京都大学 / 0048 / 新制・課程博士 / 博士(医学) / 甲第22370号 / 医博第4611号 / 新制||医||1043(附属図書館) / 京都大学大学院医学研究科医学専攻 / (主査)教授 別所 和久, 教授 戸口田 淳也, 教授 妻木 範行 / 学位規則第4条第1項該当 / Doctor of Medical Science / Kyoto University / DFAM

Chronic or degenerative diseases affecting the lumbar spine, commonly referred to as low back pain (LPB), are a major cause of dysfunction, pain, and disability worldwide. According to the Global Burden of Disease (GBD) report of 2019, LPB affects over half a billion people, severely limiting their well-being and lifestyle. Unfortunately, these numbers have been steadily increasing over the last decade, with a rise of more than 15%, mainly due to demographic aging of the population, making it a significant socioeconomic global issue. When conservative treatments such as medications, drugs, and injections fail to alleviate the symptoms, surgical interventions become necessary. Spinal surgeries have become increasingly common and account for 40% of the top ten surgical procedures in the United States alone. As a result, the global market for spinal implants and medical orthopedic devices has been growing at a compound annual growth rate (CAGR) of 5.0% in the United States. Degenerative disc diseases, herniated intervertebral discs, and spondylolisthesis are among the most common problems requiring implant surgery, with lumbar interbody fusion cages or total disc replacements being the most common options. These surgical techniques often utilize a metal endplate or hollow cage as a load-bearing structure to ensure correct load transmission and biomechanical spinal functionality. Currently, endplates for total disc replacement are produced using subtractive manufacturing techniques from bulk biomedical-graded metal alloys like Ti-6Al-4V. The endplates are inserted between two adjacent vertebral bodies, where bone ingrowth and implant fusion are necessary. However, the elastic properties of bulk metals and bone tissue do not match, resulting in stress-shielding phenomena, implant loosening, or implant subsidence. These complications frequently necessitate surgical revision of the implant, which not only impacts the daily activities of the patients but also has a relevant economic impact. Therefore, researchers are exploring alternative design and manufacturing strategies to develop next-generation prosthetic devices that overcome these challenges. Metal additive manufacturing (MAM), particularly Laser-Powder Bed Fusion (L-PBF), has revolutionized the fabrication of specialized components with complex shapes, including architected cellular materials - a novel class of engineered materials with tunable mechanical properties. The biomedical field is a prime example of where lattice application has proved beneficial. MAM provides numerous advantages, including patient-specific customization, a vast design space, and reduced stress shielding. However, issues with structural integrity, lack of AM-specific norms, and the need for fine-tuning process optimizations are still hindering MAM's widespread adoption on the international market. An essential issue that requires resolution is the impact of process-induced flaws on the fatigue behavior of components made of L-PBF lattices. Despite a growing body of scientific literature on the fatigue behavior of lattice unit cells, little attention has been given to the function of fatigue at a millimetric scale, specifically the role of sub-unital lattice elements such as struts and junctions. As fatigue is highly localized, understanding primary fatigue behavior and fracture mechanisms at a strut scale may be critical to addressing the aforementioned problems. Moreover, designing proper prosthetic devices requires fulfilling both biomechanical and biological requirements, leading to a bottleneck in component quality. Proper tuning of osteointegration often requires large porosity and small strut dimensions, approaching the limits of industrial 3D printers. This increases the likelihood of manufacturing lattices with unconnected struts, drosses, parasitic masses, and severe deviations from the nominal as-designed geometries, leading to highly susceptible components under fatigue. To address these challenges, combined approaches with bone tissue engineering may be advantageous. Biopolymers from natural sources, such as silk fibroin and collagen derivatives (i.e., gelatin), are widely used for bone-filler applications due to their exceptional biological properties. These polymers can create highly interconnected biodegradable porous 3D scaffolds suitable for cell differentiation towards an osteogenic phenotype, such as in the form of foams. These foams can be embedded into metal lattice structures, resulting in a hybrid composite device that simultaneously fulfills the load-bearing, fatigue, and osteointegrative requirements that a spinal prosthetic device necessitates. This thesis work covers a range of topics mentioned above. Firstly, an introductory theoretical background is presented in Chapter I, followed by experimental findings which are presented in three different chapters. Chapter II is dedicated to the fatigue behavior of L-PBF Ti-6Al-4V sub-unital lattice elements in the form of miniaturized dog-bone specimens that mimic struts and nodes. This chapter is divided into four sections. The first section investigates the fatigue strength of strut-like specimens based on their building orientations at four different angles with respect to the printing job plate. Morphological features of the miniaturized specimens such as average and minimum cross-section, eccentricity, waviness, and surface texture are correlated with fatigue strength. The role of inner and surface defects, such as lack-of-fusion (LoF) and gas holes, is also considered to explain the main failure mechanisms. The impact of building orientation on the printing quality of the specimens is highlighted, with an increase in surface roughness and defectiveness as the printing angle decreases, resulting in a shorter fatigue life for miniaturized struts. In the second section, the fatigue effect is studied across different fatigue regimes. The role of the mean stress effect is assessed using the Haigh diagram, which reveals an increase in fatigue life moving towards compressive loading regimes. The effect of the printing angle is also investigated, showing different trends according to the different stress ratios, suggesting different fatigue failing mechanisms. The third section introduces strut-junction miniaturized specimens and evaluates their fatigue behavior according to building orientations. Horizontal specimens show an increased fatigue life compared to their thin strut counterparts, and different morphological outcomes are highlighted, including improved surface quality even at lower angles, possibly related to the node acting as an additional supporting structure. The fourth section presents a design-led compensation strategy for sub-unital lattice specimens, aimed at reducing as-designed/as-built deviations. This systematic decrease in geometrical mismatch suggests potential new design strategies for fatigue enhancement. In Chapter III, bone tissue engineering strategies are explored for the design of foam scaffolds as bio-fillers for lattice-based design. The feasibility of the polymer-metal composite is assessed, using an N2O-based gas foaming technique to fabricate silk fibroin and silk fibroin/gelatin porous scaffolds infilled into a cubic L-PBF Ti-6Al-4V lattice structure. The adhesion at the polymer/metal interface is assessed, with simultaneous electrowetting, showing promise for better and more intimate contact on the outermost surface of the lattice struts. A statistical-based analysis of the foam porosity is then carried out, aimed at optimization towards osteointegration improvement. Selected foams are biologically evaluated, revealing good cell adhesion and differentiation towards an osteogenic phenotype. Chapter IV reports on two different strategies for the design of a Ti-6AL-4V L-PBF lattice-based endplate for total disc replacement. The first strategy focuses on homogenized-based topology optimization, designing an octet-truss prosthetic device with a graded structure and a cell size suitable for polymeric infilling. The second strategy aims at optimizing octet-truss lattice components for fatigue, evaluating the optimal building orientation for the specimens. Experimental results reveal an improvement in the fatigue life of three-point bending test specimens, suggesting the potential of the proposed model. In Chapter V, the major takeaways of this thesis work are discussed, highlighting important advancements in understanding the fatigue behavior of lattice structures and the development of novel hybrid strategies for the design of biomedical devices, with a particular focus on spinal orthopedics. Future possible directions for research are also explored.

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[EN] TiAl intermetallic have demonstrated excellent behavior at high temperature, however, the processing for producing coatings is not easy due to its high melting point, otherwise the coaxial laser cladding process promise to be an excellent tool for obtaining extensive overlapping coatings, achieving complete fusion and deposition of alloys with high melting point on surfaces with complex shape. In this work we study the parameters of coaxial laser process and preheating the substrate to achieve Ti48Al2Cr2Nb intermetallic coatings on Ti6Al4V sheet 3 mm thick, in order to improve the tribological, oxidation and corrosion behavior of the Ti6Al4V alloy. The geometrical and chemical dilution analysis of the single tracks obtained at different levels in the laser processing variables were able to identify combinations that minimize defects such as cracks, high dilution and inadequate aspect ratio. It found a direct relation between the cooling rate and the coaxial laser process parameters such as the powder feeding rate and scanning velocity. Thus the process was optimized by minimizing the cooling rate with decreasing the velocity. After this was selected as appropriate preheating temperature 350 ºC and were obtained coatings with 40% overlap, using process parameters which generate laser specific energy of 70, 80, 90 and 180 J/mm2, then they have been evaluated by optical microscopy (OM), scanning electron microscopy (SEM), X-ray diffraction (XRD), Vickers micro-hardness (HV) and nanoindentation. The microstructure of the coatings consists gamma-TiAl phase and alfa2-Ti3Al. Preheating the substrate has allowed obtaining coatings with good metallurgical bond, although cracks and pores are observed for some conditions. It is noted that the expected variation in chemical composition from coating surface to the substrate was found, with low dilution of vanadium. The hardness of the TiAl laser coatings is higher than the substrate and the bending tests results shown that the coatings have good adhesion but with limited ductility. The tribological properties of the coatings shows that in the wear tests at room temperature a lower wear rate is obtained compared to the substrate. In the case of high temperature, the coatings have a lower coefficient of friction; however, a higher wear rate is obtained when compared with the substrate. The coatings have good resistance to oxidation evaluated by isothermal oxidation tests in air at 800 ºC, when compared with the substrate, the thermal growth oxide up to 12 microns thick for 150 hours were obtained. The structure of the oxide layers is complex and comprises the growth of successive layers from the outer surface of the coating. We also studied the electrochemical corrosion behavior of the coatings obtained. The results indicate that the coaxial laser cladding can be a good alternative to obtain extensive TiAl intermetallic coatings, dense coatings with good substrate bonding and minimal defects were obtained, that improve the oxidation and wear behavior of Ti6Al4V alloy. / [ES] Los intermetálicos TiAl han demostrado tener un excelente comportamiento a alta temperatura, sin embargo, su procesado para la obtención de recubrimientos no es sencillo debido a su alto punto de fusión, por otra parte el plaqueado láser coaxial promete ser una excelente herramienta para la obtención de recubrimientos por solape de cordones, logrando la completa fusión y deposición de aleaciones con elevado punto de fusión sobre superficies con forma complejas. En esta tesis se ha estudiado los parámetros de procesado láser coaxial y el precalentamiento del sustrato para lograr recubrimientos con intermetálico Ti48Al2Cr2Nb sobre láminas de Ti6Al4V de 3 mm de espesor, con la finalidad de mejorar el comportamiento tribológico, de oxidación y de corrosión de la aleación Ti6Al4V. Del análisis geométrico y de dilución química de los cordones obtenidos con diversos niveles en las variables de procesado láser se logró identificar combinaciones que minimizan defectos como grietas, alta dilución y relación de aspecto inadecuadas. Se ha encontrado una relación directa entre la velocidad de enfriamiento y los parámetros del proceso láser coaxial, tal como la cantidad de polvo aportado y la velocidad de pasada. De esta manera el proceso ha sido optimizado minimizando la velocidad de enfriamiento con la disminución de la velocidad de pasada. De este análisis se ha seleccionado como temperatura adecuada de precalentamiento 350ºC y se han obtenido recubrimientos con un 40% de solape, utilizando parámetros de proceso que generan energías especificas aportadas por el láser de 70, 80, 90 y 180 J/mm2, los cuales han sido evaluados mediante microscopia óptica (MO), microscopia electrónica de barrido (MEB), difracción de rayos X (DRX), microdureza Vickers (HV) y nanoindentación. La microestructura de los recubrimientos se compone de fases gamma-TiAl y alfa2-Ti3Al. El precalentamiento del sustrato ha permitido la obtención de recubrimientos con buena unión metalúrgica, aunque se observan para algunas condiciones grietas y poros. Se observa que la variación en la composición química de la superficie del recubrimiento al sustrato es la esperada, con baja dilución del vanadio. La dureza de los recubrimientos obtenidos es más alta que la del sustrato, y en los ensayos de flexión se observó que los recubrimientos tienen buena adherencia pero limitada ductilidad. El comportamiento tribológico de los recubrimientos muestra que en los ensayos de desgaste a temperatura ambiente se obtiene una tasa de desgaste menor por parte de los recubrimientos comparados con el sustrato. Para el caso de alta temperatura los recubrimientos presentan un menor coeficiente de fricción, sin embargo, se obtiene una mayor tasa de desgaste cuando se compara con el sustrato. De los ensayos de oxidación isotérmica se observó que los recubrimientos tienen buena resistencia a la oxidación en aire a 800ºC, al compararlos con el sustrato, llegando a obtener capas de óxidos de hasta 12 µm de espesor a 150 horas de oxidación. La estructura de las capas de óxidos es compleja y comprende el crecimiento de capas sucesivas a partir de la superficie externa del recubrimiento. También se ha estudiado el comportamiento a corrosión electroquímica de los recubrimientos obtenidos. Los resultados indican que el plaqueado láser coaxial puede ser una buena alternativa para la obtención de recubrimientos con intermetálicos TiAl, obteniendo recubrimientos densos, con buena unión al sustrato y mínimos defectos, que mejoran el comportamiento ante la oxidación y el desgaste de la aleación Ti6Al4V. / [CA] Els intermetàl·lics TiAl han demostrat tindre un excel·lent comportament a alta temperatura, però, el seu processat per a l'obtenció de recobriments no és senzill degut al seu alt punt de fusió, d'altra banda el plaquejat làser coaxial promet ser una excel·lent eina per a l'obtenció de recobriments per solapament de cordons, aconseguint la completa fusió i deposició de aliatges amb elevat punt de fusió sobre superfícies amb forma complexes. En aquesta tesi s'ha estudiat els paràmetres de processament làser coaxial i el preescalfament del substrat per aconseguir recobriments amb intermetàl·lic Ti48Al2Cr2Nb sobre làmines de Ti6Al4V de 3 mm de espessor, amb la finalitat de millorar el comportament tribològic, d'oxidació i de corrosió de l'aliatge Ti6Al4V. De l'anàlisi geomètric i de dilució química dels cordons obtinguts amb diversos nivells en les variables de processat làser es va aconseguir identificar combinacions que minimitzen defectes com esquerdes, alta dilució i relació d'aspecte inadequades. S'ha trobat una relació directa entre la velocitat de refredament i els paràmetres del procés làser coaxial, tal com la quantitat de pols aportat i la velocitat de passada. D'aquesta manera el procés ha estat optimitzat minimitzant la velocitat de refredament amb la disminució de la velocitat de passada. D'aquesta anàlisi s'ha seleccionat com a temperatura adequada de preescalfament 350 ºC i s'han obtingut recobriments amb un 40% de solapament, utilitzant paràmetres de procés que generen energies especifiques aportades pel làser de 70, 80, 90 i 180 J/mm2, els quals han estat avaluats mitjançant microscòpia òptica (MO), microscòpia electrònica de rastreig (MER), difracció de raigs X (DRX), microduresa Vickers (HV) i nanoindentació. La microestructura dels recobriments es compon de fases gamma-TiAl i alfa2-Ti3Al. El preescalfament del substrat ha permès l'obtenció de recobriments amb bona unió metal·lúrgica, tot i que s'observen per a algunes condicions esquerdes i porus. S'observa que la variació en la composició química de la superfície del recobriment al substrat és l'esperada, amb baixa dilució del vanadi. La duresa dels recobriments obtinguts és més alta que la del substrat, i en els assajos de flexió es va observar que els recobriments tenen bona adherència però limitada ductilitat. El comportament tribològic dels recobriments mostra que en els assajos de desgast a temperatura ambient s'obté una taxa de desgast menor per part dels recobriments comparats amb el substrat. Per al cas d'alta temperatura, els recobriments presenten un menor coeficient de fricció, però, s'obté una major taxa de desgast quan es compara amb el substrat. Dels assajos d'oxidació isotèrmica es va observar que els recobriments tenen bona resistència a l'oxidació en aire a 800ºC, al comparar-los amb el substrat, arribant a obtenir capes d'òxids de fins a 12 micres de gruix a 150 hores d'oxidació. L'estructura de les capes d'òxids és complexa i comprèn el creixement de capes successives a partir de la superfície externa del recobriment. També s'ha estudiat el comportament a corrosió electroquímica dels recobriments obtinguts. Els resultats indiquen que el plaquejat làser coaxial pot ser una bona alternativa per a l'obtenció de recobriments amb intermetàl·lic TiAl, obtenint recobriments densos, amb bona unió al substrat i mínims defectes, que milloren el comportament davant l'oxidació i el desgast de l'aliatge Ti6Al4V. / Zambrano Carrullo, JC. (2015). Desarrollo y caracterización de recubrimientos TiAl mediante procesado láser coaxial sobre Ti6Al4V [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/56148

O presente trabalho visou determinar a tenacidade à fratura dinâmica, KID, primeiramente pelos conceitos da Mecânica da Fratura Elástica Linear (MFEL) e posteriormente pela Mecânica da Fratura Elasto-Plástica (MFEP), JID, em materiais que em operação podem estar sujeitos a impactos em diferentes temperaturas. Os materiais estudados, de uso na indústria aeronáutica, foram uma liga de titânio Ti6Al4V (norma SAE AMS 4911), na condição recozida e uma liga de aço inoxidável PH 15-5 (norma SAE AMS 5659), na condição H1000. Os corpos de prova pré-trincados e entalhados foram retirados nas orientações L-T e L-S, a fim de que fossem determinadas e comparadas a relação tenacidade/densidade ou tenacidade específica dos materiais estudados. Em seguida os corpos de prova foram ensaiados sob condições de carga dinâmica em uma máquina de ensaio Charpy instrumentado, marca Instron-Wolpert PW30, conforme a norma ASTM-E23, com velocidade de carregamento de 5,52 m/s e nas temperaturas de 23 e 400ºC. Os valores das tenacidades, posteriormente comparados e correlacionados, foram obtidos de acordo com as expressões matemáticas mencionadas na literatura. A razão entre as energias estimadas de iniciação (Ei) e de propagação (Ep), (Ei/Ep), foi obtida a partir dos gráficos de carga-deslocamento x tempo. A determinação e caracterização dos aspectos macro e microscópicos da fratura foram realizadas através de microscopia ótica e de varredura. Em seguida, confrontaram-se os valores e os aspectos preponderantes dos mecanismos de fratura apresentados por cada material. / The present work aimed to evaluate the dynamic fracture toughness, KID, firstly using the Linear Elastic Fracture Mechanics parameter, (LEFM), and secondly using the Elasto-Plastic Fracture Mechanics (EPFM), JID. The materials used in this work are from aeronautic grade and are subjected to in service impact loads and temperature variation. The materials are a titanium alloy Ti6Al4V (standard SAE AMS 4911), in the annealed condition and a PH 15-5 stainless steel (standard SAE AMS 5659), H1000 condition. Both precracked and notched specimens were taken in the L-T and L-S directions, for the evaluation and comparison of the toughness/density ratio, i. e., the specific dynamic fracture toughness of the materials studied. Therefore, the specimens were tested under dynamic load using an Instron-Wolpert PW30 Instrumented Charpy Equipment, following the ASTM-E23 standard, with load speed of 5,52 m/s at 23 and 400ºC. The fracture toughness values were compared using mathematical expression from literature. The ration between the initiation (Ei) and propagation (Ep) energies, (Ei/Ep), was obtained from the load-displacement x time. The characterization of the macro and microscopic aspects of the fracture mechanisms were carried out using optical microscope and scan electronic microscope. The fracture toughness values and the fractographic observations were correlated and compared for the two materials studied.

La fusion Sélective Laser (SLM), en tant que procédé de fabrication additive, permet la conception de formes complexes par une méthode de construction couche par couche, à partir d’un lit de poudre. L’interaction entre la poudre et l’onde électromagnétique est encore trop peu maîtrisée pour stabiliser efficacement la zone de fusion, et optimiser l’énergie utilisée lors du procédé. Cette étude a pour objectif : (a) la compréhension et la maîtrise des mécanismes de mise en couche par rouleau, propre aux machines SLM Phenix; (b) l’analyse et la quantification des évolutions morphologiques et microstructurales de cordons de fusion en fonction des paramètres du procédé SLM et des paramètres du lit de poudre définis précédemment ; (c) l’élaboration d’un modèle thermique et microstructurale représentatif de l’édification de cordons unitaires par le procédé SLM. Lors de cette étude, le procédé de mise en couche par rouleau a été étudié, et modélisé, afin de contrôler les épaisseurs et taux de compacités du lit de poudre. Les caractéristiques des cordons unitaires de Ti6Al4V produits par SLM ont pu alors être analysées en fonction des paramètres du lit de poudre et des paramètres énergétiques. Cette démarche a pour but de quantifier l’impact du conditionnement du lit de poudre sur le mécanisme de fusion SLM. Par la suite, une analyse fine et une reconstitution microstructurale a pu en être dégagée. Enfin, un modèle thermique radiatif couplé à une prédiction microstructurale des cordons unitaires a pu être élaboré, permettant ainsi une compréhension approfondie du mécanisme de fusion. / Selective Laser Melting (SLM), through additive manufacturing process, allows the conception of specific shapes through a layer-by-layer building method from a powder bed. The emphasis between processing parameters as, laser power, scan speed, scan strategy… has already been well investigated for a wide panel of material. Nevertheless, the powder interaction with electromagnetic waves remains a topical issue to handle the stabilization of the melting pool, and optimize the amount of energy used within the process.The purpose of this survey is : (a) the understanding and handling of powder bed layering mechanism through SLM Phenix rolling blade ; (b) the analysis and quantification of morphological and microstructural evolutions single tracks according to SLM process and powder bed parameters ; (c) development of a thermal and microstructural model standing for post SLM single tracks edification.First of all, the process of powder spreading by rolling blade has been investigated in order to tame and modelize the porosity and effective thickness of the powder bed. Thereafter, characteristics of Ti6Al4V single tracks produced by SLM were analyzed according to process and bed powder parameters. This approach tends to quantify the impact of the powder bed packing on the SLM melting mechanism. Accordingly, fine microstructural analysis and reconstruction have been extracted. Finally, a radiative thermal model linked to a microstructural prediction of single tracks has been settled, leading to a deeper understanding of the melting mechanism.

O presente trabalho visou determinar a tenacidade à fratura dinâmica, KID, primeiramente pelos conceitos da Mecânica da Fratura Elástica Linear (MFEL) e posteriormente pela Mecânica da Fratura Elasto-Plástica (MFEP), JID, em materiais que em operação podem estar sujeitos a impactos em diferentes temperaturas. Os materiais estudados, de uso na indústria aeronáutica, foram uma liga de titânio Ti6Al4V (norma SAE AMS 4911), na condição recozida e uma liga de aço inoxidável PH 15-5 (norma SAE AMS 5659), na condição H1000. Os corpos de prova pré-trincados e entalhados foram retirados nas orientações L-T e L-S, a fim de que fossem determinadas e comparadas a relação tenacidade/densidade ou tenacidade específica dos materiais estudados. Em seguida os corpos de prova foram ensaiados sob condições de carga dinâmica em uma máquina de ensaio Charpy instrumentado, marca Instron-Wolpert PW30, conforme a norma ASTM-E23, com velocidade de carregamento de 5,52 m/s e nas temperaturas de 23 e 400ºC. Os valores das tenacidades, posteriormente comparados e correlacionados, foram obtidos de acordo com as expressões matemáticas mencionadas na literatura. A razão entre as energias estimadas de iniciação (Ei) e de propagação (Ep), (Ei/Ep), foi obtida a partir dos gráficos de carga-deslocamento x tempo. A determinação e caracterização dos aspectos macro e microscópicos da fratura foram realizadas através de microscopia ótica e de varredura. Em seguida, confrontaram-se os valores e os aspectos preponderantes dos mecanismos de fratura apresentados por cada material. / The present work aimed to evaluate the dynamic fracture toughness, KID, firstly using the Linear Elastic Fracture Mechanics parameter, (LEFM), and secondly using the Elasto-Plastic Fracture Mechanics (EPFM), JID. The materials used in this work are from aeronautic grade and are subjected to in service impact loads and temperature variation. The materials are a titanium alloy Ti6Al4V (standard SAE AMS 4911), in the annealed condition and a PH 15-5 stainless steel (standard SAE AMS 5659), H1000 condition. Both precracked and notched specimens were taken in the L-T and L-S directions, for the evaluation and comparison of the toughness/density ratio, i. e., the specific dynamic fracture toughness of the materials studied. Therefore, the specimens were tested under dynamic load using an Instron-Wolpert PW30 Instrumented Charpy Equipment, following the ASTM-E23 standard, with load speed of 5,52 m/s at 23 and 400ºC. The fracture toughness values were compared using mathematical expression from literature. The ration between the initiation (Ei) and propagation (Ep) energies, (Ei/Ep), was obtained from the load-displacement x time. The characterization of the macro and microscopic aspects of the fracture mechanisms were carried out using optical microscope and scan electronic microscope. The fracture toughness values and the fractographic observations were correlated and compared for the two materials studied.

The aim of the diploma thesis is to evaluate the mechanical properties and fracture behavior of the weld join Ti6Al4V titanium alloy prepared by using an electron beam technology. The theoretical part deals with the welding of titanium alloys with the help of electron beam, the weldability evaluation of titanium alloys, the influence of electron beam welding on the microstructure and the methods of testing of weld joints. Using the experiments, the mechanical properties of the base material and the weld were evaluated and a structural analysis of the weld was performed.

Titanium alloys are major materials used in the airplane industry, and prospects show that airplane production will double in the next 20 years. Consequently, the demand for cutting tools for machining of titanium alloys will increase. The primary problem when machining titanium alloys is their low thermal conductivity. Crater wear is the main factor limiting tool life, and is generally caused by thermal diffusion due to high temperatures in the tool-chip interface. This master’s thesis was performed in collaboration with Sandvik Coromant, with the prospect to increase knowledge of how diffusion and chip formation influences crater wear progression. The aim was to study tool wear of cutting tools when turning Ti–6Al–4V. This was done by testing two different rake face geometries, both coated and uncoated, at cutting speeds of 30–115 m/min. Diffusion was investigated to learn about the impact it has on crater wear. Chips were examined to investigate chip formation and shear strain. The coated modified rake face insert showed less crater wear only for the initial few seconds of machining. Uncoated inserts with a modified rake face showed higher diffusion rate and faster crater wear progression than did standard inserts. The standard inserts showed twice as long tool life as did the modified inserts. No significant differences in the chip formation mechanism were found between modified and standard inserts. Cracks were found within shear bands that were thinner than usual, which suggest that the generation of cracks allows less shear deformation.

O presente trabalho apresenta um breve apanhado do processo de forjamento, resultados da investigação experimental e da análise computacional acerca do teste de compressão do anel e ensaio do tubo cônico, ambos visando a determinação do coeficiente de atrito existente na região de contato entre as matrizes e os corpos-de-prova, para as ligas de alumínio AA6351 e de titânio Ti6Al4V. Foram realizadas curvas teóricas de calibração do coeficiente de atrito tanto para o alumínio quanto para o titânio com faixa de temperatura distinta para cada um dos materiais. Após a realização da calibração por meio das curvas foram realizados os ensaios práticos de compressão do anel e do tubo cônico, também foram realizadas as simulações computacionais dos ensaios do tubo. Estas simulações permitiram a verificação teórica do fluxo de material no interior dos corpos de prova comparando-as com o material obtido em ensaios práticos, comprovando a eficiência dos programas de simulação, visto que a geometria do tubo favorece a comparação entre a simulação e os testes experimentais. Os resultados obtidos tanto nos experimentos teóricos como os práticos, efetuou-se uma comparação com os dados das referências bibliográficas descritas neste trabalho. Em que os dois lubrificantes testados apresentaram desempenho satisfatório, devido à redução do contato interfacial da relação matriz/peça. E o ensaio do tubo cônico mostrou-se viável apenas para determinação a quente do coeficiente de atrito, neste caso o comportamento em ambos os ensaios é similar. / This paper presents a brief overview of the forging process and the results of experimental investigation and computational analysis of ring compression testing and conical tube-upsetting test, both aiming to determine the coefficient of friction in the region of contact between die and bodies-of-evidence for the AA6351 aluminum alloy and titanium Ti6Al4V. Theoretical calibration through curves were performed of the coefficient of friction were performed for both aluminum and titanium with different temperature range for each material. After completion of the calibration curves compression ring and the conical tube practical tests were performed, computer simulations of the tube-upsetting test were also performed. Continue) These simulations allowed to verify the theoretical flow of material within the samples and comparing them with the material obtained in practical tests, proving the efficiency of simulation programs, since the geometry of the tube facilitates the comparison between the simulation and testing experiments. The results in both theoretical and practical experiments, were a compared with the data from the references described herein. Two oils tested showed a satisfactory performance due to the reduced interfacial contact relationship die/workpiece. And the tube-upsetting test was feasible only to determine the hot coefficient of friction, in this case the behavior in both tests is similar.