The present dissertation reports the findings of a study of cracking behavior of a newly developed superalloy, Allvac 718Plus during high power beam welding and post-weld heat treatment. Microstructures of the base alloy, heat affected zone (HAZ) and fusion zone (FZ) of welded and post-weld heat treated (PWHT) coupons were examined by the use of standard metallographic techniques involving optical microscopy, analytical scanning electron microscopy (SEM) and analytical transmission electron microscopy. Moreover, grain boundary segregation behavior of boron atoms during pre-weld heat treatments was evaluated using secondary ion mass spectroscopic system. In the first phase of the research, 718Plus was welded using a low and high heat input CO2 laser to assess its weld cracking response. Detailed examination of the welds by analytical electron microscopic technique revealed the occurrence of cracking in the HAZ of low heat input welds, while their FZ was crack free. However, both the FZ and HAZ of high heat input welds were crack-free. Resolidified constituents were observed along the cracked grain boundaries of the lower heat input welds, which indicated that HAZ cracking in this newly developed superalloy was associated with grain boundary liquation. However, despite a more extensive liquation of grain boundaries and grain interior in the HAZ of high heat input welds, no cracking occurred. This was attributed to the combination of lower welding stresses generated during cooling, and relaxation of these stresses by thick intergranular liquid. Although HAZ cracking was prevented by welding with a high heat input laser, it resulted in a significant damage to the parent microstructure through its extensive liquation. Thus, the use of low heat input welding is desirable. However, this resulted in HAZ cracking which needs to be minimized or eliminated. Therefore, during the second phase of this research, the effects of pre-weld thermal processing on the cracking response of 718Plus were investigated. Results from the quantification of the cracking of the alloy showed that HAZ cracking may be significantly reduced or eliminated through an adequate selection of pre-weld thermal cycle. In the third stage of this research, crack-free welds of 718Plus were post-weld heat treated using standard thermal schedules. A significant solid state cracking of the alloy occurred during the PWHT. The cracking was attributed to the presence of embrittling phases on HAZ grain boundaries, coupled with aging contraction stresses that are generated by a considerable precipitation of gamma prime phase during aging.

The present dissertation reports the findings of a study of cracking behavior of a newly developed superalloy, Allvac 718Plus during high power beam welding and post-weld heat treatment. Microstructures of the base alloy, heat affected zone (HAZ) and fusion zone (FZ) of welded and post-weld heat treated (PWHT) coupons were examined by the use of standard metallographic techniques involving optical microscopy, analytical scanning electron microscopy (SEM) and analytical transmission electron microscopy. Moreover, grain boundary segregation behavior of boron atoms during pre-weld heat treatments was evaluated using secondary ion mass spectroscopic system. In the first phase of the research, 718Plus was welded using a low and high heat input CO2 laser to assess its weld cracking response. Detailed examination of the welds by analytical electron microscopic technique revealed the occurrence of cracking in the HAZ of low heat input welds, while their FZ was crack free. However, both the FZ and HAZ of high heat input welds were crack-free. Resolidified constituents were observed along the cracked grain boundaries of the lower heat input welds, which indicated that HAZ cracking in this newly developed superalloy was associated with grain boundary liquation. However, despite a more extensive liquation of grain boundaries and grain interior in the HAZ of high heat input welds, no cracking occurred. This was attributed to the combination of lower welding stresses generated during cooling, and relaxation of these stresses by thick intergranular liquid. Although HAZ cracking was prevented by welding with a high heat input laser, it resulted in a significant damage to the parent microstructure through its extensive liquation. Thus, the use of low heat input welding is desirable. However, this resulted in HAZ cracking which needs to be minimized or eliminated. Therefore, during the second phase of this research, the effects of pre-weld thermal processing on the cracking response of 718Plus were investigated. Results from the quantification of the cracking of the alloy showed that HAZ cracking may be significantly reduced or eliminated through an adequate selection of pre-weld thermal cycle. In the third stage of this research, crack-free welds of 718Plus were post-weld heat treated using standard thermal schedules. A significant solid state cracking of the alloy occurred during the PWHT. The cracking was attributed to the presence of embrittling phases on HAZ grain boundaries, coupled with aging contraction stresses that are generated by a considerable precipitation of gamma prime phase during aging.

Le but de ce travail est d'étudier l'influence de la microstructure de roches poreuses hétérogènes sur le comportement à l'échelle macroscopique. Ainsi, nous avons caractérisé la microstructure et les propriétés micromécaniques (grâce à des tests de nano-indentation) de deux roches oolithiques poreuses (calcaire de Lavoux et minerai de fer) pour calculer leurs propriétés mécaniques et thermiques effectives. Les roches oolithiques sont constituées d'un assemblage de grains poreux (oolithes), de pores et de cristaux intergranulaires. La microscopie électronique à balayage et la tomographie 3D aux rayons X ont été utilisées pour identifier les différents composants de ces roches. Une attention particulière a été accordée à la tomographie aux rayons X car cette méthode analytique permet de caractériser le réseau poreux (taille, distribution spatiale et fraction volumique), ainsi que la forme des oolithes et des cristaux inter-oolithiques. La nouveauté de ce travail réside dans la prise en compte de la forme 3D réelle des pores. Par conséquent, nous avons approximé les oolites poreuses par des sphères et les pores de forme irrégulière par des ellipsoïdes. Cette approximation a été réalisée grâce à l'analyse en composantes principales (ACP), qui fournit les propriétés géométriques telles que la longueur des demi-axes et l'orientation des ellipsoïdes résultants. La sphéricité des oolites approximées a été calculée et les valeurs proches de 1 nous ont permis de considérer les oolithes comme des sphères. Pour vérifier l'approximation dans le cas des pores, nous avons évalué la contribution de ces pores tridimensionnels de forme irrégulière aux propriétés élastiques et thermiques effectives. Ainsi, les tenseurs de contribution de souplesse pour les pores irréguliers 3D et leurs approximations ellipsoïdales ont été calculés en utilisant la méthode des éléments finis (FEM). Ces tenseurs ont été comparés et une erreur relative a été estimée pour évaluer la précision de l'approximation. Cette erreur produit une distance maximale de 4,5% entre les deux solutions pour les pores et les ellipsoïdes, ce qui vérifie la procédure d'approximation proposée basée sur ACP. La méthode numérique FEM a été vérifiée en comparant la solution numérique des tenseurs de contribution des ellipsoïdes à la solution analytique basée sur la théorie d'Eshelby. La différence entre ces deux solutions ne dépasse pas 3%. La même méthode numérique a été utilisée pour calculer les tenseurs de contribution de résistivité thermique. Les tenseurs de souplesse et de résistivité calculés ont été utilisés pour évaluer les propriétés élastiques effectives (module élastique et coefficient de cisaillement) et la conductivité thermique effective en considérant le schéma d'homogénéisation de Maxwell en deux étapes. Les résultats ont montré une influence importante de la porosité sur les propriétés effectives. Enfin, les résultats obtenus pour les pores irréguliers ont été comparés à ceux des ellipsoïdes et ils ont montré un bon accord avec un écart maximal de 4% ce qui vérifie l'approximation des pores de forme irrégulière par des ellipsoïdes triaxiaux / The aim of this work is to study the influence of the microstructure of heterogeneous porous rocks on the behavior at the macroscopic scale. Thus, we characterized the microstructure and micromechanical properties (thanks to nano-indentation tests) of two porous oolitic rocks (Lavoux limestone and iron ore) to calculate their effective mechanical and thermal properties. Oolitic rocks are constituted by an assemblage of porous grains (oolites), pores and inter-granular crystals. Scanning electron microscopy and X-ray 3D Computed Tomography were used to identify the different components of these rocks. Particular attention was given to X-Ray computed tomography since this analytical method allows the characterization of the porous network (size, spatial distribution, and volume fraction), and the shapes of oolites and inter-oolitic crystals. The novelty of this work lies in taking into account the 3D real shape of pores. Hence, we approximated porous oolites by spheres and irregularly shaped pores by ellipsoids. This approximation was performed thanks to the principal component analysis (PCA), which provides the geometrical properties such as length of semi-axes and orientation of resulting ellipsoids. The sphericity of the approximated oolites was calculated and the values close to 1 allowed us to consider oolites as spheres. To verify the approximation in the case of pores, we evaluated the contribution of these irregularly shaped three-dimensional pores to the overall elastic properties. Thus, compliance contribution tensors for 3D irregular pores and their ellipsoidal approximations were calculated using the finite element method (FEM). These tensors were compared and a relative error was estimated to evaluate the accuracy of the approximation. This error produces a maximum discrepancy of 4.5% between the two solutions for pores and ellipsoids which verifies the proposed approximation procedure based on PCA. The FEM numerical method was verified by comparing the numerical solution for compliance contribution tensors of ellipsoids to the analytical solution based on Eshelby’s theory. The difference between these two solutions does not exceed 3%. The same numerical method was used to calculate thermal resistivity contribution tensors. Calculated compliance and resistivity contribution tensors were used to evaluate effective elastic properties (bulk modulus and shear coefficient) and effective thermal conductivity by considering the two-step Maxwell homogenization scheme. The results showed an important influence of the porosity on effective properties. Finally, the results obtained for irregular pores were compared to those for ellipsoidal ones and they showed a good agreement with a maximum deviation of 4% which verifies once again the approximation of irregularly shaped pores by tri-axial ellipsoids

More complex and bigger structures have increased the applicability of low alloy high strength steels due to weight and cost reductions in these projects. One of the requirements for the use of these materials is the preservation of performance after welding. Meanwhile, the norms on which the Welding Procedures Specifications (WPS) are based have not yet considered the development of modern steel and its new production process, resulting in unnecessary welding costs that diminish the profits of the application of this type of steel. This thesis aimed to develop and evaluate an experimental methodology to guide the creation and control of welding procedures for structural steel through a microstructural atlas of the heat affected zone (HAZ) in a thermomechanical control process (TMCP), 65 ksi steel (ASTM A572 Grade 65). This steel was used in the project of an industrial building for CBMM in Araxá, Minas Gerais, Brazil. It is proposed that through a microstructural atlas of a given steel, it is possible to determine the range of cooling rates that the steel may suffer during welding without affecting mechanical properties and without risking cold cracks. When comparing the microstructure of steel welds performed in field conditions, it is possible to determine the heat input range for a given process in the preparation of a WPS. The selected case study is from a high strength low alloy class 65 ksi steel (ASTM A572 Grade 65) that was used in the structure of an industrial building. The steel was produced using TMCP. The atlas was created via the construction of a continuous cooling transformation diagram using physical simulation (dilatometer and Gleeble) of the coarse grain HAZ (GCHAZ). The characterization of the simulated region was performed by metallography and mechanical tests. The microstructure of real welds made by a qualified WPS were compared to the atlas in order to certify the correct use of parameters and to validate the method. The methodology was also qualified and the potential economic benefits were quantified (based only on the reduction of consumables used and the increased availability of the welding process machine) for the selected industrial project. The mapped microstructures varied from martensite (at high cooling rates) to pearlite/ferrite with large grain size (at low cooling rates). There was remarkable prevalence of bainitic microstructure in a wide range of cooling rates, consistent with the chemical composition of the steel studied. Comparisons with real weld microstructures showed the atlas is compatible with them, and that it can more accurately describe the effective thermal cycle xi that occurs in the coarse grain region of the HAZ (other regions were not included). The application of this methodology in the development of new WPS would allow greater flexibility in the welding procedures, including welding without preheating. In this respect alone, it was possible to forecast savings of approximately R$200,000.00, 1,000 hours of processing and 172 tonnes of carbon equivalent emissions. / Estruturas cada vez mais complexas e de maiores dimensões vêm aumentando a aplicabilidade de aços de baixa liga e alta resistência, devido à redução de peso e custo dessas estruturas. Um dos requisitos para o uso desses materiais é a manutenção do desempenho após soldagem. Entretanto, as normas em que se baseiam as Especificações de Procedimentos de Soldagem (EPS) ainda não consideram aços mais modernos em termos de rota de fabricação, o que pode fazer com que custos desnecessários de soldagem minimizem os ganhos da aplicação desses aços. Este trabalho teve como objetivo o desenvolvimento e avaliação de uma metodologia para, experimentalmente, orientar a elaboração e o controle da aplicação de procedimentos de soldagem para aços estruturais, através de atlas microestrutural de regiões da zona afetada pelo calor (ZAC). Propõe-se que, através de um atlas microestrutural de um dado aço, seja possível determinar a faixa otimizada de energia de soldagem para um dado processo na elaboração e aplicação da EPS e, consequentemente, as velocidades de resfriamento que o aço possa sofrer durante a soldagem, sem perder as propriedades mecânicas e sem colocálo em risco quanto a trincas a frio. Tomou-se como estudo de caso o aço produzido por laminação controlada de classe de resistência de 65 ksi (ASTM A572 Grau 65), utilizado em um projeto de um prédio industrial na empresa CBMM. Trata-se de um aço fabricado pelo processo TMCP com resfriamento acelerado. A elaboração do Atlas se deu através da construção de um diagrama CCT, por simulação física (dilatômetro e Gleeble), da região de grãos grosseiros da zona afetada pelo calor (ZAC GG). Foram feitas caracterizações metalográficas e mecânicas das regiões simuladas. Microestruturas de soldas realizadas com EPS qualificadas foram comparadas com as do Atlas para se certificar da adequabilidade dos parâmetros utilizados e validação da abordagem. Foram realizadas ainda a qualificação e quantificação de potenciais benefícios econômicos no citado projeto industrial, obtidos pelo uso desta metodologia. As microestruturas apresentadas no mapa variavam de martensíta, para altas taxas de resfriamento, até perlita/ferrita de tamanho de grão elevado, para baixas taxas de resfriamento. Observou-se notável predominância da microestrutura bainítica em uma larga faixa de taxas de resfriamento, compatível com as propriedades e composição do aço estudado (alta soldabilidade). As comparações com as microestruturas de soldas reais mostraram que o Atlas pode descrever de forma precisa o ciclo térmico efetivamente imposto ix na ZAC GG. Concluiu-se que a aplicação desta metodologia na elaboração de novas EPS permitiria uma maior flexibilidade nos procedimentos de soldagem, admitindo inclusive soldagem sem pré-aquecimento. Em relação a não necessidade de pré-aquecimento, podese prever uma economia significante de custos e redução de emissão de gases que provocam efeito estufa. / Mestre em Engenharia Mecânica

En usinage, la zone de coupe présente des conditions de température, des cinétiques thermiques, des déformations et des pressions extrêmes. Dans ce contexte, être capable de relier les variations des conditions de coupe (vitesse de coupe, avance, lubrification, usure, outil,…) à l’intégrité de la surface usinée constitue un objectif scientifique majeur. Cette thèse s’intéresse au cas du tournage finition du 15-5PH (acier inoxydable martensitique utilisé, entre autre, pour la fabrication des pièces de rotor d’hélicoptère ainsi que les pompes et les vannes de circuit primaire de centrale nucléaire) et s’inscrit dans le cadre du projet MIFSU (Modélisation de l’Intégrité et de la Fatigue des Surfaces Usinées).Dans un premier temps, le comportement du matériau a été étudié afin d’alimenter les simulations d’usinage. Des essais de dilatométrie libre ont été conduit afin de calibrer les cinétiques d’austénitisation du 15-5PH pour des vitesses de chauffe élevées (jusqu’à 11000 °C/s). Les paramètres du modèle de changement de phase de Leblond ont alors été identifiés. De plus, des essais de compression dynamique (dε/dt allant de 0.01 à 80 /s et ε > 1) ont été réalisés pour calibrer une loi de comportement élasto-plastique aux grandes déformations avec une sensibilité à la vitesse de déformation. Ces essais ont aussi permis de mettre en évidence des phénomènes de recristallisation dynamique et leurs influences sur la contrainte d’écoulement du matériau. Un modèle de recristallisation dynamique a donc également été mis en œuvre.En parallèle, un modèle numérique de prédiction de l’intégrité des surfaces tournées a été construit. Ce modèle repose sur une méthodologie dite « hybride » (développée au cours de la thèse Frédéric Valiorgue pour l’acier AISI 304L) qui consiste à supprimer la modélisation de l’outil de coupe et de la formation du copeau, et à remplacer l’impact thermomécanique de ces derniers sur la surface usinée par des chargements équivalents. Une étape de calibration de ces chargements a donc été réalisée à travers des essais de coupe orthogonale et de frottement (étude de sensibilité des efforts d’usinage, du coefficient de frottement et du coefficient de partage thermique) aux variations des paramètres de coupe.Enfin, les résultats des simulations numériques de tournage portant sur la prédiction des changements de microstructure (austénitisation et recristallisation dynamique) ainsi que des contraintes résiduelles ont été comparés aux résultats issus d’une campagne d’essais de chariotage. / During machining, extreme conditions of pressure, temperature and strain appear in the cutting zone. In this thermo-mechanical context, the link between the cutting conditions (cutting speed, lubrication, feed rate, wear, tool coating…) and the machining surface integrity represents a major scientific target. This PhD study is a part of a global project called MIFSU (Modeling of the Integrity and Fatigue resistance of Machining Surfaces) and it focuses on the finish turning of the 15-5PH (a martensitic stainless steel used for parts of helicopter rotor). Firstly, material behavior has been studied in order to provide data for machining simulations. Stress-free dilatometry tests were conducted to obtain the austenitization kinetics of 15-5PH steel for high heating rates (up to 11,000 ° C/s). Then, parameters of Leblond metallurgical model have been calibrated. In addition, dynamic compression tests (dε/dt ranging from 0.01 to 80/s and ε > 1) have been performed to calibrate a strain-rate dependent elastoplasticity model (for high strains). These tests also helped to highlight the dynamic recrystallization phenomena and their influence on the flow stress of the material. Thus, recrystallization model has also been implemented.In parallel, a numerical model for the prediction of machined surface integrity has been constructed. This model is based on a methodology called "hybrid" (developed during the PhD thesis of Frédéric Valiorgue for the AISI 304L steel). The method consists in replacing tool and chip modeling by equivalent loadings (obtained experimentally). A calibration step of these loadings has been carried out using orthogonal cutting and friction tests (with sensitivity studies of machining forces, friction and heat partition coefficients to cutting parameters variations).Finally, numerical simulations predictions of microstructural changes (austenitization and dynamic recrystallization) and residual stresses have been successfully compared with the results of an experimental campaign of turning.

La microstructure des matériaux constitue un outil essentiel pour optimiser les propriétés mécaniques des structures et ainsi améliorer leurs performances. Les modèles de Cauchy ne sont pas toujours adaptés à la description de la réponse dynamique de certains matériaux microstructurés montrant des comportements mécaniques exotiques. Les théories de milieux continus généralisés peuvent être de bonnes candidates pour modéliser ces matériaux d’une façon plus précise et plus réaliste, aussi bien en statique qu’en dynamique, puisqu’elles peuvent décrire, même d’une façon simplifiée, la manifestation macroscopique de la présence d’une microstructure. Ce manuscrit est organisé comme suit : - Dans le chapitre 1 nous introduisons les aspects généraux de la mécanique des renforts fibreux.- Dans le chapitre 2 nous rappelons certains concepts fondamentaux concernant la mécanique des milieux continus classiques. De plus, nous introduisons les théories de deuxième gradient à l’aide du Principe des Travaux Virtuels.- Dans le chapitre 3 nous nous proposons de présenter une première modélisation des renforts fibreux de composites en mettant en place des modèles numériques discrets. Cette modélisation discrète permet de rendre compte de certains effets de la microstructure des renforts fibreux sur leur comportement macroscopique global. En particulier, il sera montré que la flexion locale des mèches à l’échelle mesoscopique a un effet non-négligeable sur le comportement macroscopique global de ces matériaux. Dans un deuxième moment nous introduisons une modélisation continue de deuxième gradient pour la description des mêmes matériaux et nous montrons que les termes d’ordre supérieur permettent une description satisfaisante des effets de flexion locale sur-cités.- Dans le chapitre 4 on particularise le cadre général de la mécanique des milieux continus introduit dans le chapitre 2 au cas particulier des milieux continus 2D. On mettra un accent fort sur l’interprétation géométrique des mesures de déformation de deuxième gradient qui seront directement reliées aux courbures dans le plan de certaines lignes matérielles. Ces lignes matérielles seront ensuite interprétées dans les chapitres suivantes comme décrivant les mèches des renforts fibreux de composites qu’on se propose d’étudier.- Dans le chapitre 5 nous introduisons une hypothèse cinématique forte sur les déformations admissibles, en supposant que les mèches du renfort considéré sont inextensibles. Cette hypothèse nous permettra de construire un modèle simplifié de premier gradient pour le comportement des renforts de composites 2D qui est encore représentatif de leur comportement mécanique. Une méthode numérique permettant de montrer certaines solutions concernant le cas du bias extension test est codée en Mathematica et les résultats obtenus sont discutés. / Dered materials in the simplest and more effective way. However, there are some cases in which the considered materials are heterogeneous even at relatively large scales and, as a consequence, the effect of microstructure on the overall mechanical behavior of the medium cannot be neglected. In such situations, Cauchy continuum theory may not be useful to fully describe the mechanical behavior of considered materials. It is in fact well known that such continuum theory is not able to catch significant phenomena related to concentrations of stress and strain and to specific deformation patterns in which high gradients of deformation occur and which are, in turn, connected to particular phenomena which take place at lower scales. Generalized continuum theories may be good candidates to model such micro-structured materials in a more appropriate way since they are able to account for the description of the macroscopic manifestation of the presence of microstructure in a rather simplified way. 
The present manuscript is organized as follows: In ch.1 a general description of fibrous composite reinforcements is given. In ch.2 some fundamental issues concerning classical continuum mechanical models are recalled. In ch.3 we start analyzing some discrete and continuum models for the description of the mechanical behavior of 2D woven composites. At this stage of the manuscript, we want to show how some discrete numerical simulations allowed us to unveil some very special deformation modes related to the effect of the local bending of fibers on the overall macroscopic deformation of fibrous composite reinforcements. Such discrete simulations showed rather clearly that microscopic bending of the fibers cannot be neglected when considering the deformation of fibrous composite reinforcements. For this reason, we subsequently introduced a continuum model which is able to account for such microstructure-related effects by means of second gradient terms appearing in the strain energy density. In ch.4 we reduce the general continuum mechanical framework introduced in ch.2 to the particular case of 2D continua. In ch.5 we introduce a strong kinematical hypothesis on the admissible deformations, assuming that the yarns composing the woven reinforcements are inextensible.

Un acier austénitique stabilisé au titane, le 15-15Ti AIM1, a été choisi à l'état écroui comme matériau de référence des gaines de combustible du premier coeur d'ASTRID (prototype de Réacteur à Neutrons Rapides (RNR) refroidi au sodium). Cette étude contribue à la compréhension de l'évolution microstructurale sous irradiation de l'AIM1 à forte dose (>100 dpa) et en particulier des mécanismes de gonflement. Des campagnes d'irradiations aux ions de l'AIM1 et de son précurseur le 15-15Ti D4 (AIM1 sans phosphore), ont été menées sur l'installation Jannus-Saclay. Ces irradiations ont été réalisées jusqu'à une dose de 150 dpa en simple faisceau Fe2+ et 120 dpa en double faisceaux Fe2+ et He+ entre 550 et 630°C pour étudier les effets de l'hélium. En parallèle, des recuits thermiques à 650°C de durées comparables aux temps d'irradiation (<100h) ont été réalisés pour séparer les effets de la température et de l'irradiation. Les microstructures et les défauts d'irradiation ont été caractérisés principalement au microscope électronique à transmission (MET) et à la sonde atomique tomographique (SAT). Pendant les recuits thermiques à 650°C, une précipitation rapide de carbures de titane nanométriques sur les dislocations est observée. Une faible densité d'amas enrichis en phosphore (germes de phosphures) a également été détectée. Après irradiation aux ions, la microstructure de l'AIM1 et du 15-15Ti fait apparaître une population dense de boucles fautées de Frank reparties de manière homogène et qui évolue peu avec la dose (entre 45 et 150 dpa). La précipitation est constituée principalement de carbures de titane nanométriques, de phosphures (dans l'AIM1) et de carbures de chrome. La précipitation de phosphures dans l'AIM1 apparait accélérée par l'irradiation. Une ségrégation du Ni et du Si sur les dislocations est aussi mise en évidence. Les irradiations en simple faisceau même à 150 dpa créent une faible densité de cavités réparties de façon hétérogène dans les grains. Il a été montré que l'implantation simultanée d'hélium à 1 appm/dpa conduit à une densité de cavités nettement plus élevée. Dans ce cas, une association entre les cavités et les nanoprécipités (TiC et phosphures) est observée. Enfin une première comparaison entre les irradiations aux ions et aux neutrons sur le 15-15Ti D4 souligne de notables différences dans l'évolution de la précipitation et les mécanismes de formation des cavités. Un modèle de dynamique d'amas avec le code Crescendo permet de modéliser la formation des boucles de Frank, des cavités et l'évolution du réseau de dislocations et prend en compte la production d'hélium. Les paramètres du modèle ont été ajustés pour reproduire les données expérimentales des irradiations en simple faisceau à 630°C. L'extrapolation du modèle illustre le décalage du pic de gonflement vers les basses températures quand le taux de dommage diminue. Le modèle prenant en compte la présence de l'hélium reproduit l'augmentation de la densité de cavités observée en double faisceaux Fe-He / A cold-worked titanium stabilized austenitic steel, named 15-15Ti AIM1, is the reference material for fuel cladding to be used in the _rst core of ASTRID (prototype of Sodium cooled Fast neutron Reactor -SFR). This study contributes to the understanding of the microstructural evolution under high dose irradiation of AIM1 (> 100 dpa) and especially swelling mechanisms. Several ion irradiations of AIM1 and its precursor 15-15Ti D4 (AIM1 without phosphorus), were done at Jannus-Saclay facility. These irradiations were performed up to 150 dpa in single beam (Fe 2+) and up to 120 dpa in dual beams (Fe 2+ and He +) at a temperature set between 550 and 630 ° C in order to study the helium e_ects. Besides, thermal annealing at 650 ° Cequivalent to irradiation time (<100h) was carried out to separate the effects of temperature and irradiation. The microstructures and the irradiation-induced defects were characterized mainly by the transmission electron microscopy (TEM) and tomographic atom probe (SAT). During thermal annealing at 650 ° C, rapid precipitation of nanometric titanium carbides over dislocations was observed. A low density of phosphorus-enriched clusters (phosphide nucleation) was also detected. After irradiation with ions, the microstructure of AIM1 and 15-15Ti revealed high density of Frank faulted-loops distributed homogeneously and which didn'tevolve with the irradiation dose (between 45 and 150 dpa). The precipitation of nanometric titanium carbides, phosphides (in AIM1) and chromium carbides was observed. Precipitation of phosphides in AIM1 is accelerated by irradiation. Irradiation_induced segregation of Ni and Si on dislocations has also been highlighted. Single-beam irradiations even at 150 dpa show very low cavities density distributed heterogeneously in the grains. It is shown that the simultaneous injection of 1 appm / dpa helium leads to much higher cavity density. In this case, cavities are attached to nanoprecipitates (TiC and phosphides). Finally, a comparison between ion and neutron irradiation on 15-15Ti D4 highlighted significant differences in the evolution of precipitation and cavity formation mechanisms. A cluster dynamics model with the Crescendo code was used to simulate the formation of Frank loops, cavities and the evolution of the dislocation network, taking into account the helium production. The model parameters were adjusted to reproduce the experimental single beam irradiation data at 630°C. The extrapolation of the model shows the displacement of the swelling peak at low temperatures as the rate of damage decreases. Taking into account the presence of Helium, the model reproduces the increase of cavity density observed in double Fe-He beams.

[pt] A presente tese tem como objetivo estudar a estabilidade microestrutural da superliga 625 a base de Ni pelas suas propriedades mecânicas e suas várias aplicações na indústria, em três condições distintas: maciça (placa forjada industrialmente), partículas de pó precursora da peça 3D e uma peça produzida por impressão a laser (Deposição Direta de Metais - DMD). Amostras destas condições foram submetidas a tratamentos de solubilização e envelhecimento isotérmico a 650 graus Celsius e 750 graus Celsius durante 10 horas e 100 horas, de modo a promover fenômeno de precipitação e, assim, correlacionar com as propriedades mecânicas do material. A caracterização microestrutural foi realizada por microscopia ótica (MO), microscopia eletrônica de varredura (MEV), microscopia eletrônica de transmissão (MET) no modo convencional utilizando contraste de difração, na modalidade analítica de transmissão/varredura (STEM), e em alta resolução (HRTEM). Espectroscopias de raios X por dispersão em energia (EDS) e de perdas de energia de elétrons (EELS) foram utilizadas para analisar a composição local da matriz e das fases presentes. Foram realizados ensaios de microdureza para avaliar o efeito dos tratamentos térmicos. A análise microestrutural da amostra maciça na condição como recebida apresentou grãos equiaxiais com fases NbTiC e M6C. Com o tratamento térmico de solubilização a 1100 graus Celsius por 40 minutos houve uma dissolução parcial dos carbetos. O envelhecimento a 650 graus Celsius por 10 horas resultou em carbetos de NbTiC e um aumento da dureza em 5 porcento em relação a amostra como solubilizada. Entretanto no tratamento de envelhecimento a 100 horas ocorreu precipitação homogênea da fase gama aumentando a dureza do material em 45 porcento, se comparada à mesma como solubilizada. A liga maciça envelhecida a 750 graus Celsius por 10 horas apresentou os carbetos NbTiC e M23C6 nos contornos de grãos e dispersos na matriz. Já a liga maciça envelhecida por 100 horas a esta mesma temperatura, apresentou a fase δ dispersa na matriz. A análise microestrutural do pó precursor mostrou ser policristalino constituído predominantemente de grãos colunares da matriz austenítica. Análises das amostras produzidas por DMD como recebida revelou estrutura dendrítica com carbetos de Nb e fase Laves nas regiões interdendríticas. A solubilização das amostras DMD durante 40 minutos por 1100 graus Celsius e 1200 graus Celsius mostrou ser insuficientes para a dissolução dos precipitados. A fim de melhorar a difusão do Nb e a dissolução dos carbetos e da fase Laves, foi realizado o tratamento de solubilização a 1200 graus Celsius por 100 horas. Esta amostra tratada a 650 graus Celsius por 100 horas apresentou carbetos M23C6 precipitados nos contornos de grão e nas interfaces entre matriz CFC e a fase Laves. Entretanto, no envelhecimento a 750 graus Celsius durante 100 horas ocorreu à precipitação dos carbetos M23C6 e M6C nos contornos de grão e dispersos na matriz, aumentando assim a dureza do material em 18 porcento, se comparada à mesma como solubilizada. O aumento da microdureza em 12 porcento após o tratamento térmico está relacionado à precipitação dos carbetos nos contornos de grão e dispersos na matriz resultado dos tratamentos térmicos de envelhecimento. / [en] This thesis studies the microstructural stability of Ni-base Super alloy 625 for its mechanical properties and its varieties of applications in the industry, in three different conditions: bulk (industrially forged plate), precursor powder particles for 3D printing process and a sample produced by laser Direct Metal Deposition (DMD). Aiming at promoting precipitation processes and, therefore, correlate with the mechanical properties of the material, samples of these conditions were submitted to solution annealing and isothermal aging treatments at 650 Celsius degrees and 750 Celsius degrees for 10 hours and 100 hours. Characterization of the microstructure was performed by optical microscopy (OM), scanning electron microscopy (SEM), transmission electron microscopy (TEM), in the conventional diffraction contrast mode, scanning/transmission (STEM) analytical mode, and high resolution microscopy (HRTEM). Energy dispersive X-ray spectrometry (EDXS) and electron energy loss spectroscopy (EELS) were used to analyze the local composition of the matrix and precipitated phases. Micro hardness measurements were performed to evaluate the effect of thermal treatments. The microstructural analysis of the bulk sample in the as-received condition showed an equiaxial grain structure with NbTiC and M6C precipitated phases. Solid solution treatment at 1100 Celsius degrees for 40 minutes allowed partial dissolution of the carbides. Aging at 650 Celsius degrees for 10 hours showed NbTiC carbides and a hardness increase of 5 percent compared to the as-solubilized sample. However, aging at this temperature for 100 hours promoted the homogeneous precipitation of the gama phase, thus increasing the material s hardness by 45 percent, when compared to it as solubilized. The bulk sample aged at 750 Celsius degrees for 10 hours showed grain boundary and homogeneous precipitation of NbTiC and M23C6 carbides. This sample condition upon aging at this temperature for 100 hours shows δ phase homogeneously precipitated in the matrix. The microstructural analysis of the precursor powder showed micrometer size individual particles as polycrystalline, consisting predominantly of columnar grains of the austenitic matrix. Analysis of samples produced by DMD in the as-received condition revealed dendritic microstructure with carbides of Nb and Laves phase in the interdendritic regions. The solution treatment of the DMD samples for 40 minutes at 1100 Celsius degrees and 1200 Celsius degrees proved to be insufficient for the dissolution of the precipitate. In order to enhance diffusion of Nb and so carbide and Laves phase dissolution, a solution anneal was carried out at 1200 Celsius degrees for 100 hours. This sample treated at 650 Celsius degrees for 100 hours showed M23C6 carbides precipitated at grain boundaries and also at the Laves phase/matrix interfaces. However, upon aging at 750 Celsius degrees for 100 hours the precipitation of M23C6 and M6C takes place at the grain boundary and in the austenitic matrix, thus increasing the material s hardness by 18 percent, when compared to it as solubilized. The increase of the hardness by 12 percent after the heat treatment is related to the precipitation of the carbides in the grain boundaries and dispersed in the matrix resulting from the aging thermal treatments.

Additive manufacturing technologies, particularly electron beam powder bed fusion (PBF-EB/M), are becoming increasingly important for the processing of intermetallic titanium aluminides. This study presents the effects of hot isostatic pressing (HIP) and subsequent two-step heat treatments on the microstructure and mechanical properties of the TNM-B1 alloy (Ti–43.5Al–4Nb–1Mo–0.1B) fabricated via PBF-EB/M. Adequate solution heat treatment temperatures allow the adjustment of fully lamellar (FL) and nearly lamellar (NL-β) microstructures. The specimens are characterized by optical microscopy and scanning electron microscopy (SEM), X-ray computed tomography (CT), X-ray diffraction (XRD), and electron backscatter diffraction (EBSD). The mechanical properties at ambient temperatures are evaluated via tensile testing and subsequent fractography. While lack-of-fusion defects are the main causes of failure in the as-built condition, the mechanical properties in the heat-treated conditions are predominantly controlled by the microstructure. The highest ultimate tensile strength is achieved after HIP due to the elimination of lack-of-fusion defects. The results reveal challenges originating from the PBF-EB/M process, for example, local variations in chemical composition due to aluminum evaporation, which in turn affect the microstructures after heat treatment. For designing suitable heat treatment strategies, particular attention should therefore be paid to the microstructural characteristics associated with additive manufacturing.

[ES] Los procesos convencionales de transformación de materiales requieren afrontar nuevos retos que se presentan en la actual sociedad industrial como es la propia sostenibilidad medioambiental. De la misma forma, los productos fabricados en el futuro deberán cumplir ciertos requisitos medioambientales, como la reciclabilidad de la materia prima utilizada. Dentro de este contexto la fabricación de productos mediante técnicas tridimensionales como la fabricación aditiva, permite utilizar únicamente el material necesario que se requiere para un producto completo. Dichas técnicas de fabricación son las solicitadas por el sector aeronáutico, entre otros, que requiere de unos valores de calidad muy exigentes. Dentro de estos ensayos, el estudio del comportamiento del material ante crecimiento de grieta es de gran importancia. Mediante este tipo de fabricación se obtiene un producto en estado casi final a través de la adición de capas de alrededor de 100 micras, que da como resultado una orientación de grano metalúrgico preferente y diferente a la misma aleación fabricada por forja convencional. Los fenómenos ocurridos durante la fabricación pueden dar lugar a defectos como grietas o porosidades que disminuyen las capacidades resistentes, por lo que un estudio para predecir la vida del componente es importante. Dentro de los procesos de fabricación aditiva nos encontramos con la fabricación por haz de electrones, que consigue calidades de material casi con porosidad nula, por lo que empresas del sector aeronáutico o médico consideran esta técnica como de gran fiabilidad. El trabajo desarrollado en esta tesis se basa en el estudio de aleaciones de titanio fabricadas mediante fabricación aditiva por haz de electrones. En concreto, el estudio se centra en el comportamiento a tenacidad a la fractura para relacionarlo con las características microestructurales más relevantes. Los análisis llevados a cabo consideran diversas orientaciones que tienen lugar en la bandeja de fabricación, realizándose ensayos mecánicos tanto estáticos como dinámicos. Una segunda parte de la tesis se basa en el modelado mediante elementos finitos extendido, XFEM, que se desarrolla como alternativa a los métodos tradicionales de mallado. En el XFEM una aproximación de elementos finitos se construye de forma que sea capaz de representar funciones de enriquecimiento dentro de los elementos mediante grados de libertad adicionales. Un punto crítico en el proceso de cálculo mediante elementos finitos es el proceso de mallado. La precisión obtenida en la aproximación depende del tamaño de los elementos de la malla. Por tanto, el cálculo con precisión en puntos importantes como la zona cercana a grieta exige una malla con un tamaño de elemento muy pequeño. Con la técnica XFEM se alcanza una mayor precisión mediante un proceso de enriquecimiento de extremo de grieta. Los resultados que ofrece la herramienta XFEM se comparan con los obtenidos experimentalmente con componentes fabricados mediante impresión 3D. Esta comparativa se lleva a cabo sobre diversas geometrías con la presencia de agujeros, de tal forma que se ha podido predecir el crecimiento de grieta que tiene lugar en materiales por impresión 3D. De la misma forma, se llevan a cabo comparativas de piezas con geometría compleja, para validar el modelo desarrollado. / [CA] Els processos convencionals de transformació de materials requereixen afrontar nous reptes que es presenten en l'actual societat industrial com és la pròpia sostenibilitat mediambiental. De la mateixa forma, els productes fabricats en el futur hauran de complir certs requisits mediambientals, com el reciclatge de la matèria primera. Dins d'aquest context, la fabricació de productes mitjançant tecnologia 3D com la fabricació additiva, permet usar només el material necessari que es requereix per a un producte complet. Aquestes tècniques de fabricació són les sol·licitades pel sector aeronàutic que requereix d'uns valors de qualitat molt exigents. Dins d'aquests assajos, l'estudi del comportament del material a través de creixement de clivella és vital. Mitjançant aquesta mena de fabricació s'obté un producte en estat quasi final a través de l'addició de capes d'alçària al voltant de 100 micres, que dona com a resultat una orientació de gra metal·lúrgic preferent i diferent al mateix però fabricat convencionalment. Els fenòmens ocorreguts durant la fabricació poden donar lloc a defectes com a clivelles o porositats que poden disminuir les capacitats resistents, per la qual cosa un estudi per a predir la vida del material és important. Dins dels processos de fabricació additiva ens trobem amb la fabricació per feix d'electrons la qual aconsegueix qualitats de material quasi amb porositat nul·la, per la qual cosa empreses del sector aeronàutic i mèdic han conclòs a aquesta tècnica com la més fiable. El treball desenvolupat en aquesta tesi es basa en l'estudi d'aliatges de titani fabricades mitjançant fabricació additiva per feix d'electrons, principalment el seu comportament a la tenacitat a la fractura per a relacionar-ho amb les característiques microestructurals més rellevants. Les anàlisis dutes a terme se centren en diverses orientacions que tenen lloc en la plataforma de fabricació, realitzant-se assajos mecànics tant estàtics com dinàmics. Una segona part de la tesi es basa en el modelatge mitjançant elements finits estesos, XFEM, que es desenvolupa com a alternativa als mètodes lliures de malla. En el XFEM una aproximació d'elements finits es construeix de manera que siga capaç de representar funcions (enriquiment) dins dels elements. Un punt crític en el procés de càlcul en qualsevol mètode que usa una malla és el procés d'emmallat. La precisió obtinguda en l'aproximació depén de la grandària dels elements de malla. Per tant, el càlcul amb precisió en punts importants, com la zona pròxima a clivella, exigeix l'ús d'una malla amb una grandària d'element molt xicoteta. Amb la tècnica XFEM aconseguim aqueixa precisió mitjançant un procés de enriquiment. / [EN] Conventional material transformation processes require facing new challenges that arise in today's industrial society, such as environmental sustainability. Similarly, products manufactured in the future must meet certain environmental requirements, such as the recyclability of the raw material used. Within this context, the manufacture of products using 3D technology such as additive manufacturing, allows using only the necessary material that is required for a complete product. These manufacturing techniques are requested by the aeronautical sector, which requires very demanding quality values. Within these tests, the study of the behavior of the material through crack growth is of great importance. By means of this manufacturing technology, a product is obtained in an almost final state through the addition of layers of about 100 microns, which results in a preferential metallurgical grain orientation and different from the same alloy manufactured by conventional methods. The phenomena occurring during manufacturing can lead to defects such as cracks or porosities that can reduce the strength capabilities, so a study to predict the life of the component is important. Within the additive manufacturing processes we find the electron beam manufacturing which achieves material qualities with almost zero porosity. As a consequence, companies in the aeronautical or medical sector have concluded this technique as very reliable. The work developed in this thesis is based on the study of titanium alloys manufactured by electron beam additive manufacturing. More precisely, the work is focused on the fracture toughness behavior in order to relate it to the most relevant microstructural characteristics. The analyses carried out consider different orientations and positions that take place in the fabrication tray, performing both static and dynamic mechanical tests. A second part of the thesis is based on the application of the extended finite element method, XFEM, which is developed as an alternative to conventional finite element method. In XFEM a finite element approximation is constructed in such a way that it is able to represent functions within the elements. A critical point in the calculation process in the finite element method is the meshing process. The accuracy obtained in the approximation depends on the size of the elements of the mesh. Therefore, accurate computation at important points such as the near-crack zone requires the use of a mesh with a very small element size. With the XFEM technique, we achieve this accuracy by means of an enrichment process. The results provided by the XFEM tool are compared with those obtained experimentally with respect to components manufactured by 3D printing. This comparison is carried out on different geometries with the presence of holes, in such a way that it has been possible to predict the crack growth that takes place in 3D printed materials. In the same way, comparisons of parts with complex geometry are carried out to validate the developed model. / Niñerola González, R. (2022). Estudio del comportamiento por crecimiento de grieta de aleaciones fabricadas por adición mediante haz de electrones [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/183818