Magnesium and magnesium alloys are used in a wide variety of structural applications including automotive, aerospace, hand tools and electronic industries thanks to their light weight, high specific strength, adequate corrosion resistance and good castability. Al and Zn are the primary alloying elements in commercial Mg alloys and commonly used in automotive industries. AZ91 is one of the most popular Mg alloys containing 9% Al and 1% Zn. Hence, lots of research have been done during last decades on AZ91D. However, the existing data concerning mechanical properties and microstructural features showed large scatter and is even contradictory. This work focused on the correlation between the microstructure and the mechanical properties of as-cast AZ91 alloy. An exhaustive characterization of the grain size, secondary dendrite arm spacing (SDAS) distribution, and fraction of Mg17Al12 using optical and electron backscattered diffraction (EBSD) was performed. These microstructural parameters were correlated to offset yield point (Rp0.2), fracture strength and elongation to fracture. It was understood that the intermetallic phase, Mg17Al12, plays an important role in determining the mechanical and physical properties of the alloy at temperature range from room temperature up to 190oC. It was realized that by increasing the Mg17Al12 content above 11% a network of intermetallic may form. During deformation this rigid network should break before any plastic deformation happen. Hence, increase in Mg17Al12 content resulted in an increase in offset yield point. The presence of this network was supported by study of thermal expansion behaviour of the alloy containing different amount of Mg17Al12. A physically-based model was adapted and validated in order to predict the flow stress behaviour of as-cast AZ91D at room temperature up to 190ºC for various microstructures. The model was based on dislocation glide and climb in a single-phase (matrix) material containing reinforcing particles. The temperature dependant variables of the model were quite well correlated to the underlying physics of the material.

The effect of deformation on microstructural changes in metals and alloys is the subject of considerable practical interest. The ultimate goal is to control, improve and optimize the microstructure and texture of the finished products produced by metal forming operations. The development in the subject field is remarkable but a more in-depth study could lead us to the better understanding of the phenomena.   In the present work microstructural evolution during the plastic deformation of as-cast pure metals and alloys is studied. An experimental method was developed to study the material behavior under the hot compression testing. This method was applied on the as-cast structure of copper, bearing steel, Incoloy 825 and β brass at different temperatures and strain rates. The temperature of the samples was measured during and after the deformation process. The microstructure of the samples was examined by optical microscopy and scanning electron microscopy (SEM). The microstructural evolution during deformation process was investigated by transmission electron microscopy (TEM) and electron backscatter diffraction (EBSD). The samples were subsequently subjected to electron microprobe analysis (EMPA) to investigate the effect of the deformation on the microsegregation of Mo, Cr, Si, and Mn.   It was observed that the temperature of the samples deformed at strain rates of 5 and 10 s-1 increases abruptly after the deformation stops. However, compression test at the lower strain rates of 1 and 0.5 s-1 revealed that a constant temperature was maintained in the early stage of deformation, followed by an increase until the maximum temperature was obtained. This temperature behavior can be explained by the microstructural evolution during the deformation process. Micrograph analysis revealed the formation of deformation bands (DBs) in highly strained regions. The DBs are highly effective sites for recrystallization. The interdendritic regions are suitable sites for the formation of DBs due to the high internal energy in these regions. EMPA indicated a tendency towards uphill diffusion of Mo in the DBs with increasing strain. The effect of strain on the dissolution of carbides in the band structure of bearing steel was investigated by measuring the volume fraction of carbides inside the band structure at different strain levels. The results indicate that carbide dissolution is influenced by strain.    The microstructural evolution inside the DBs was studied as a function of several properties: temperature, internal energy, and microsegregation. Compression of β brass revealed that twinning is the most prominent feature in the microstructure. EBSD analysis and energy calculations demonstrated that the twinning is not due to a martensitic process but rather the order/disorder transition during the deformation process. The effect of heat treatment at Tc (650°C) prior to deformation on the microstructure of β brass was also investigated, which revealed a relationship between twin formation and the anti-phase domain boundaries / <p>QC 20131104</p>

No description available.

Neste trabalho foi medida a tenacidade à fratura de quatro ligas fundidas com composição química base do aço AISI M2 – uma de composição química convencional (liga I), e as demais modificadas por adições de nitrogênio (liga II), cério (liga III) e antimônio (liga IV) – submetidas a tratamentos térmicos visando a decomposição do carboneto M2C, a esferoidização e engrossamento dos carbonetos produto M6C e MC, em altas temperaturas e por diversos tempos. A metodologia empregada nesta avaliação da tenacidade à fratura foi a dos corpos de prova curtos com entalhe chevron segundo ASTM E 1304-97, de forma a superar a necessidade do pré-trincamento por fadiga, procedimento de difícil controle e custoso em materiais como os aços rápidos temperados e revenidos. Verificou-se que a metodologia utilizada para obtenção e ensaio de corpos de prova chevron foi de fácil execução (comparada à metodologia convencional) permitindo grande número de experimentos. Para verificar a consistência dos resultados, em algumas condições, também se utilizou a metodologia convencional segundo a ASTM E 399-90, cujo pré-trincamento foi feito utilizando os procedimentos propostos por Harris e Dunegan. Os resultados obtidos para os aços fundidos foram correlacionados com os obtidos para outros aços rápidos convencionais (VM2, M2 Thyssen) e um aço rápido sinterizado (SINTER 23). A microestrutura foi caracterizada utilizando-se técnicas de ataques metalográficos diferenciais, metalografia quantitativa manual e computadorizada e microscopia eletrônica de varredura. A avaliação microestrutural indica que não ocorreu precipitação eutética do carboneto M6C, em nenhuma das ligas fundidas. O carboneto M2C apresenta morfologia tanto irregular (plaquetas – tipo 1) quanto regular-complexa (lamelas – tipo 2). As ligas I, III e IV, apresentaram a predominância da morfologia tipo 1 enquanto que a liga II modificada pelo nitrogênio, apresentou apenas a morfologia tipo 2. O carboneto MC apresentou-se com morfologia regular-complexa. Medidas do espaçamento interdendrítico indicam que não houve influência significativa dos elementos modificadores sobre este parâmetro. Ensaios de resistência à flexão, indicam pouca influência dos elementos modificadores, mas forte influência dos tratamentos térmicos sobre o limite de resistência à ruptura transversal do aço fundido. Em todas as ligas, a resistência à flexão cresceu com o tempo de tratamento a 1200°C, bem como com a temperatura de decomposição em tratamentos por 2 horas. Análise das fraturas por microscopia eletrônica de varredura indicou que o crescimento das trincas se deu na região interdendrítica. O aço convencional apresentou resistência à ruptura transversal muito superior à dos aços fundidos. Os ensaios de tenacidade à fratura apresentaram resultados compatíveis com a literatura para os aços AISI M2 convencional e SINTER 23. Os resultados obtidos para o aço fundido, indicam queda nos valores de tenacidade à fratura nos materiais tratados a 1050°C com o avanço do tempo de tratamento; pouca variação dos valores com o tempo nas amostras tratadas a 1150°C; e aumento significativo da tenacidade à fratura com o tempo de tratamento a 1200°C. Os valores de tenacidade obtidos para os aços rápidos fundidos foram mais elevados que os obtidos para os materiais trabalhados e para o material sinterizado. / Fracture Toughness of four cast alloys with chemical composition based on the High-Speed Steel AISI M2 were measured. One of the alloys (alloy I) had the conventional AISI M2 composition, while the other three were modified by the addition of N (alloy II), Ce (alloy III) and Sb (alloy IV). The cast alloys were heat-treated in order to promote the decomposition of the M2C carbide as well as spheroidize and coarsen the product M6C e MC carbides. The method chosen for measuring fracture toughness was based on the use of short rod and bar chevron notched samples, according to ASTM E1304 – 97, in order to evade the need for fatigue pre-cracking, notoriously difficult for High Speed Steels quenched and tempered. The chevron-notch method proved straightforward and allowed for successful testing a great number of specimens. Conventional compact sample fracture toughness, according to ASTM E 399-90, with pre-cracking obtained using Harris-Dunegan drop-weight procedure, was used to validate the results. The results for cast alloys were compared with conventionally produced High Speed Steels (VM2, M2 Thyssen) and with a powder metallurgy High Speed Steel (SINTER 23). Microstructural characterization was performed using selective etching of polished surfaces, manual and automated quantitative metallography and SEM. Microstructural evaluation of as-cast alloys showed that there was no eutectic precipitation of M6C carbides. The M2C carbides show an irregular eutectic morphology (Type 1- plates) as well as a regular-complex eutectic morphology. Measurements of interdendritic spacing did not detect any effect of the modification. The bending test rupture strengths did not vary with the addition of modifying elements, but increased with the time and temperature of decomposition, spheroidization and coarsening of carbides. Rupture strengths increased with the heat-treatment time at 1200°C as well as with increasing temperatures for 2 h heat-treatments. SEM examination of the fracture surfaces showed that crack preferential growth path was interdendritical. Conventional High Speed Steels tested in bending presented better results for the rupture strength than cast steels. Fracture toughness results for M2 conventional steels and for the SINTER 23 steel were similar to the results from the literature. Fracture toughness results obtained for cast steels diminished with increasing decomposition time at 1050°C, did not change much with increasing decomposition time at 1150°C, increased markedly withy increasing decomposition times at 1200°C. The fracture toughness results for the as-cast steels were higher than the results obtained for the wrought steels and for the powder metallurgy steel.

The demanding structural applications (e.g. aerospace, biomedical, etc.) require new materials with improved mechanical performance. The novel Ti-based dendrite + nano-/ultrafine-structured (Ti-based DNUS) composites exhibit an advantageous combination of high compressive strength (2000 – 2500 MPa) and large compressive ductility (10 – 30 %) already in the as-cast state [1,2] and, therefore, can be referred as high-performance materials. However, these Ti-based composites frequently exhibit very low or even lack of tensile ductility [3]. Therefore, the aim of this research work is to develop high strength Ti-based DNUS composites with pronounced tensile plasticity and to correlate the mechanical properties with their microstructure. In order to reach the goal, the high-strength Ti66Nb13Cu8Ni6.8Al6.2 (at.%) alloy exhibiting large compressive ductility [4] was selected for the modification. The microstructure of Ti66Nb13Cu8Ni6.8Al6.2 is composed of two metallographic constituents including β-Ti dendrites and an interdendritic component. The β-Ti dendrites are enriched in Nb and, therefore, Nb is referred as “dendritic element” whereas the interdendritic component is enriched in Ni and Cu and, therefore, these are referred as “interdendritic elements”. To perform a systematic study of the “interdendritic elements” (Ni, Cu and Co) effect on microstructure, a number of alloys with different concentration and types of alloying elements (Ti-Nb-Cu-Ni-Al, Ti-Nb-Co-Ni-Al, Ti-Nb-Cu-Co-Al and Ti-Nb-Ni(Co)-Al) were developed. It was shown that a higher concentration of the “interdendritic elements” in a composition within one alloy system corresponds to a higher volume fraction of the interdendritic component. Additionally, the crystal structure of the interdendritic phases is affected by type of the “interdendritic elements”. Since the most advanced applications (e.g. aerospace) require materials with high specific strengths, the new ductile Ti-Nb-Cu-Ni-Al alloys were modified to reduce their density, i.e. the Nb was substituted by lighter V. As a result, a new family of Ti-V-Cu-Ni-Al alloys with improved specific strength compared to the Ti-Nb-Cu-Ni-Al alloys was developed. Additionally, moduli of resilience of the Ti-V-Ni-Cu-Al alloys are superior when compared with those of the commercial Ti-based spring materials. The effect of microstructure on deformation of the newly developed alloys was studied through the in-situ microstructural analysis of samples at different strained states by means of scanning electron microscopy. To reveal the effect of the metallographic constituents on strength, the microhardness mapping of the new alloys was performed. Using the obtained empirical principles of microstructure adjustment, a new Ti68.8Nb13.6Co6Cu5.1Al6.5 (at.%) alloy with a large static toughness (superior to those of the recently developed Ti-based metallic glass composites) was developed. This large static toughness is due to both high strength and significant tensile plasticity. To study the effect of microstructure on tensile plasticity of Ti68.8Nb13.6Co6Cu5.1Al6.5 the in-situ microstructural analysis of samples at different strained states in the scanning electron microscope as well as the transmission electron microscopy studies were performed. / Der erhöhte Anspruch an strukturelle Anwendungen (z.B. Luftfahrt, Biomedizin, etc.) verlangt neue Werkstoffe mit verbesserten mechanischen Leistungsfähigkeiten. Neuartige Ti-basierte dendritische nano-/ultrafeine Komposite (Ti-basierte DNUS Komposite) besitzen eine vorteilhafte Kombination von hoher Druckfestigkeit mit großer plastischer Verformbarkeit unter Druckbelastung bereits im Gusszustand [1,2] wodurch sie als hochleistungsfähige Werkstoffe angesehen werden. Jedoch besitzen diese Ti-basierte DNUS Komposite heufig eine stark verringerte oder gar keine Duktilität unter Zugbelastung [3]. Deswegen ist es das Ziel dieser Forschungsarbeit neue hochfeste Ti-basierte DNUS Komposite mit ausgeprägter Duktilität unter Zugbelastung zu entwickeln und die mechanischen Eingeschaften mit ihrer Mikrostruktur zu korrelieren. Um dieses Ziel zu erreichen wurde die hochfeste Legierung Ti66Nb13Cu8Ni6.8Al6.2 (at.%) [4], die eine große plastische Verformbarkeit unter Druckbelastung aufweist, ausgewählt. Die Mikrostruktur von Ti66Nb13Cu8Ni6.8Al6.2 setzt sich aus zwei metallographischen Konstituenten, einschließlich β-Ti Dendriten und einer interdendritischen Komponente, zusammen. Die β-Ti Dendriten sind mit Nb angereichert, weswegen Nb als “dendritisches Element” bezeichnet wird, wohingegen die interdendritische Komponente mit Ni und Cu angereichert ist und deswegen diese als “interdendritische Elemente” bezeichnet werden. Um den Einfluss der “interdendritischen Elemente” (Ni, Cu and Co) auf die Mikrostruktur zu untersuchen wurden Legierungen mit verschiedenen Konzentrationen unterschiedlicher Legierungselemente (Ti-Nb-Cu-Ni-Al, Ti-Nb-Co-Ni-Al, Ti-Nb-Cu-Co-Al and Ti-Nb-Ni(Co)-Al) entwickelt. Es wurde gezeigt, dass eine höhere Konzentration “interdendritischer Elemente” in einer bestimmten Zusammensetzung einem höheren Volumanteil der interdendritischen Komponente entspricht. Zusätzlich wird die Kristallstruktur der interdendritischen Phase sehr stark durch die “interdendritischen Elemente” beeinflusst. Da die meisten hoch entwickelten Anwendungen (z.B. Luftfahrt) gesteigerte spezifische Festigkeiten erforden, wurden die neuen duktilen Ti-Nb-Cu-Ni-Al Legierungen modifiziert um ihre Dichte zu reduzieren, indem Nb durch das leichtere V ersetzt wurde. Als Ergebniss wurde eine neue Familie von Ti-V-Cu-Ni-Al Legierungen, mit im Vergleich zu Ti-Nb-Cu-Ni-Al Legierungen verbesserten spezifischen Festigkeiten, entwickelt. Zusäzlich ist die elastische Formänderungsenergiedichte der neu entwickelten Legierungen höher verglichen mit kommerziellen Ti-basierten Federmaterialien. Der Effekt der Mikrostruktur auf das Verformungsverhalten der Legierungen wurde mittels in-situ mikrostruktureller Analysen verschiedener Verformungszustände im Rasterelektronenmikroskop untersucht. Um ein Einfluss der metallographischen Konstituenten auf die Festigkeit zu bestimmen wurden Mikrohärtekarten erstellt. Unter Verwendung der erhalten empirischen Prinzipen zur Einstellung der Mikrostruktur wurde eine neue Legierung Ti68.8Nb13.6Co6Cu5.1Al6.5 (at.%) mit hoher statischer Zähigkeit (besser als die der kürzlich entwickelten Ti-basierten gläsernen metallischen Kompositlegierungen) entwickelt. Diese hohe statische Zähigkeit wird sowohl durch die hohe Festigkeit als auch durch die ausgeprägte Plastizität unter Zugbelastung verursacht. Um den Einfluss der Mikrostruktur auf die Plastizität unter Zug zu untersuchen wurde Transmissionelektronmikroskopie sowie in-situ mikrostrukturelle Analysen verschiedener Verformungszustände im Rasterelektronmikroskop durchgefühlt.

Neste trabalho foi medida a tenacidade à fratura de quatro ligas fundidas com composição química base do aço AISI M2 – uma de composição química convencional (liga I), e as demais modificadas por adições de nitrogênio (liga II), cério (liga III) e antimônio (liga IV) – submetidas a tratamentos térmicos visando a decomposição do carboneto M2C, a esferoidização e engrossamento dos carbonetos produto M6C e MC, em altas temperaturas e por diversos tempos. A metodologia empregada nesta avaliação da tenacidade à fratura foi a dos corpos de prova curtos com entalhe chevron segundo ASTM E 1304-97, de forma a superar a necessidade do pré-trincamento por fadiga, procedimento de difícil controle e custoso em materiais como os aços rápidos temperados e revenidos. Verificou-se que a metodologia utilizada para obtenção e ensaio de corpos de prova chevron foi de fácil execução (comparada à metodologia convencional) permitindo grande número de experimentos. Para verificar a consistência dos resultados, em algumas condições, também se utilizou a metodologia convencional segundo a ASTM E 399-90, cujo pré-trincamento foi feito utilizando os procedimentos propostos por Harris e Dunegan. Os resultados obtidos para os aços fundidos foram correlacionados com os obtidos para outros aços rápidos convencionais (VM2, M2 Thyssen) e um aço rápido sinterizado (SINTER 23). A microestrutura foi caracterizada utilizando-se técnicas de ataques metalográficos diferenciais, metalografia quantitativa manual e computadorizada e microscopia eletrônica de varredura. A avaliação microestrutural indica que não ocorreu precipitação eutética do carboneto M6C, em nenhuma das ligas fundidas. O carboneto M2C apresenta morfologia tanto irregular (plaquetas – tipo 1) quanto regular-complexa (lamelas – tipo 2). As ligas I, III e IV, apresentaram a predominância da morfologia tipo 1 enquanto que a liga II modificada pelo nitrogênio, apresentou apenas a morfologia tipo 2. O carboneto MC apresentou-se com morfologia regular-complexa. Medidas do espaçamento interdendrítico indicam que não houve influência significativa dos elementos modificadores sobre este parâmetro. Ensaios de resistência à flexão, indicam pouca influência dos elementos modificadores, mas forte influência dos tratamentos térmicos sobre o limite de resistência à ruptura transversal do aço fundido. Em todas as ligas, a resistência à flexão cresceu com o tempo de tratamento a 1200°C, bem como com a temperatura de decomposição em tratamentos por 2 horas. Análise das fraturas por microscopia eletrônica de varredura indicou que o crescimento das trincas se deu na região interdendrítica. O aço convencional apresentou resistência à ruptura transversal muito superior à dos aços fundidos. Os ensaios de tenacidade à fratura apresentaram resultados compatíveis com a literatura para os aços AISI M2 convencional e SINTER 23. Os resultados obtidos para o aço fundido, indicam queda nos valores de tenacidade à fratura nos materiais tratados a 1050°C com o avanço do tempo de tratamento; pouca variação dos valores com o tempo nas amostras tratadas a 1150°C; e aumento significativo da tenacidade à fratura com o tempo de tratamento a 1200°C. Os valores de tenacidade obtidos para os aços rápidos fundidos foram mais elevados que os obtidos para os materiais trabalhados e para o material sinterizado. / Fracture Toughness of four cast alloys with chemical composition based on the High-Speed Steel AISI M2 were measured. One of the alloys (alloy I) had the conventional AISI M2 composition, while the other three were modified by the addition of N (alloy II), Ce (alloy III) and Sb (alloy IV). The cast alloys were heat-treated in order to promote the decomposition of the M2C carbide as well as spheroidize and coarsen the product M6C e MC carbides. The method chosen for measuring fracture toughness was based on the use of short rod and bar chevron notched samples, according to ASTM E1304 – 97, in order to evade the need for fatigue pre-cracking, notoriously difficult for High Speed Steels quenched and tempered. The chevron-notch method proved straightforward and allowed for successful testing a great number of specimens. Conventional compact sample fracture toughness, according to ASTM E 399-90, with pre-cracking obtained using Harris-Dunegan drop-weight procedure, was used to validate the results. The results for cast alloys were compared with conventionally produced High Speed Steels (VM2, M2 Thyssen) and with a powder metallurgy High Speed Steel (SINTER 23). Microstructural characterization was performed using selective etching of polished surfaces, manual and automated quantitative metallography and SEM. Microstructural evaluation of as-cast alloys showed that there was no eutectic precipitation of M6C carbides. The M2C carbides show an irregular eutectic morphology (Type 1- plates) as well as a regular-complex eutectic morphology. Measurements of interdendritic spacing did not detect any effect of the modification. The bending test rupture strengths did not vary with the addition of modifying elements, but increased with the time and temperature of decomposition, spheroidization and coarsening of carbides. Rupture strengths increased with the heat-treatment time at 1200°C as well as with increasing temperatures for 2 h heat-treatments. SEM examination of the fracture surfaces showed that crack preferential growth path was interdendritical. Conventional High Speed Steels tested in bending presented better results for the rupture strength than cast steels. Fracture toughness results for M2 conventional steels and for the SINTER 23 steel were similar to the results from the literature. Fracture toughness results obtained for cast steels diminished with increasing decomposition time at 1050°C, did not change much with increasing decomposition time at 1150°C, increased markedly withy increasing decomposition times at 1200°C. The fracture toughness results for the as-cast steels were higher than the results obtained for the wrought steels and for the powder metallurgy steel.

The demanding structural applications (e.g. aerospace, biomedical, etc.) require new materials with improved mechanical performance. The novel Ti-based dendrite + nano-/ultrafine-structured (Ti-based DNUS) composites exhibit an advantageous combination of high compressive strength (2000 – 2500 MPa) and large compressive ductility (10 – 30 %) already in the as-cast state [1,2] and, therefore, can be referred as high-performance materials. However, these Ti-based composites frequently exhibit very low or even lack of tensile ductility [3]. Therefore, the aim of this research work is to develop high strength Ti-based DNUS composites with pronounced tensile plasticity and to correlate the mechanical properties with their microstructure. In order to reach the goal, the high-strength Ti66Nb13Cu8Ni6.8Al6.2 (at.%) alloy exhibiting large compressive ductility [4] was selected for the modification. The microstructure of Ti66Nb13Cu8Ni6.8Al6.2 is composed of two metallographic constituents including β-Ti dendrites and an interdendritic component. The β-Ti dendrites are enriched in Nb and, therefore, Nb is referred as “dendritic element” whereas the interdendritic component is enriched in Ni and Cu and, therefore, these are referred as “interdendritic elements”. To perform a systematic study of the “interdendritic elements” (Ni, Cu and Co) effect on microstructure, a number of alloys with different concentration and types of alloying elements (Ti-Nb-Cu-Ni-Al, Ti-Nb-Co-Ni-Al, Ti-Nb-Cu-Co-Al and Ti-Nb-Ni(Co)-Al) were developed. It was shown that a higher concentration of the “interdendritic elements” in a composition within one alloy system corresponds to a higher volume fraction of the interdendritic component. Additionally, the crystal structure of the interdendritic phases is affected by type of the “interdendritic elements”. Since the most advanced applications (e.g. aerospace) require materials with high specific strengths, the new ductile Ti-Nb-Cu-Ni-Al alloys were modified to reduce their density, i.e. the Nb was substituted by lighter V. As a result, a new family of Ti-V-Cu-Ni-Al alloys with improved specific strength compared to the Ti-Nb-Cu-Ni-Al alloys was developed. Additionally, moduli of resilience of the Ti-V-Ni-Cu-Al alloys are superior when compared with those of the commercial Ti-based spring materials. The effect of microstructure on deformation of the newly developed alloys was studied through the in-situ microstructural analysis of samples at different strained states by means of scanning electron microscopy. To reveal the effect of the metallographic constituents on strength, the microhardness mapping of the new alloys was performed. Using the obtained empirical principles of microstructure adjustment, a new Ti68.8Nb13.6Co6Cu5.1Al6.5 (at.%) alloy with a large static toughness (superior to those of the recently developed Ti-based metallic glass composites) was developed. This large static toughness is due to both high strength and significant tensile plasticity. To study the effect of microstructure on tensile plasticity of Ti68.8Nb13.6Co6Cu5.1Al6.5 the in-situ microstructural analysis of samples at different strained states in the scanning electron microscope as well as the transmission electron microscopy studies were performed. / Der erhöhte Anspruch an strukturelle Anwendungen (z.B. Luftfahrt, Biomedizin, etc.) verlangt neue Werkstoffe mit verbesserten mechanischen Leistungsfähigkeiten. Neuartige Ti-basierte dendritische nano-/ultrafeine Komposite (Ti-basierte DNUS Komposite) besitzen eine vorteilhafte Kombination von hoher Druckfestigkeit mit großer plastischer Verformbarkeit unter Druckbelastung bereits im Gusszustand [1,2] wodurch sie als hochleistungsfähige Werkstoffe angesehen werden. Jedoch besitzen diese Ti-basierte DNUS Komposite heufig eine stark verringerte oder gar keine Duktilität unter Zugbelastung [3]. Deswegen ist es das Ziel dieser Forschungsarbeit neue hochfeste Ti-basierte DNUS Komposite mit ausgeprägter Duktilität unter Zugbelastung zu entwickeln und die mechanischen Eingeschaften mit ihrer Mikrostruktur zu korrelieren. Um dieses Ziel zu erreichen wurde die hochfeste Legierung Ti66Nb13Cu8Ni6.8Al6.2 (at.%) [4], die eine große plastische Verformbarkeit unter Druckbelastung aufweist, ausgewählt. Die Mikrostruktur von Ti66Nb13Cu8Ni6.8Al6.2 setzt sich aus zwei metallographischen Konstituenten, einschließlich β-Ti Dendriten und einer interdendritischen Komponente, zusammen. Die β-Ti Dendriten sind mit Nb angereichert, weswegen Nb als “dendritisches Element” bezeichnet wird, wohingegen die interdendritische Komponente mit Ni und Cu angereichert ist und deswegen diese als “interdendritische Elemente” bezeichnet werden. Um den Einfluss der “interdendritischen Elemente” (Ni, Cu and Co) auf die Mikrostruktur zu untersuchen wurden Legierungen mit verschiedenen Konzentrationen unterschiedlicher Legierungselemente (Ti-Nb-Cu-Ni-Al, Ti-Nb-Co-Ni-Al, Ti-Nb-Cu-Co-Al and Ti-Nb-Ni(Co)-Al) entwickelt. Es wurde gezeigt, dass eine höhere Konzentration “interdendritischer Elemente” in einer bestimmten Zusammensetzung einem höheren Volumanteil der interdendritischen Komponente entspricht. Zusätzlich wird die Kristallstruktur der interdendritischen Phase sehr stark durch die “interdendritischen Elemente” beeinflusst. Da die meisten hoch entwickelten Anwendungen (z.B. Luftfahrt) gesteigerte spezifische Festigkeiten erforden, wurden die neuen duktilen Ti-Nb-Cu-Ni-Al Legierungen modifiziert um ihre Dichte zu reduzieren, indem Nb durch das leichtere V ersetzt wurde. Als Ergebniss wurde eine neue Familie von Ti-V-Cu-Ni-Al Legierungen, mit im Vergleich zu Ti-Nb-Cu-Ni-Al Legierungen verbesserten spezifischen Festigkeiten, entwickelt. Zusäzlich ist die elastische Formänderungsenergiedichte der neu entwickelten Legierungen höher verglichen mit kommerziellen Ti-basierten Federmaterialien. Der Effekt der Mikrostruktur auf das Verformungsverhalten der Legierungen wurde mittels in-situ mikrostruktureller Analysen verschiedener Verformungszustände im Rasterelektronenmikroskop untersucht. Um ein Einfluss der metallographischen Konstituenten auf die Festigkeit zu bestimmen wurden Mikrohärtekarten erstellt. Unter Verwendung der erhalten empirischen Prinzipen zur Einstellung der Mikrostruktur wurde eine neue Legierung Ti68.8Nb13.6Co6Cu5.1Al6.5 (at.%) mit hoher statischer Zähigkeit (besser als die der kürzlich entwickelten Ti-basierten gläsernen metallischen Kompositlegierungen) entwickelt. Diese hohe statische Zähigkeit wird sowohl durch die hohe Festigkeit als auch durch die ausgeprägte Plastizität unter Zugbelastung verursacht. Um den Einfluss der Mikrostruktur auf die Plastizität unter Zug zu untersuchen wurde Transmissionelektronmikroskopie sowie in-situ mikrostrukturelle Analysen verschiedener Verformungszustände im Rasterelektronmikroskop durchgefühlt.

Made available in DSpace on 2014-12-17T15:42:01Z (GMT). No. of bitstreams: 1 IedaNSM.pdf: 5948604 bytes, checksum: dbf245a349dd04cff535e8ba2e89601d (MD5) Previous issue date: 2007-07-06 / The aim of this work was to study a series of 11 different compositions of Ti-Zr binary alloys resistance to aggressive environment, i. e., their ability to keep their surface properties and mass when exposed to them as a way to evaluate their performance as biomaterials. The first stage was devoted to the fabrication of tablets from these alloys by Plasma-Skull casting method using a Discovery Plasma machine from EDG Equipamentos, Brazil. In a second stage, the chemical composition of each produced tablet was verified. In a third stage, the specimen were submitted to: as-cast microstructure analysis via optical and scanning electron microscopy (OM and SEM), x-ray dispersive system (EDS) chemical analysis via SEM, Vickers hardness tests for mechanical evaluation and corrosion resistence tests in a 0.9% NaCl solution to simulate exposition to human saliva monitored by open circuit potential and polarization curves. From the obtained results, it was possible to infer that specimens A1 (94,07 wt% Ti and 5,93% wt% Zr), A4 (77,81 wt % Ti and 22,19 wt % Zr) and A8 (27,83 wt% Ti and 72,17 wt% Zr), presented best performance regarding to corrosion resistance, homogeneity and hardness which are necessary issues for biomaterials to be applied as orthopedic and odontological prosthesis / Este trabalho teve como finalidade estudar uma s?rie de onze ligas met?licas bin?rias, tit?nio zirc?nio, quanto ? capacidade de resistirem ?s deteriora??es sem sofrerem modifica??es de suas propriedades iniciais de massa e superf?cie quando expostas a meios agressivos, como condi??o fundamental para que as mesmas sejam aplicadas como biomateriais. A primeira etapa tratou da confec??o das amostras das ligas em forma de pastilhas, empregando-se o processo de fundi??o Plasma Skull realizado na m?quina Discovery Plasma, produzida no Brasil pela EDG Equipamentos. Na segunda etapa, as amostras confeccionadas foram submetidas aos ensaios para a determina??o da composi??o qu?mica resultante de cada liga da s?rie ap?s a fus?o. E durante a terceira etapa foram feitos os procedimentos de avalia??es das amostras quanto ? homogeneidade e apresenta??o da microestrutura de cada uma das ligas no estado bruto de fus?o, como resultados dos ensaios metalogr?ficos por microscopia ?ptica e microscopia eletr?nica de varredura acoplada a espectroscopia por energia dispersiva de raios-x; quanto ? propriedade mec?nica de dureza medida em escala Vickers (HV); e quanto ?s propriedades qu?micas de resist?ncia ? corros?o, quando expostas em solu??o de cloreto de s?dio 0,9 %, para simular a saliva, empregando-se o monitoramento do potencial de circuito aberto e as curvas de polariza??o. A partir dos resultados obtidos foi poss?vel identificar as pastilhas de composi??es qu?micas A1 (94,07% de Ti e 5,93% de Zr), A4 (77,81% de Ti e 22,19% de Zr) e A8 (27,83% de Ti e 72,17% de Zr) que resultaram como maiores detentoras do conjunto de propriedades de resist?ncia ? corros?o, homogeneidade e dureza, as quais s?o mais necess?rias em biomateriais tipo pr?teses ortop?dicas ou odontol?gicas