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La thèse s'inscrit dans le cadre du projet GENOME « Gestion Optimisée de l'Energie » dont l'enjeu majeur est la conception d'un avion plus électrique. L'augmentation de l'efficacité énergétique et de la compacité des systèmes électriques de ces avions entraîne de fortes sollicitations en température. Ces sollicitations sont liées à la compacité des systèmes (réduction de masse et de volume) ainsi qu'à leur localisation par rapport aux sources chaudes (réacteur d'avion par exemple). De ce fait, les matériaux magnétiques des nouveaux convertisseurs électriques doivent pouvoir fonctionner sous des conditions de hautes températures, supérieures à 200°C. Il s'agit du polycristallin FeCoV dédié à la fabrication des tôles du stator et du rotor des génératrices rapides (situées à proximité des réacteurs) et le nanocristallin FeCuNuSiB dédié à la conception des inductances et transformateurs des convertisseurs statiques. Ce manuscrit s'intéresse à l'étude du vieillissement thermique de ces deux familles de matériaux magnétiques. Ces matériaux, fournis par la société APERAM, se déclinent sous plusieurs nuances et finitions. L'étude du vieillissement consiste en l'application de plusieurs essais de vieillissement continus sous différentes températures (jusqu'à 300 °C pour les FeCoV et 240 °C pour les nanocristallins). Plusieurs grandeurs macroscopiques magnétiques, électriques et mécaniques (pour les FeCoV) sont mesurées à chaque intervalle de vieillissement. Grâce à ces mesures macroscopiques et à des mesures complémentaires effectuées à l'échelle microscopique, des analyses sont faites et des hypothèses sont proposées afin d'expliquer les mécanismes de vieillissement de ces deux familles de matériaux et dans le but de proposer des modèles phénoménologiques fiables / The thesis takes part of the project GENOME “Gestion Optimisée de l’Energie” whose major issue is the design of the more electrical aircraft. The increase in the energy efficiency and the compactness of the electrical systems of these aircrafts lead to high temperature stresses. These thermal stresses are related to the compactness of the systems (reduction of mass and volume) as well as their location with respect to the hot sources (aircraft engine for example). Thus, the magnetic materials of the new electrical converters must be able to operate under conditions of high temperatures, above 200 °C. Typically, the FeCoV polycrystalline materials are dedicated to the fabrication of the stator and rotor sheets of the fast generators (located near the aircraft engine) and the FeCuNbSiB nanocrystalline materials are dedicated to the design of inductors and transformers of the static converters.This manuscript concerns the thermal ageing study of these two magnetic material families. These materials, supplied by the company APERAM, are available in several shades. The ageing study consists on applying several continuous ageing treatments at different temperatures (up to 300 °C for FeCoV and 240 °C for FeCuNbSiB). At each ageing step, several macroscopic properties namely: magnetic, electrical and mechanical (for the FeCoV materials) properties are measured. Using these macroscopic properties and complementary measurements carried out on a microscopic scale, analyses are made and hypotheses are proposed in order to explain the ageing mechanisms of these magnetic material families. The understanding of the magnetic ageing mechanisms is necessary towards establishing of phenomenological ageing models

An understanding of crack tip fields and fracture mechanisms in single crystals can help in developing better polycrystalline alloys and manufacturing processes. To this end, the effects of loading rate, material inertia and strain rate sensitivity on crack tip fields and their influence on fracture mechanisms in FCC single crystals are examined in this work by performing finite element analysis. It is shown that, in the absence of inertial effects, high loading rates elevate the stresses ahead of a crack tip and decrease the plastic strains in rate dependent single crystals. Also, it is found that the quasi-static near-tip stress field can be adequately characterized by the energy release rate J and a constraint parameter Q. Similar two-parameter characterization is possible even under dynamic loading. It is observed that if a suitable reference solution is used, the role of inertia manifests as a loss of constraint with increasing loading rate irrespective of strain rate sensitivity and lattice orientation. Thus, at very high loading rates, inertial effects oppose the role of rate sensitivity and cause a decrease in stresses near the tip. The relative influence of these two factors depends on rate sensitivity index. For a mildly rate dependent single crystal, the predicted cleavage fracture toughness remains constant up to a certain loading rate and thereafter increases sharply. On the other hand, for a strongly rate dependent single crystal, fracture toughness drops initially up to a certain loading rate beyond which it increases marginally. The loss of crack tip constraint is found to retard the ductile fracture mechanisms of void growth and coalescence. However, this is dependent on lattice orientation. In-situ experimental observation of void growth near a notch tip also shows strong orientation dependence. In addition, 3D finite element results indicate though-thickness dependence of equivalent plastic slip and hydrostatic stress leading to variations in void growth along the thickness direction of the specimens. The predicted load-displacement curves, lattice rotation, slip traces and void growth using finite element analysis are found to be in good agreement with the experimental observations. Thus, the present study has provided an understanding of the role of several factors such as constraint level, rate sensitivity, material inertia, lattice orientation and 3D effects on the mechanics of fracture of ductile single crystals.