Abstract The aim of the project is to determine the mechanical properties and the microstructure with a to b transformation of the titanium alloy Ti-6Al-4V. The experiments made were tensile tests at temperatures 20, 400 and 800C and SEM images before and after inductive methods. Ti-6Al-4V is one of the most used types of alloy mainly because it has good qualities in strength, corrosion resistance and low weight with respect to the strength of the material. The strength is dependent on the microstructure and the ratio between the different phases a and b. This is the reason it is interesting to measure the transformation between the phases and then use the data to simulate and determine the required conditions for the manufacturing process....
The PhD thesis deals with the influence of temperature and strain rate on the mechanical behaviour o...
The lightening of structure is one of the most important issue in the aircraft industry. The weight ...
The improvement of specific performances of metallic materials used for aerospaceapplications needs ...
L'objectif de ce travail de thèse est de mieux comprendre l'influence de la température, de la vites...
The aim of this thesis is to better understand the influence of temperature, strain rate and initial...
L’amélioration des performances mécaniques des matériaux utilisés dans l’aéronautique repose général...
Le présent travail concerne l’étude de l’usinage de l’alliage de titane Ti-6Al-4V, matériau très app...
Les procédés de fabrication additive ont actuellement atteint une maturité suffisante pour produired...
This research is part of the TiMaS project (Titanium Machining and Simulation). The main goal of thi...
Das Verformungsverhalten und die Verformungskinetik von technisch reinem Titan (Ti-2) und der Titanl...
Titanium alloys have been interesting combinations of mechanical properties and corrosion, thus gene...
A realização do presente trabalho permitiu o estudo dos micromecanismos de deformação e fratura da l...
The use and knowledge of additive manufacturing technologies are rapidly growing. It is crucial to u...
This thesis was developed in the frame of a Brazil-France cooperation agreement between the École de...
Issu de : EuroSPF - 11th European Conference on Superplastic Forming, Toulouse, FRANCE, 7-9 Septembe...
The PhD thesis deals with the influence of temperature and strain rate on the mechanical behaviour o...
The lightening of structure is one of the most important issue in the aircraft industry. The weight ...
The improvement of specific performances of metallic materials used for aerospaceapplications needs ...
L'objectif de ce travail de thèse est de mieux comprendre l'influence de la température, de la vites...
The aim of this thesis is to better understand the influence of temperature, strain rate and initial...
L’amélioration des performances mécaniques des matériaux utilisés dans l’aéronautique repose général...
Le présent travail concerne l’étude de l’usinage de l’alliage de titane Ti-6Al-4V, matériau très app...
Les procédés de fabrication additive ont actuellement atteint une maturité suffisante pour produired...
This research is part of the TiMaS project (Titanium Machining and Simulation). The main goal of thi...
Das Verformungsverhalten und die Verformungskinetik von technisch reinem Titan (Ti-2) und der Titanl...
Titanium alloys have been interesting combinations of mechanical properties and corrosion, thus gene...
A realização do presente trabalho permitiu o estudo dos micromecanismos de deformação e fratura da l...
The use and knowledge of additive manufacturing technologies are rapidly growing. It is crucial to u...
This thesis was developed in the frame of a Brazil-France cooperation agreement between the École de...
Issu de : EuroSPF - 11th European Conference on Superplastic Forming, Toulouse, FRANCE, 7-9 Septembe...
The PhD thesis deals with the influence of temperature and strain rate on the mechanical behaviour o...
The lightening of structure is one of the most important issue in the aircraft industry. The weight ...
The improvement of specific performances of metallic materials used for aerospaceapplications needs ...