Le couplage des traitements de surface mécaniques et thermochimiques a fait l’objet de nombreuses études ces dernières années. L’objectif d’un tel couplage est l’amélioration des cinétiques de diffusion d’espèces chimiques résultant en une augmentation des profondeurs de diffusion, et/ou une diminution de la température du traitement thermochimique sur les matériaux prétraités mécaniquement. Dans cette thèse, le procédé SMAT (Surface Mechanical Attrition Treatment) de nanocristallisation superficiel par déformation plastique sévère a été combiné avec la nitruration plasma sur un acier inoxydable 316L de qualité médicale. Ce procédé duplex permet une amélioration notable sur la capacité de diffusion de l’azote sous la surface de l’acier SMATé. Une étape intermédiaire entre le SMAT et la nitruration plasma a été proposée ; son rôle significatif pour la diffusion de l’azote a été démontré. Ainsi, la comparaison des résultats obtenus après la nitruration plasma sur les échantillons SMATés avec ceux uniquement nitrurés a permis de constater une augmentation jusqu’à 60% de l’épaisseur des couches nitrurées. Par ailleurs, de nombreux moyens de caractérisation ont été mis en œuvre à travers divers essais mécaniques de fatigue et de tribologie. Un modèle numérique multi-échelle de diffusion a également été développé pour simuler les profils de concentration d’azote après traitement duplex. Les profils de concentration d’azote simulés sont en bon accord avec les résultats expérimentaux / Coupled mechanical and thermochemical surface treatments have been the subject of much research effort in recent years. The goal of such a coupling is to improve diffusion kinetics leading to increased penetration depths, and/or to decrease the treatment temperature for mechanically pretreated materials. In this work, SMAT (Surface Mechanical Attrittion Treatment), used to refine the grain size by severe plastic deformation, is combined with plasma nitriding of a 316L medical-grade stainless steel. This duplex process significantly improves nitrogen diffusion. An intermediate treatment between SMAT and plasma nitriding is also proposed and its significant effect on the nitrogen diffusion is demonstrated. Comparisons between nitrided-only samples and duplex-treated samples have shown up to 60% increase of the nitrided layer thickness. In order to better understand the link between the generated microstructures and the mechanical fatigue and tribological responses, the samples have been characterised by many different techniques. Also, a multiscale numerical model of the diffusion process is proposed in order to simulate the nitrogen concentration profiles after duplex treatment. The simulated and experimental profiles correspond rather well

Le grenaillage est souvent utilisé sur les pieds d’aube de turbine haute pression afin de retarder l’apparition des fissures dans les zones de concentration de contraintes. Ce traitement de surface génère des contraintes résiduelles et de l’écrouissage en surface de la pièce, ce qui influe sur sa durée de vie. L’enjeu de cette thèse est de mettre en place une méthodologie permettant de prendre en compte cet état mécanique initial, ainsi que son évolution en service, dans l’analyse de durée de vie d’une aube élaborée en superalliage monocristallin à base de nickel (AM1). Tout d’abord, cet état mécanique (contraintes résiduelles et écrouissage) est déterminé expérimentalement. Les contraintes résiduelles sont notamment évaluées par diffraction des rayons X en utilisant la méthode d’Ortner. Cet état mécanique est ensuite introduit dans les calculs de structure. Pour cela, on s’inspire de la méthode connue de l’introduction directe du champ d’eigenstrains qui est, ensuite, étendue afin d’introduire également les variables d’écrouissage ainsi que l’état mécanique anisotrope complet dans toute la structure. L’étape suivante a visé à suivre expérimentalement et à modéliser l’évolution de ces quantités sous sollicitations thermique, d’une part et cycliques à température constante (650°C), d’autre part. Enfin, la chaîne complète de calcul de durée de vie de l’AM1 est appliquée afin d’analyser la durée de vie des éprouvettes grenaillées. Les résultats obtenus sont discutés en regard des essais de fatigue effectués sur éprouvettes représentatives / Shot-peening is widely used on roots of high pressure turbine blade to postpone crack initiation in stress concentration area. This pre-stressing introduces compressive residual stress and strain hardening in a surface layer which will influence lifetime. The aim of this thesis is to propose a methodology which allows taking into account the impact of such pre-stressing and their evolution on the fatigue behaviour of a single crystal nickel-based superalloy (AM1) used for high pressure turbine blades. Firstly, the experimental work is devoted to the determination of the initial mechanical state (residual stresses and strain hardening). Residual stresses are namely determined using X-ray diffraction involving the use of a specific method developed by Ortner. This experimental initial mechanical state is then introduced as an input in structure calculation. The well-known method involving the direct introduction of eigenstrain profiles is used and improved to also introduce strain hardening variables and the complete anisotropic mechanical state in all the integration points of the structure. The next step consist in following experimentally and modeling the evolution of these quantities under thermal and mechanical loads under an uniform temperature (650°C). Finally, the complete lifetime assessment is carried out on representative shot-peened samples. Results are discussed with respect to experimental fatigue tests

<p align="justify">The conservation of structures of the historical heritage is an increasing concern nowadays for public authorities. The technical design phase of repair operations for these structures is of prime importance. Such operations usually require an estimation of the residual strength and of the potential structural failure modes of structures to optimize the choice of the repairing techniques.</p> <p><p align="justify">Although rules of thumb and codes are widely used, numerical simulations now start to emerge as valuable tools. Such alternative methods may be useful in this respect only if they are able to account realistically for the possibly complex failure modes of masonry in structural applications.</p><p><p align="justify">The mechanical behaviour of masonry is characterized by the properties of its constituents (bricks and mortar joints) and their stacking mode. Structural failure mechanisms are strongly connected to the mesostructure of the material, with strong localization and damage-induced anisotropy.</p><p><p align="justify">The currently available numerical tools for this material are mostly based on approaches incorporating only one scale of representation. Mesoscopic models are used in order to study structural details with an explicit representation of the constituents and of their behaviour. The range of applicability of these descriptions is however restricted by computational costs. At the other end of the spectrum, macroscopic descriptions used in structural computations rely on phenomenological constitutive laws representing the collective behaviour of the constituents. As a result, these macroscopic models are difficult to identify and sometimes lead to wrong failure mode predictions.</p><p><p align="justify">The purpose of this study is to bridge the gap between mesoscopic and macroscopic representations and to propose a computational methodology for the analysis of plane masonry walls. To overcome the drawbacks of existing approaches, a multi-scale framework is used which allows to include mesoscopic behaviour features in macroscopic descriptions, without the need for an a priori postulated macroscopic constitutive law. First, a mesoscopic constitutive description is defined for the quasi-brittle constituents of the masonry material, the failure of which mainly occurs through stiffness degradation. The mesoscopic description is therefore based on a scalar damage model. Plane stress and generalized plane state assumptions are used at the mesoscopic scale, leading to two-dimensional macroscopic continuum descriptions. Based on periodic homogenization techniques and unit cell computations, it is shown that the identified mesoscopic constitutive setting allows to reproduce the characteristic shape of (anisotropic) failure envelopes observed experimentally. The failure modes corresponding to various macroscopic loading directions are also shown to be correctly captured. The in-plane failure mechanisms are correctly represented by a plane stress description, while the generalized plane state assumption, introducing simplified three-dimensional effects, is shown to be needed to represent out-of-plane failure under biaxial compressive loading. Macroscopic damage-induced anisotropy resulting from the constituents' stacking mode in the material, which is complex to represent properly using macroscopic phenomenological constitutive equations, is here obtained in a natural fashion. The identified mesoscopic description is introduced in a scale transition procedure to infer the macroscopic response of the material. The first-order computational homogenization technique is used for this purpose to extract this response from unit cells. Damage localization eventually appears as a natural outcome of the quasi-brittle nature of the constituents. The onset of macroscopic localization is treated as a material bifurcation phenomenon and is detected from an eigenvalue analysis of the homogenized acoustic tensor obtained from the scale transition procedure together with a limit point criterion. The macroscopic localization orientations obtained with this type of detection are shown to be strongly related to the underlying mesostructural failure modes in the unit cells.</p> <p><p align="justify">A well-posed macroscopic description is preserved by embedding localization bands at the macroscopic localization onset, with a width directly deduced from the initial periodicity of the mesostructure of the material. This allows to take into account the finite size of the fracturing zone in the macroscopic description. As a result of mesoscopic damage localization in narrow zones of the order of a mortar joint, the material response computationally deduced from unit cells may exhibit a snap-back behaviour. This precludes the use of such a response in the standard strain-driven multi-scale scheme.</p> <p><p align="justify">Adaptations of the multi-scale framework required to treat the mesostructural response snap-back are proposed. This multi-scale framework is finally applied for a typical confined shear wall problem, which allows to verify its ability to represent complex structural failure modes.</p><p> / Doctorat en sciences appliquées / info:eu-repo/semantics/nonPublished