Open-die forging is one of the oldest forming processes in history, which has been continuously developed through technical innovations. The rapid development in the fields of measurement and control technology and the computing capacity of IT systems in recent decades offer the opportunity to take open-die forging to a higher level. In order to establish a fully autonomous forging process, a forging cell is being set up at the Institute of Metal Forming at TU Bergakademie Freiberg. It consists of two forging presses, a furnace and a KR 360 L280-2 robot arm from KUKA as a manipulator with a load capacity of up to 280 kg. A 3D scanning system allows to capture the workpiece geometry between individual pass sequences or even single press strokes. Additionally, the scanning system is equipped with three thermal imaging cameras, which record the surface temperature during a scan. A central computer controls all individual components of the forging cell.

Orientadores: Sergio Tonini Button, Mauro Moraes de Souza / Dissertação (mestrado) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecanica / Made available in DSpace on 2018-08-11T13:19:22Z (GMT). No. of bitstreams: 1 SouzaFilho_Valterde_M.pdf: 4133313 bytes, checksum: a0db5181ce553fa4a0c17b20db4a876b (MD5) Previous issue date: 2008 / Resumo: A conformação a quente, especificamente em prensa horizontal, é um tema de pouco estudo no meio acadêmico, mas interessante pelo emprego da alta taxa de deformação que alcança 90s-1. A microestrutura resultante desse processo é influenciada por algumas variáveis como temperatura, taxa de deformação, tamanho de grão austenítico inicial e taxa de resfriamento. A proposta deste trabalho é prever o comportamento da microestrutura dos aços perante essa alta taxa de deformação com a utilização da simulação numérica. Para tanto, os materiais DIN 20NiCrMo8 MOD e DIN 16MnCr5 MOD foram ensaiados nessa taxa de deformação em um processo de conformação industrial. A comparação do tamanho de grão austenítico obtido da conformação industrial com o tamanho de grão austenítico obtido através da simulação numérica é demonstrada. A influência da taxa de resfriamento sobre a microestrutura para cada material também foi demonstrada. Concluiu-se que a previsão do tamanho de grão austenítico é adequada utilizando-se o software comercial MSC.Superform acrescido do cálculo para crescimento de grãos. A previsão do comportamento mecânico após o processo de conformação utilizando-se de equações da literatura foi insatisfatória, porém pode-se demonstrar a influência da variação da taxa de resfriamento na microestrutura das peças conformada a quente / Abstract: A conformação a quente, especificamente em prensa horizontal, é um tema de pouco estudo no meio acadêmico, mas interessante pelo emprego da alta taxa de deformação que alcança 90s-1. A microestrutura resultante desse processo é influenciada por algumas variáveis como temperatura, taxa de deformação, tamanho de grão austenítico inicial e taxa de resfriamento. A proposta deste trabalho é prever o comportamento da microestrutura dos aços perante essa alta taxa de deformação com a utilização da simulação numérica. Para tanto, os materiais DIN 20NiCrMo8 MOD e DIN 16MnCr5 MOD foram ensaiados nessa taxa de deformação em um processo de conformação industrial. A comparação do tamanho de grão austenítico obtido da conformação industrial com o tamanho de grão austenítico obtido através da simulação numérica é demonstrada. A influência da taxa de resfriamento sobre a microestrutura para cada material também foi demonstrada. Concluiu-se que a previsão do tamanho de grão austenítico é adequada utilizando-se o software comercial MSC.Superform acrescido do cálculo para crescimento de grãos. A previsão do comportamento mecânico após o processo de conformação utilizando-se de equações da literatura foi insatisfatória, porém pode-se demonstrar a influência da variação da taxa de resfriamento na microestrutura das peças conformada a quente / Mestrado / Materiais e Processos de Fabricação / Mestre em Engenharia Mecânica

The aim of this diploma thesis is to describe the causes and mechanisms of degradation processes that affect the surface of tools made of tool steel and to design and verify a practical solution that would lead to higher resistance of tools to these processes. Chapters in the theoretical part deal with fracture behavior of the material and the possibilities of its elimination, the experimental part includes testing of the effect of coating on the durability of hot forming tools.

The project elaborated in frame of the engineering studies branch N2326 presenting the design of manufacturing technology of forging carrier of steel 14 220. Pursuant to the literary pursuit a problem of solid hot forming was proposed to product by drop forging with flash on 3 forging operations. All the operations are realized on the vertical crank forging press LZK 4000 B produced by ŠMERAL BRNO a.s. with nominal forming force 40 NM. Heating material on the forging temperature 1100 °C will proceed in the electric induction furnace produced by ROBOTERM s.r.o. type KSO 800kW, the flash trimming on the trimming press LDO 315 A/S with nominal forming force 3,15 MN. Dies are made from tool steel 19 552.9 and strapped in die holder QLZK 4000/UC. A part of the project is technical economic analysis evaluation and elaboration of production scheme. Expected annual volume is 100 000 pieces.

No description available.

La recherche permanente de solutions d’allègement des structures aéronautiques a conduit au développement de nouveaux alliages comme les Al-Cu-Li et les Al-Mg-Li qui se caractérisent par une densité inférieure aux alliages conventionnels et par des propriétés améliorées. De manière générale, la formabilité de ces alliages, que ce soit à froid ou à chaud est encore assez mal connue. Le projet « Formage avancé des alliages basses densité pour application aéronautique » se propose donc de caractériser précisément la plage de formabilité de ces nouveaux alliages et d’investiguer les voies de mise en œuvre les plus adaptées : procédé d’étirage conventionnel ou procédé de mise en forme pendant une étape de traitement thermique. Ce projet regroupe les entreprises AEROLIA SAS, ACB, AIRBUS Operation SAS et CONSTELLIUM.Ces développements seront destinés au fuselage métallique et plus particulièrement à la structure pointe-avant qui présente une géométrie en double courbure ; ils concernent à la fois les panneaux de fuselage et les profilés. / The ongoing researches to lighten aeronautical structures have led to the development of new materials like Al-Cu-Li and Al-Mg-Li alloys. These alloys exhibit lower density and higher mechanical properties than conventional alloys. However, their ability to be formed either by cold or hot forming process is not well known. The aims of this PhD research works are thus to characterize the formability of these new alloys and to suggest the most appropriate forming sequence to elaborate complex aeronautic parts. Various forming processes will be studied such as cold forming by stretching of sheet metal parts or hot forming by stamping of sheet metal parts after or during different heat treatments. An experimental as well as a numerical approach will be used to develop the forming process of these new alloys to elaborate fuselage panels with more or less complex shapes. These PhD research works are a component of a larger project led by IRT Jules Verne and entitled “Advanced forming of low density alloys for aeronautic applications”. This project includes several firms from aeronautic domain (AEROLIA SAS, ACB, AIRBUS SAS and CONSTELLIUM).

Cette thèse s’est déroulée dans le cadre d’une cotutelle internationale entre l’IMT - École des Mines d’Albi-Carmaux et l’Ecole Polytechnique de l’Université de Sao Paulo (EPUSP). Elle a pour but de contribuer à l’étude du comportement mécanique des alliages de titane Ti6Al4V, et plus spécialement dans le domaine du formage superplastique et du formage à chaud. L’objectif général de ce doctorat est de contribuer au développement de procédés de formages non conventionnels des alliages de titane pour applications aéronautiques. C’est pourquoi, en fonction des équipements disponibles sur les deux sites, les travaux de recherche se sont déroulés soit à l’Ecole des Mines soit à l’EPUSP. Cette thèse adresse la problématique scientifique des interactions entre le comportement mécanique dans le domaine du formage superplastique et de formage à chaud d’une part et la microstructure initiale et son évolution dans le domaine de sollicitation d’autre part. Pour cela une stratégie d’essais et de caractérisation a été développée et suivie. Les essais incluent des essais mécaniques uniaxiaux à haute température sur différents alliages Ti6Al4V présentant des microstructures initiales différentes (taille de grain 0,5; 3,0 et 4,9 μm). Une attention particulière a été portée à l’évolution microstructurale avant essai - c’est- à-dire durant sa montée en température et la stabilisation thermique de l’échantillon – et durant l’essai. Les conditions d’essai ont été choisies de façon à couvrir le domaine du formage à chaud et du formage superplastique, température de 700°C à 950°C et vitesse de déformation entre 10-1 s-1 et 10-4 s-1. La croissance de grain dépend de la microstructure initiale mais aussi de la durée de l’essai en température (croissance statique) et de la vitesse de déformation (croissance dynamique). Afin d’améliorer la validité du modèle des observations microstructurales de taille de grain sont effectués après les essais mécaniques par micrographie optique et Microscope Electronique à Balayage. Un modèle de comportement unifié a été introduit de façon à être capable de couvrir toute la plage de température et de vitesse de déformation : écrouissage cinématique non linéaire, sensibilité à la vitesse de déformation et loi de croissance de la taille des grains sont inclus dans le modèle. Afin de pouvoir valider le modèle, il a été introduit dans le code de simulation ABAQUS®. Les résultats des simulations (en particulier déformation macroscopique et taille de grain locale) ont été comparés, pour l’un des matériaux de l’étude, aux résultats d’un essai de gonflage axisymétrique de tôle. Pour obtenir un cycle de contrôle simple, les essais effectués au laboratoire de l’IPT/LEL à Sao José dos Campos au Brésil ont été opérés à vitesse de déformation constante. Les résultats montrent une très bonne corrélation avec les prédictions et permettent de conclure à une validation du modèle de comportement développé dans la thèse dans des conditions industrielles de formage de l’alliage de titane. / This thesis was developed in the frame of a Brazil-France cooperation agreement between the École des Mines d'Albi-Carmaux and the Polytechnic School of Engineering of the University of Sao Paulo (EPUSP). It aims to contribute to the study of the mechanical behaviour of Ti6Al4V alloys especially in terms of superplastic forming. The general objective of this research is to develop non-conventional forming processes for new titanium alloys applied to aerospace components. Therefore, in accordance of the equipment’s available in the two groups, the work will be conducted either at the Ecole des Mines d'Albi-Carmaux and either at EPUSP. This thesis aims to answer questions such as what are the implications in relation to the microstructural and mechanical behaviour of these alloys during superplastic and hot forming in order to establish a behaviour law for these alloys based on titanium. This requires a good knowledge of the properties of materials used in the superplastic and hot forming domain to control the parameters governing the phenomenon of superplasticity or high temperature plasticity. For this, a testing strategy and characterization methodology of those new titanium alloys was developed. The tests include high temperature uniaxial tensile tests on several Ti6Al4V alloys showing different initial grain sizes. Special focus was made on the microstructural evolution prior to testing (i.e. during specimen temperature increase and stabilization) and during testing. Testing range was chosen to cover the hot forming and superplastic deformation domain. Grain growth is depending on alloy initial microstructures but also on the duration of the test at testing temperature (static growth) and testing strain rate (dynamic growth). After testing microstructural evolutions of the alloys will be observed by optical micrograph or SEM and results are used to increase behaviour model accuracy. Advanced unified behaviour models where introduced in order to cover the whole strain rate and temperature range: kinematic hardening, strain rate sensitive and grain growth features are included in the model. In order to get validation of the behaviour model, it was introduced in ABAQUS numerical simulation code and model predictions (especially macroscopic deformation and local grain growth) were compared, for one of the material investigated, to axisymmetric inflation forming tests of sheet metal parts, also known as bulge test. To obtain a simple control cycle, tests performed at IPT/LEL laboratory in San José Dos Campos in Brazil were operated with a constant strain rate. Results show a very good correlation with predictions and allows to conclude on an accuracy of the behaviour models of the titanium alloys in industrial forming conditions.

This thesis summarizes the work done on tribological characterization of multifunctional hardfacing coatings with self-lubricating properties, intended for use in mechanical components operating in high temperature applications for which conventional lubricants are no longer effective. Deposition techniques like laser cladding have a great potential in reworking/repair of high value industrial components in order to extend their lifetime. It is expected that the use of self-lubricating laser claddings could be useful in high temperature applications like metal forming, leading to decreased friction and wear. In this study, the tribological behavior of self-lubricating claddings has been studied against steel and aluminum counter surfaces, using ASI52100 bearing steel in addition to AA6082 and AA2007 aluminum flat pins as the counter bodies. Nickel- and iron-based powders have been chosen for the preparation of claddings. Self-lubricating properties of Ag/MoS2 have been compared to an untreated reference cladding and grade 1.2367 tool steel. For steel counter surfaces, tribological properties in the temperature range between RT and 600⁰C have been investigated and at 300°C for aluminum counter surfaces. Tribological tests were done by a high frequency linear oscillation (SRV) test machine under reciprocating conditions. The wear scar and volume of coatings were measured by using a 3D optical profilometer. SEM/EDS analysis were additionally performed for the characterization of microstructure and wear scar. The results indicated that MoS2 reduced friction and wear of the Fe-based cladding material when tested against steel at room temperature compared to the reference alloy and grade 1.2367 tool steel, and that the addition of silver further decreased wear in addition to early stage friction. It was also observed that the tribolayer, which was formed during the sliding of Ni-based - 5 Ag - 10 MoS2 and against aluminium under lubricated conditions, was protective and provided low and steady friction.

L'Inconel 718 est un superalliage base-nickel très utilisé pour la fabrication de pièces aéronautiques soumises à de fortes contraintes et de hautes températures. La maîtrise de la microstructure finale issue de la mise en forme à chaud est un des éléments clés pour le contrôle des propriétés mécaniques et pour répondre aux exigences strictes du secteur. Dans cette étude, l'évolution de la microstructure de l'Inconel 718 est étudiée au moyen d'essais de torsion suivis d'une trempe à l'eau (pour examiner les évolutions dynamiques) ou d'un maintien à la température de déformation puis d'une trempe à l'eau (pour examiner les évolutions post-dynamiques). Ces essais sont réalisés dans les domaines de température δ-supersolvus et δ-subsolvus et pour des vitesses de déformation de 10-2 à 0.1 s-1. Des analyses microstructurales par microscopie électronique à balayage et cartographie des orientations cristallographiques par EBSD sont réalisées pour suivre l'évolution de la fraction recristallisée, de la taille de grains recristallisés ainsi que de l'état de précipitation lors de la déformation et des maintiens pré- et post-déformation. Sur base de ces observations expérimentales, les principaux mécanismes métallurgiques actifs sont identifiés, puis modélisés : écrouissage, germination de nouveaux grains, migration de joints de grains, et interaction avec les particules de seconde-phases. Un modèle d'évolution microstructurale en champ moyen a été enrichi pour prendre en compte l'ensemble de ces mécanismes élémentaires et leur dépendance aux conditions thermomécaniques. Ce modèle permet de décrire, pour les domaines δ-subsolvus et δ-supersolvus, les cinétiques de recristallisation dynamique et post-dynamique de l'Inconel 718, les cinétiques de précipitation et dissolution de la phase δ, ainsi que l'évolution de la taille de grains. Il prédit également les courbes contrainte-déformation dans le domaine de température δ-supersolvus. / Inconel 718 is nickel-based Superalloy widely used in the aeronautic industry to manufacture aircraft parts subjected to extreme in-service conditions of high stresses at elevated temperatures. Controlling the microstructure after hot forming is a key element to control the mechanical properties of the final products and meet the tight specifications imposed by the aeronautic industry.In this work, the microstructure evolution of Inconel 718 was investigated via isothermal and iso-strain rate torsion tests followed by water quenching (to investigate dynamic evolution) or by annealing at deformation temperature then water quenching (to investigate post-dynamic evolution). These tests were conducted in both δ-Supersolvus and δ-Subsolvus temperature domains and for strain rates of 0.01 to 0.1 s-1.Scanning electron microscopy (SEM) and Electron Back Scattered Diffraction (EBSD) were used to characterize the microstructure and follow the evolution of the recrystallized fraction, the recrystallized grain size and the δ-phase precipitation after deformation and during pre-deformation and post-deformation annealing. Based on these experimental observations, the main metallurgical mechanisms have been identified and modelled: hardening, nucleation of new grains, grain boundaries migration and the δ-phase- recrystallization interaction.A two-site mean field approach having a low computational cost was chosen to model the microstructural evolution at different thermomechanical conditions. This model describes the main mechanisms taking place during hot forming of Inconel 718 in both δ-Supersolvus and δ-Subsolvus domains and predicts the recrystallization kinetics in both dynamic and post-dynamic regimes , the δ-phase precipitation and dissolution kinetics and the grain size evolution. The model predicts also the strain-stress curves at high temperatures in the absence of δ-phase particles.

This project was made within the engineering studies and its aim was to design an assembly line to product assigned components of appropriate quality and quantity, using the technology of hot extrusion, both backward and forward. A series of technology steps was suggested, parameters necessary for individual operations were set and on this basis, adequate machines were chosen. The conclusion of this work contains technical-economical evaluation for the chosen options which expects the ten-year return with average production of 40 000 pieces.