Letteratura scientifica selezionata sul tema "Alliages réfractaires – Fissuration"
Cita una fonte nei formati APA, MLA, Chicago, Harvard e in molti altri stili
Indice
Consulta la lista di attuali articoli, libri, tesi, atti di convegni e altre fonti scientifiche attinenti al tema "Alliages réfractaires – Fissuration".
Accanto a ogni fonte nell'elenco di riferimenti c'è un pulsante "Aggiungi alla bibliografia". Premilo e genereremo automaticamente la citazione bibliografica dell'opera scelta nello stile citazionale di cui hai bisogno: APA, MLA, Harvard, Chicago, Vancouver ecc.
Puoi anche scaricare il testo completo della pubblicazione scientifica nel formato .pdf e leggere online l'abstract (il sommario) dell'opera se è presente nei metadati.
Tesi sul tema "Alliages réfractaires – Fissuration"
Chassaigne, Jean-Christophe. "Fissuration à hautes températures du superalliage base nickel N18 élaboré par métallurgie des poudres : Etude du couplage mécanique-environnement en pointe de fissure". Paris, ENMP, 1997. http://www.theses.fr/1997ENMPA001.
Testo completoBennouna, Abdouh. "Etude de l'oxydation du superalliage réfractaire inconel 718 (NC19F eNb) : rôle des précipités de carbure de niobium et de phase delta (Ni 3Nb)". Toulouse, INPT, 1986. http://www.theses.fr/1986INPT005G.
Testo completoRézaï-Aria, Farhad. "Fatigue thermique et fatigue isotherme d'un superalliage à base de cobalt : étude métallurgique de l'endommagement et modélisation". Paris 11, 1986. http://www.theses.fr/1986PA112377.
Testo completoMolins, Régine. "Oxydation de superalliages à base de nickel : identification des mécanismes et conséquences sur le mode de propagation des fissures en fatigue à haute température". Paris, ENMP, 1995. http://www.theses.fr/1995ENMP0526.
Testo completoPonnelle, Sylvain. "Propagation des fissures par fatigue a haute temperature dans l'Inconel 718 : effets de microstructure et de chargements complexes". Paris, ENMP, 2001. http://www.theses.fr/2001ENMP1003.
Testo completoDoghri, Anis. "Vers une maîtrise de la réparation par le procédé CLAD de pièces aéronautiques en Inconel 738 LC : compréhension des mécanismes de fissuration et modélisations associées". Electronic Thesis or Diss., Université de Lorraine, 2019. http://www.theses.fr/2019LORR0112.
Testo completoY' hardened nickel-based superalloys, such as Inconel 738 LC (IN738LC), are materials which are extensively used in hot sections parts of helicopter and aircraft engines. Those materials exhibit enhanced mechanical properties at high temperature. Nevertheless, cracking and several defects can occur on these parts during casting or during their service life. However, welding type repairing processes can lead to considerable cracking of IN738LC superalloy. It appears that laser cladding is a promising additive manufacturing technology which allows the repair of damaged parts. The present work main objective is aimed at investigating Inconel 738 LC repair by laser cladding. Both experimental and numerical aspects are studied for the repair of IN738LC by means of the CLAD process. Experimental laser clad deposits are produced under several configurations following industrial cases. Two distinct cracking mechanisms are identified in the heat-affected zone and within the deposit, respectively. A multi-physics simulation of laser cladding is developed in order to take into account thermal, mechanical and metallurgical phenomena. Simulation is compared to experimental measurements for validation. Finally, these numerical tools are used to define cracking risk criteria. In summary, a high preheating of the samples allows to suppress liquation and HAZ cracking, but also to obtain un-cracked deposit, which indicates that the repair of non-weldable alloys is possible
Branza, Traian. "Rechargement par soudage d'aciers réfractaires moulés : application à la réparation des matrices de formage superplastique". Toulouse 3, 2005. http://www.theses.fr/2005TOU30246.
Testo completoSuperplastic forming (SPF) of TA6V aeronautical sheets is performed at temperatures close to 900°C. Forming tools, manufactured with heat resistant cast steels, are exposed to highly severe thermomechanical stress likely to cause their damage. The purpose of this study is to develop weld repair techniques for SPF dies and to characterize the weld joints using microstructural investigations and mechanical testing. The parameters of welding and filling are optimized in order to guarantee the best quality of the welded zone. The influence that parameters related to the weld repair process and the materials used, have on the propensity of the cast steels to crack during welding, is investigated. These analyses are performed on the macrographs of the welded zone and also using image analysis technique. For the very deep groove, two weld repair techniques are developed, the surface remelting of the material and the buttering. The mechanical performances of the repaired structures are evaluated using low cycle fatigue tests. The mechanical behaviour of the weld repair joints is also investigated using numerical simulation
Govaere, Adèle. "Impact des carbures sur la variabilité des propriétés en fatigue de superalliages pour disques". Thesis, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique, 2020. http://www.theses.fr/2020ESMA0020.
Testo completoNowadays, original engine makers are challenged by the environmental requirements imposing drastic decrease of CO2 and NOx emissions. It leads to the development of γ/γ′ nickel-based superalloys to ensure good tensile and fatigue properties and a good oxidation behavior of turbine discs. AD730TM was elaborated for applications up to 700°C and the crack initiation and propagation mechanisms this alloy need to be investigated. Non-metallic inclusions are brittle elements that are sensitive to oxidation. They can act as stress concentration sites and can lead to crack initiation. Low cycle fatigue tests were performed at 450°C and 700°C to determine the tests conditions promoting a crack initiation from such inclusions. Fractographic analyzes revealed that inclusions lead to the specimen fracture when the environmental effects are limited and at high strain or stress ranges.In order to better understand the parameters promoting inclusions cracking, oxidation and in situ tensile tests in a SEM chamber were performed. They highlighted an important volume expansion and the cracking of niobium oxides. A stress threshold necessary to crack inclusions was also determined. To improve the fatigue tests understanding, crack propagation tests were carried out to estimate the crack initiation time according to the temperature and the stress range applied. This crack initiation time is shorter when the cracks initiate within inclusions
Doghri, Anis. "Vers une maîtrise de la réparation par le procédé CLAD de pièces aéronautiques en Inconel 738 LC : compréhension des mécanismes de fissuration et modélisations associées". Thesis, Université de Lorraine, 2019. http://www.theses.fr/2019LORR0112/document.
Testo completoY' hardened nickel-based superalloys, such as Inconel 738 LC (IN738LC), are materials which are extensively used in hot sections parts of helicopter and aircraft engines. Those materials exhibit enhanced mechanical properties at high temperature. Nevertheless, cracking and several defects can occur on these parts during casting or during their service life. However, welding type repairing processes can lead to considerable cracking of IN738LC superalloy. It appears that laser cladding is a promising additive manufacturing technology which allows the repair of damaged parts. The present work main objective is aimed at investigating Inconel 738 LC repair by laser cladding. Both experimental and numerical aspects are studied for the repair of IN738LC by means of the CLAD process. Experimental laser clad deposits are produced under several configurations following industrial cases. Two distinct cracking mechanisms are identified in the heat-affected zone and within the deposit, respectively. A multi-physics simulation of laser cladding is developed in order to take into account thermal, mechanical and metallurgical phenomena. Simulation is compared to experimental measurements for validation. Finally, these numerical tools are used to define cracking risk criteria. In summary, a high preheating of the samples allows to suppress liquation and HAZ cracking, but also to obtain un-cracked deposit, which indicates that the repair of non-weldable alloys is possible
Mataveli, Suave Lorena. "High Temperature Durability of DS200+Hf Alloy". Thesis, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique, 2017. http://www.theses.fr/2017ESMA0032/document.
Testo completoThe anisotropy in mechanical behavior of the directionally solidified DS200+Hf alloy and the damage mechanisms have been investigated between 650°C and1100°C. Single-crystalline specimens of the same alloy have also been used to get a better understanding of the anisotropy in mechanical properties and durability. Tension, creep, low-cycle fatigue (LCF), dwell-fatigue and crack propagation tests have been performed and analyzed by SEM observations to better understand the damage modes in this alloy. At 650°C, a considerable creep (and LCF) life anisotropy is observed while almost no anisotropy remains at 1100°C in creep. The γ rafting is mainly responsible for this decrease in creep anisotropy and for theincrease in creep rate in dwell-fatigue. An intergranular fracture mode has been observed for ail kind of solicitation along transverse direction, mainly due to the presence of grain boundary particles such as carbides. These carbides are also the main crack initiation sites in LCF at 650°C and at 900°C. At high temperature (900°C), oxidation not only controls the crack initiation mechanisms by inducing surface carbides cracking, but it also affects the crack propagation through a combined localized γ depletion and crack tip blunting, leading ove ra li to a higher crack propagation threshold. Such a behavior is not observed in high vacuum and surface carbides are no more the main crack initiation sites. lt is shown that at low temperature during transverse creep testing (750°C), highly misoriented grain boundaries, having one grain favorably oriented for single slip and lattice rotation, are the most critical ones