Les alliages d'aluminium utilisés dans les structures aéronautiques (fuselage, voilure) sont soumis à des chargements cycliques, faisant de la fatigue l'un des facteurs dimensionnant. Dans cette thèse, les mécanismes d'amorçage de ces fissures de fatigue – au niveau des particules intermétalliques – et de micropropagation sont étudiés expérimentalement et numériquement sur les alliages 2050-T8 et 7050-T7451. Les analyses des premiers chapitres portent sur la description des particules intermétalliques qui sont les plus susceptibles de donner lieu à une amorce de fissure dans la matrice d'aluminium. Les effets de la nature des particules et de leur taille sont quantifiés. La proximité entre les particules intermétalliques et les pores y est décrite. Cette analyse expérimentale fait intervenir des observations de surface en microscopie électronique à balayage (MEB), ainsi que des caractérisations tridimensionnelles (3D) réalisées à l'aide de la tomographie par rayonnement synchrotron. Dans les chapitres suivants, les analyses traitent de la prévision des chemins de fissuration à l'échelle d'un grain. Elles s'appuient sur des observations expérimentales de surface et des simulations de plasticité cristalline 3D pour comprendre les chemins de fissuration. Un modèle d'endommagement tenant compte de la cristallographie est alors proposé pour simuler la propagation de fissure par éléments finis. / Aluminium alloys used for aerospace structures (wing, fuselage) are subjected to cyclic loading. Fatigue properties of such alloys are therefore taken into account for the design of such parts. In this thesis, initiation mechanisms of fatigue cracks – near intermetallic particles – and micropropagation are studied experimentally and numerically on alloys 2050-T8 and 7050-T7451. In the first chapters, the analysis focuses on intermetallic particles which are most prone to initiate a fatigue crack in the aluminium matrix. The effects of the nature of particles as well as their size are quantified. The proximity between intermetallic particles and pores is described. This experimental analysis use surface observations obtained with a scanning electron microscope (SEM), and three-dimensional (3D) characterizations using synchrotron tomography. In the last chapters, analysis are oriented towards the prediction of crack paths at the grain size. They rely on surface experimental observations and 3D crystal plasticity modelling in order to understand crack paths. A damage model taking into account crystallography is proposed to simulate crack propagation using the finite element method.

A multi-analytical approach based on in-situ and ex-situ local probing techniques was employed to investigate localized corrosion mechanisms of some aluminum alloys in chloride containing solutions, focusing on the influence of intermetallic particles (IMPs) in the alloys. In the EN AW-3003 alloy, SEM-EDS analysis revealed constituent and dispersoid IMPs. There are two types of constituent IMPs, with size ranging from 0.5 to several μm, and composition typically Al6(Fe,Mn) or Al12(Mn,Fe)3Si, respectively,having a Mn/Fe ratio of about 1:1. Fine dispersoids of 0.5 μm or less in size normally have the composition Al12Mn3Si1-2. Scanning Kelvin probe force microscopy (SKPFM measurements showed that the constituent IMPs have a higher Volta potential compared to the matrix, and the Volta potential difference increased with particle size, probably related to the composition of the IMPs. The SKPFM results also showed a Volta potential minimum in the boundary region adjacent to some larger IMPs. The open-circuit potential and electrochemical impedance spectroscopy measurements indicated local electrochemical activities occurring on the surface, and active-like dissolution in the acidic solutions, but a passive-like behavior in the near-neutral solutions. Infrared reflection-absorption spectroscopy measurements after exposure and thermodynamic calculations suggested the formation of mixtures of aluminum oxyhydroxide and acetate on the surface in acetic acid solutions. The formation and fraction of dominant species of the corrosion products depend on the pH of the solution, and aluminum chloride compounds may form at very low pH. Moreover, an integrated in-situ atomic force microscopy (AFM) and scanningelectrochemical microscopy (SECM) set-up was used to investigate the localized activities on the surface. With a dual mode probe, acting as both AFM tip and SECM microelectrode, concurrent topography and electrochemical current images were obtained on the same area of the surface. Numerical simulations of the SECM suggested a micrometer lateral resolution under favorable conditions and the ability to resolve μmsized active sites with a separation distance of about 3 μm or larger. The simulations were verified by SECM mapping of the aluminum alloys in the chloride solutions. The AFM/SECM measurements revealed enhanced cathodic activity on some larger IMPs and local anodic dissolution around larger IMPs. In-situ AFM monitoring confirmed preferential dissolution in the boundary region adjacent to some of these IMPs. The results elucidate the micro-galvanic effect and size effect of the IMPs during the initiation of localized corrosion of the Al alloys. Furthermore, differences in corrosion properties between EN AW-3003 and a newly developed Al–Mn–Si–Zr alloy were studied with a similar approach. Compared to EN AW-3003, the new alloy had a smaller number of particles with a large Volta potential difference relative to the matrix. In slightly corrosive solutions extensive localized dissolution and deposition of corrosion products occurred on EN AW-3003, whereas only a small number of corroding sites and “tunnel-like” pits occurred on the Al–Mn–Si–Zr alloy. The lower corrosion activity and the smaller tunnel-like pits resulted in lower material loss of the Al–Mn–Si–Zr alloy, which is beneficial for applications using a thin material. / QC 20100702