriétés entre les deux composants. Le couple cuivre/carbone étant non réactif, un élément d’addition carburigène (Cr ou B) est ajouté à la matrice de cuivre afin de créer cette liaison chimique forte. Un matériau modèle a été réalisé par pulvérisation cathodique afin d’étudier la diffusion de l’élément d’addition au sein de la couche de cuivre vers la zone interfaciale et la formation d’un carbure métallique. Une méthode de chimie des solutions a ensuite été utilisée pour élaborer des poudres de cuivre allié de stœchiométrie donnée. Enfin, les matériaux composites (Cu-B/FC et Cu-Cr/FC) ont été élaborés par métallurgie des poudres et leurs propriétés thermiques et mécaniques corrélées à la microstructure et à la chimie des zones interfaciales / In the field of power electronics, thermal management of silicon chips plays a key role in our ability to increase their performance. Heat generated by the electronic components is dissipated through the heat sink, generally made of Copper that is brazed on to a ceramic substrate. This study focuses on the elaboration of adaptive heat sink material using Copper alloys/Carbon fibers (CF) composite materials which have a good thermal conductivity and a CTE close to the ceramic substrate. In this kind of material, it is necessary to have a strong matrix/reinforcement link in order to optimize transfer properties. Since there is no reaction between Copper and Carbon, a carbide element (Cr or B) is added to the Copper matrix to create this strong chemical bond. A model material has been elaborated by cathode sputtering in order to study the diffusion of the alloying element in the Copper layer and the metallic carbide formation in the interfacial zone. Copper alloy powders, with a given stoichiometry, have also been synthesized by a chemical method. Lastly, composite materials (Cu-B/CF and Cu-Cr/CF) have been elaborated by a powder metallurgy process and their thermal and mechanical properties correlated to the microstructure and the chemistry of the interfacial zones.

Si l'emploi des matériaux composites dans l'aéronautique est déjà effectif sur des éléments de structures principales et de grande taille, leur généralisation aux structures secondaires bute sur leur positionnement en termes de coûts et performances face aux métaux. Il s'agit dans ce travail de contribuer à la mise en place d'une filière française de pièces composites hautes performances à bas coûts en s'appuyant sur un procédé de moulage en grande série, à savoir le thermoformage à haute pression. Ainsi, il a été question dans un premier temps d'optimiser ce procédé vis-à-vis des principales matières rencontrées dans les structures aéronautiques. Ensuite, les stratifiés moulés ont été caractérisés et les effets des conditions environnementales sévères (humidité, température, impact) sur leur comportement mécanique étudiés. Par ailleurs, réduire les coûts des pièces signifie également réduire les coefficients de sécurité qui restent très élevés pour les pièces composites. Cela passe par une meilleure prédictibilité de la rupture des matériaux et du comportement mécanique au-delà du linéaire. Sur le carbone/PEEK satin de 5 pris comme matériau d'illustration, les phénomènes non linéaires (viscoplasticité) ainsi que les mécanismes d'endommagement et de rupture ont été étudiés. Un accent particulier a été mis sur le délaminage et un critère permettant de prédire son amorçage a été proposé. La possibilité de faire des modèles éléments finis des pièces directement à l'échelle mésoscopique (du pli) a été également explorée et laisse entrevoir des pistes prometteuses pour des dimensionnements plus sûrs et donc moins conservatifs. / If the use of composite materials is already effective on elements of main structures and large size parts, their generalization to secondary parts is not effective due to their cost and their performances compared to metals. The framework of this thesis is to contribute to the establishment of a French chain of high performance composite parts at low cost. Thus, it was initially question of optimizing the process vis-à-vis the main composite materials used in the aerospace structures. Then, the molded laminates were characterized and the effects of severe conditions (humidity, temperature, impact) on their mechanical behavior were studied. Also, reduce the cost of parts also means reducing the safety factors which remain very high. This requires a better prediction of the failure and the mechanical behavior beyond the linear. Taking the five harness satin weave carbon/PEEK material as example, non-linear phenomena (viscoplasticity), damage mechanisms and failure criteria were studied, with particular emphasis on the delamination. The possibility to perform finite element analysis of the parts directly at the mesoscopic scale (ply-scale) was also explored and suggests promising expectations for a less conservative sizing of composite structures.

[pt] A necessidade cada vez mais freqüente de reforço em estruturas de concreto armado, exige um completo conhecimento do comportamento da estrutura reforçada devido a alterações de rigidez do conjunto, aumento da carga de ruptura, alterações na distribuição de fissuras, modificação de comportamento e posição da linha neutra, entre outros. Nos últimos anos diversos estudos experimentais têm sido conduzidos, fornecendo parâmetros cada vez mais confiáveis à elaboração de projetos e ao dimensionamento seguro em relação aos estados limites de utilização e de ruptura. No desenvolvimento deste trabalho, utiliza-se um programa computacional baseado no método dos elementos finitos,capaz de descrever o comportamento de elementos estruturais prismáticos em concreto armado reforçados à flexão. Descreve-se o modelo hipoelástico de Elwi e Murray -1979- para o concreto simples e um modelo multilinear para simulação dos reforços. Tais relações resultam de estudos analíticos e experimentais sobre o concreto armado e estão originalmente implementadas no programa FEPARCS -Elwi e Murray, 1980-, que neste trabalho é modificado e adaptado de acordo com a realidade da execução de reforços em estruturas em serviço. O programa FEPACS, capaz de realizar análises numéricas não-lineares, é acoplado a um programa de pré e pós-processamento gráfico especialmente desenvolvido para geração, gerenciamento do processo de cálculo e para análise de resultados obtidos. Os resultados obtidos utilizando o programa proposto são validados através de uma comparação com resultados experimentais obtidos na literatura. / [en] The frequent use of composite materials, in the strengthening of reinforced concrete structures requires complete knowledge of the structural behavior because of the changes that such strengthening will cause to the overall stiffness,the collapse load, the cracks distribution and the behavior and position of the neutral axis. Over the last few years experimental studies have been performed,bringing out more trustworthy parameters for ultimate strength design. In this work, a computational program was implemented based on the finite element method, which is able to describe the flexural strengthening of reinforced concrete beams. The model used in this program is that of Elwi and Murray -1979-, which assumes a so-called hypo elastic theory for concrete and a approach to simulate the reinforcement. These relationships were derived from reinforced concrete analytical and experimental studies and are originally implemented in the FEPARCS program -Elwi and Murray, 1980-, which has been modified in order to obtain a more realistic approach to in- service structural strengthening. The program developed, which is able to perform non-linear numerical analyses, is coupled to pre and pos-processing graphic programs specially developed for model generation, management of the calculation sequence and presentation of final results. The results produced by this program have been validated by comparison with experimental results available in literature.

Orientador: Edson Cocchieri Botelho / Resumo: Este trabalho de pesquisa consiste na obtenção e caracterizações térmica, mecânica, reológica e elétrica de compósitos multifuncionais obtidos a partir da utilização de fibras de carbono (FC), resina furfurílica (RF) e nanotubos de carbono (CNT) para aplicações aeroespaciais. O uso de uma bioresina como fonte alternativa ao petróleo em compósitos multifuncionais e a avaliação dos ganhos de propriedades na utilização de nanotubos de carbono (0, 1,3 e 2,5% em volume) associados a fibras contínuas de carbono (tecido plain weave) são os objetivos principais deste trabalho. O desenvolvimento deste trabalho de pesquisa estabelece os parâmetros de processo mais adequados para a obtenção de compósitos multifuncionais com propósitos estruturais, térmicos e/ou elétricos. Neste trabalho, os compósitos multifuncionais foram processados com a utilização de moldagem por compressão a quente, sendo esta uma das contribuições desta dissertação. Após processados, os laminados foram avaliados a partir de ensaios mecânicos (cisalhamento interlaminar por compression shear test (CST), impacto a baixas velocidades, DCB (Double Cantilever Beam test), ENF (End Notched Flexure) e fadiga); assim como, a partir de análises térmicas (DMA (Análise Dinâmico-Mecânica), DSC (Calorimetria Exploratória Diferencial), TGA (Análise Termogravimétrica) e TMA (Análise Termomecânica)), ensaios elétricos, análises morfológicas (MO (Microscopia Óptica), MEV (Microscopia Eletrônica de Varredura) e ultrassom) e análises ... (Resumo completo, clicar acesso eletrônico abaixo) / Doutor

SEISMIC STRENGTHENING OF A MID-RISE REINFORCED CONCRETE FRAME USING CFRPs: AN APPLICATION FROM REAL LIFE Tan, Mustafa T&uuml / mer M.S., Department Of Civil Engineering Supervisor: Prof. Dr. G&uuml / ney &Ouml / zcebe Co-Supervisor: Assoc. Prof. Dr. BariS Binici May 2009, 162 pages FRP retrofitting allows the utilization of brick infill walls as lateral load resisting elements. This practical retrofit scheme is a strong alternative to strengthen low to mid-rise deficient reinforced concrete (RC) structures in Turkey. The advantages of the FRP applications, to name a few, are the speed of construction and elimination of the need for building evacuation during construction. In this retrofit scheme, infill walls are adopted to the existing frame system by using FRP tension ties anchored the boundary frame using FRP dowels. Results of experiments have previously shown that FRP strengthened infill walls can enhance lateral load carrying capacity and reduce damage by limiting interstory drift deformations. In previous, analytical studies, a detailed mathematical model and a simplified version of the model for compression struts and tension ties was proposed and verified by comparing model estimations with test results. In this study, an existing 9-storey deficient RC building located in Antakya was chosen to design and apply a hybrid strengthening scheme with FRPs and reduced number of shear walls. Linear elastic analysis procedure was utilized (force based assessment technique) along with the rules of Mode Superposition Method for the reftrofit design. FRP retrofit scheme was employed using the simplified model and design was conducted such that life safety performance criterion is satisfied employing elastic spectrum with 10% probability of exceedance in 50 years according to the Turkish Earthquake Code 2007. Further analytical studies are performed by using Modal Pushover and Nonlinear Time-History Analyses. At the end of these nonlinear analyses, performance check is performed according to Turkish Earthquake Code 2007, using the strains resulting from the sum of yield and plastic rotations at demand in the critical sections. CFRP retrofitting works started at October 2008 and finished at December 2008 for the building mentioned in this study. Eccentric reinforced concrete shearwall installation is still being undertaken. All construction business is carried out without evacuation of the building occupants. This project is one of the first examples of its kind in Turkey. Keywords: CFRP, Carbon Fiber Reinforced Polymers, Masonry Infill Walls, Reinforced Concrete Infill Walls, Mid-Rise Deficient Structures, Turkish Earthquake Code 2007, Modal Pushover Analysis, Nonlinear Time History Analysis, Linear Elastic Building Assessment

Heat actuated adsorption heat pumps offer the opportunity to improve overall energy efficiency in waste heat applications by eliminating shaft work requirements accompanying vapor compression cycles. The coefficient of performance (COP) in adsorption heat pumps is generally low. The objective of this thesis is to model the adsorption system to gain critical insight into how its performance can be improved. Because adsorption heat pumps are intermittent devices, which induce cooling by adsorbing refrigerant in a sorption bed heat/mass exchanger, transient models must be used to predict performance. In this thesis, such models are developed at the adsorbent particle level, heat/mass exchanger component level and system level. Adsorption heat pump modeling is a coupled heat and mass transfer problem. Intra-particle mass transfer resistance and sorption bed heat transfer resistance are shown to be significant, but for very fine particle sizes, inter-particle resistance may also be important. The diameter of the adsorbent particle in a packed bed is optimized to balance inter- and intra-particle resistances and improve sorption rate. In the literature, the linear driving force (LDF) approximation for intra-particle mass transfer is commonly used in place of the Fickian diffusion equation to reduce computation time; however, it is shown that the error in uptake prediction associated with the LDF depends on the working pair, half-cycle time, adsorbent particle radius, and operating temperatures at hand. Different methods for enhancing sorption bed heat/mass transfer have been proposed in the literature including the use of binders, adsorbent compacting, and complex extended surface geometries. To maintain high reliability, the simple, robust annular-finned-tube geometry with packed adsorbent is specified in this work. The effects of tube diameter, fin pitch and fin height on thermal conductance, metal/adsorbent mass ratio and COP are studied. As one might expect, many closely spaced fins, or high fin density, yields high thermal conductance; however, it is found that the increased inert metal mass associated with the high fin density diminishes COP. It is also found that thin adsorbent layers with low effective conduction resistance lead to high thermal conductance. As adsorbent layer thickness decreases, the relative importance of tube-side convective resistance rises, so mini-channel sized tubes are used. After selecting the proper tube geometry, an overall thermal conductance is calculated for use in a lumped-parameter sorption bed simulation. To evaluate the accuracy of the lumped-parameter approach, a distributed parameter sorption bed simulation is developed for comparison. Using the finite difference method, the distributed parameter model is used to track temperature and refrigerant distributions in the finned tube and adsorbent layer. The distributed-parameter tube model is shown to be in agreement with the lumped-parameter model, thus independently verifying the overall UA calculation and the lumped-parameter sorption bed model. After evaluating the accuracy of the lumped-parameter model, it is used to develop a system-level heat pump simulation. This simulation is used to investigate a non-recuperative two-bed heat pump containing activated carbon fiber-ethanol and silica gel-water working pairs. The two-bed configuration is investigated because it yields a desirable compromise between the number of components (heat exchangers, pumps, valves, etc.) and steady cooling rate. For non-recuperative two-bed adsorption heat pumps, the average COP prediction in the literature is 0.39 for experiments and 0.44 for models. It is important to improve the COP in mobile waste heat applications because without high COP, the available waste heat during startup or idle may be insufficient to deliver the desired cooling duty. In this thesis, a COP of 0.53 is predicted for the non-recuperative, silica gel-water chiller. If thermal energy recovery is incorporated into the cycle, a COP as high as 0.64 is predicted for a 90, 35 and 7.0°C source, ambient and average evaporator temperature, respectively. The improvement in COP over heat pumps appearing in the literature is attributed to the adsorbent particle size optimization and careful selection of sorption bed heat exchanger geometry.

Gegenstand dieser Arbeit ist die Modifizierung von Oberflächen durch die Abscheidung alternierender Schichtsysteme auf Kohlenstofffasern und die Abscheidung von Aluminiumoxid auf organischen Membranen. Im ersten Kapitel wird das Vorgehen zur Abscheidung von organischen und anorganischen Schichten auf Kohlenstofffasern mittels der Atomlagenabscheidung und der oberflächeninitiierten Gasphasenabscheidung betrachtet. Dabei wird als Erstes auf die Abscheidung von Einzellagen und deren Optimierung eingegangen sowie im Anschluss auf die Übertragung dieser Parameter auf die Abscheidung von alternierenden Multilagensystemen. Mittels elektronenmikroskopischen-Untersuchungen, Rasterelektronenmikroskopie und energiedispersiver Röntgenspektroskopie, wird die Abscheidung der Materialien untersucht. Weiterhin können mit Hilfe von thermogravimetrischen Analysen die Oxidationsbeständigkeit der beschichteten Kohlenstofffasern sowie die einzelnen Schichtdicken bestimmt werden. Im zweiten Kapitel wird auf die Beschichtung von organischen Membranen eingegangen. Das Hauptaugenmerk liegt dabei auf der Beschichtung von nicht-hierarchisch und hierarchisch strukturierten Membranen mit Aluminiumoxid. Dafür werden die Atomlagenabscheidung und die Grenzflächenreaktion der Gasphase mit der im Feststoff gebundenen Flüssigphase angewendet. Unter Anwendung dieser beiden Verfahren ist es gelungen, dünne und gleichmäßige Schichten auf den Membranen abzuscheiden. Die Charakterisierung erfolgte mittels Rasterelektronenmikroskopie und energiedispersiver Röntgenspektroskopie. Zum Schluss wurden Filtrationsexperimente zum Vergleich der Stabilität und Durchflussraten der beschichteten mit den unbeschichteten Membranen durchgeführt.

Les composites utilisés dans l'industrie aéronautique sont hétérogènes. Ils sont composés d'une matrice polymère souple et ductile et d'un renfort dur et fragile. Les différentes phases ainsi que l'anisotropie du matériau peuvent rendre l'usinage de ces matières, difficile. Deux problèmes majeurs peuvent être rencontrés lors de l'usinage : garder l'intégrité de la matière usinée et réduire l'usure de l'outil de coupe. Les niveaux de qualité demandés dans le secteur aéronautique imposent une coupe sans défaut, ces derniers pouvant entrainer une altération ultérieure de la pièce. Les principaux défauts rencontrés sont : le délaminage des plis, la surchauffe de la résine, les plis non coupés francs ou l'écaillage. / Aeronautic composites are inhomogeneous and most often consist in two distinctly phases. The reinforcement fibres are relatively hard and brittle whereas the matrix is soft and ductile. The anisotropy causes some severe challenges when machining composites. People in the field often experience a trade-off between two main problems ; on one hand, keeping the composite parts integrity and quality, and on the other hand, reducing the wear of the cutting tools. The quality level required in aeronautic applications imposes a high quality cut of machined parts. Common defects that may occur during machining of these materials are delamination, overheat of the resin, uncut fibres, and fibre pull-out.