The framework of this thesis is the modelling and the lifetime prediction of high pressure aeronautical turbine blades. These parts are realized in nickel base single crystal superalloys. This work is focused on the microstructural evolution arising at high temperatures under mechanical loading known as the directionnal coarsening. In a first time, this work consists in studying the mechanical behaviour of the initial non-aged material. Tests have been performed at 950°C in order to enrich the available data base. They have allowed us to identify a hyperbolic sinus viscosity model over a wide range of stain rates. The initial behaviour has also been studied at the mesoscopic scale. A constitutive model has been identified for both phases in...
Ce travail s'inscrit dans le contexte de la modélisation et de la prévision de la durée de vie des a...
The present work deals with crystal plasticity of single crystal nickel-base superalloys. In this co...
Single crystal components operating at elevated temperatures are subjected to severe thermomechanica...
The framework of this thesis is the modelling and the lifetime prediction of high pressure aeronauti...
A 3D phenomenological model coupling viscoplasticity, microstructural evolutions and damage is propo...
This work is in the context of modeling and predicting the life of high pressure turbine blades of g...
Constitutive modelling is employed by engine designers to predict stresses and strains in turbine en...
The creep of high pressure turbine blades is a critical issue for the certification of a helicopter ...
Ni-based single crystal (SX) superalloys are used for turbine blade applications because of their hi...
In view of the turbine entry temperature evolution, the main challenge for metallurgists is to elabo...
Monocrystalline nickel based superalloys are the most suitable materials for the design of high perf...
The study carried out during this thesis consists in analyzing the micromechanisms that control the ...
Inconel 718 is a nickel base superalloy commonly used to manufacture the rotating disks of turbojet ...
Nickel-based single crystal superalloys are extensively used for turbines blades (above 1000°C) of a...
The field of mechanics, particularly micromechanics, has undergone great developments. It is well kn...
Ce travail s'inscrit dans le contexte de la modélisation et de la prévision de la durée de vie des a...
The present work deals with crystal plasticity of single crystal nickel-base superalloys. In this co...
Single crystal components operating at elevated temperatures are subjected to severe thermomechanica...
The framework of this thesis is the modelling and the lifetime prediction of high pressure aeronauti...
A 3D phenomenological model coupling viscoplasticity, microstructural evolutions and damage is propo...
This work is in the context of modeling and predicting the life of high pressure turbine blades of g...
Constitutive modelling is employed by engine designers to predict stresses and strains in turbine en...
The creep of high pressure turbine blades is a critical issue for the certification of a helicopter ...
Ni-based single crystal (SX) superalloys are used for turbine blade applications because of their hi...
In view of the turbine entry temperature evolution, the main challenge for metallurgists is to elabo...
Monocrystalline nickel based superalloys are the most suitable materials for the design of high perf...
The study carried out during this thesis consists in analyzing the micromechanisms that control the ...
Inconel 718 is a nickel base superalloy commonly used to manufacture the rotating disks of turbojet ...
Nickel-based single crystal superalloys are extensively used for turbines blades (above 1000°C) of a...
The field of mechanics, particularly micromechanics, has undergone great developments. It is well kn...
Ce travail s'inscrit dans le contexte de la modélisation et de la prévision de la durée de vie des a...
The present work deals with crystal plasticity of single crystal nickel-base superalloys. In this co...
Single crystal components operating at elevated temperatures are subjected to severe thermomechanica...