In the present work the deformation behaviour of magnesium-based alloy AZ31 which was produced by horizontal continual casting is investigated. Samples with two different orientations are deformed in tension and compression at strain rate of 10-3 s-1 in temperature range of 20 řC to 300 řC. Simultaneously, the acoustic emission is recorded and studied with focused on mechanical twinning. The mechanisms of plastic deformation of material and anisotropy between tension and compression are discussed. Dependence of deformation behaviour on temperature is analyzed. The microstructure of original and deformed material is also studied by means of optical microscopy.

The optimisation of compressor stage aerofoil and fan blade design remains an important area of titanium alloy research and development for aerospace gas turbines. Such research has important implications for critical and sensitive component integrity and efficiency. In particular, a better understanding of how deformation twinning interacts with microstructural features in titanium alloys is required, because such twinning facilitates plastic deformation at a higher strain rate than dislocations. To investigate this behaviour, commercial purity titanium and the titanium alloy Ti–6Al–4V were subjected to ballistic impact testing at room temperature with a high strain rate of 10³s⁻¹. In addition, a detailed analysis was conducted of three manufacturing processes of Ti–6Al–4V (wt. %) that are likely to cause deformation twinning: metallic shot peening, laser shock peening and deep cold rolling. The results presented in this thesis have furthered the understanding of the role of deformation twinning in the plastic deformation of α-phase titanium. Key findings of the research include the characterisation of deformation twinning types and the conditions that favour certain deformation twinning types. From the analysis of the ballistic testing of commercial purity titanium, the first definitive evidence for the existence of {112‾4} twinning as a rare deformation twinning mode at room temperature in coarse-grained commercial purity titanium is presented. In addition, the ballistic testing results of the Ti–6Al–4V alloy highlighted very different deformation twinning characteristics. Commercial purity titanium deformed plastically by a combination of {101‾2} and {112‾1} tensilve twinning and {112‾4} and {112‾2} compression twinning modes. By contrast, the deformation twinning of Ti–6Al–4V was limited to only the {101‾2} and {112‾1} tensile twinning modes. The two tensile deformation twinning types have very different morphologies in equiaxed fine grained Ti–6Al–4V. {112‾1} deformation twins span multiple grain boundaries and {101‾2} deformation twins reorient entire grains to a twinned orientation. This observation provides evidence for whole grain twinning of equiaxed fine grained Ti–6Al–4V by {101‾2} twinning. Grain boundary interactions between various deformation twinning types and alpha phase grain boundaries in commercial purity titanium and Ti–6Al–4V are reported and analysed. In commercial purity titanium {101‾2} as well as other deformation twinning types were observed interacting across alpha phase boundaries and higher angle alpha phase grain boundaries. The analyses of the manufacturing processes of Ti–6Al–4V highlight the very different dislocation and deformation twinning structures in surfaces processed by these techniques. A notable feature of material processed by laser shock peening is the almost complete absence of deformation twinning, contrasting with the frequent observation of extensive deformation twinning observed in the material processed by metallic shot peening and deep cold rolling. Therefore, the findings suggest that there is a strain rate limit above which deformation twinning is suppressed. The implications of this research are that a better understanding of the conditions that that favour certain deformation twinning types or propagation behaviours will enable more accurate plasticity modelling and better alloy design. This is important for the design and the manufacturing of titanium components and the high strain rate deformation to which titanium components in aerospace gas turbines can be subjected because of bird strike, foreign object debris ingestion or fan blade failures.

Este trabalho consiste no estudo das propriedades mecânicas de tração e impacto do aço Hadfield refinado com Hf em relação ao aço Hadfield sem refino. Foram realizadas simulações no software Thermo-Calc para caracterizar o caminho de solidificação e a evolução microestrutural do aço Hadfield (composição química de 13% de Mn, 1,2% de C e 0,65% de Si). Foram fundidos os corpos de prova de aço Hadfield sem refino e refinado pela adição de Hf, ambos com a composição química de acordo com a norma ASTM A128 - grau B2. Os corpos de prova foram submetidos ao tratamento térmico de solubilização à temperatura de 1120oC por 10 horas. A caracterização macroestrutural mostrou que o aço Hadfield com adição de Hf apresenta tamanho do grão austenítico cinco vezes menor (600 µm) do que o aço Hadfield sem refino (de 3000 µm para 600 µm), sendo que este resultado foi confirmado pela técnica de EBSD (Electron backscatter diffraction). Os resultados do ensaio de tração dos corpos de prova para as duas condições mostraram que as propriedades de limite de escoamento (6%), tenacidade (88%), resistência à tração (37%), e do coeficiente de encruamento (30%) do aço Hadfield refinado aumentaram em relação ao aço Hadfield sem refino. A energia absorvida no impacto aumentou de 156 J/cm2 para 179 J/cm2 com o refino do tamanho de grão austenítico. A lei de Hall-Petch foi utilizada para explicar o efeito do refino de grão no limite de escoamento, mas não pode ser usada para explicar o aumento na resistência a tração, tenacidade, e as mudanças no coeficiente de encruamento. A caracterização microestrutural das amostras rompidas em tração e impacto mostrou que a fração de maclas aumentou em 46% (em tração) e 45% (no impacto) para o aço Hadfield refinado em comparação com o aço Hadfield sem refino. Os resultados da caracterização microestrutural dos corpos de prova rompidos no ensaio de tração e impacto indicam que o mecanismo de deformação plástica por maclação foi mais atuante com o refino do grão austenítico. / The tensile and impact properties of Hf-refined Hadfield steel were compared to the properties of non-refined Hadfield steel. Simulations in Thermo-Calc software were made in order to study the solidification and microstructural evolution of a Hadfield steel (13% Mn, 1.2% C and 0.65% Si). Samples of non-refined and refined Hadfield steel (with addition of 0.1% of H), both with chemical composition as described in ASTM A128- grade B2, were cast and subjected to a solution heat treatment at 1100oC for 10 hours, followed by water quenching. Macrostructural characterization showed that the refined Hadfield steel featured an austenitic grain size equal to 600 ?m, five times smaller than the grain size of the non-refined Hadfield steel (3000 µm). These results were confirmed by EBSD (Electron backscatter diffraction) analysis. The tensile test results showed an increase in the values of the yield stress (6%), the fracture toughness (88%), the tensile strength (37%) and the strain hardening coefficient (30%) with the reduction on the austenitic grain size from 3000 µm to 600 µm. Additionally, the value of the absorbed energy of the impact test was improved from 156 J/cm2 to 179J/cm2 with reduction on the grain size. The Hall-Petch law was used to explain the small increase of 8% in the value of the yield stress with the grain refinement, but this law could not be used to explain the increase in the values of the fracture toughness, the tensile strength and the strain hardening coefficient. The microstructural characterization of the fractured test-pieces after tensile and impact testing showed that the values of the fraction of mechanical twins (definer) in the plastically deformed microstructure near the fracture surfaces of the refined condition increased by 45% when compared to the non-refined condition. These results indicated that the austenitic grain refinement of the Hadfield steel changed the plastic deformation mechanism, favoring the activation of the plastic deformation by twinning mechanism and, therefore, increasing the values of the fracture toughness (~88%), the ultimate tensile strength (~30%), the strain-hardening coefficient (~30%) and the absorbed energy during Charpy-test (~15%).

Este trabalho consiste no estudo das propriedades mecânicas de tração e impacto do aço Hadfield refinado com Hf em relação ao aço Hadfield sem refino. Foram realizadas simulações no software Thermo-Calc para caracterizar o caminho de solidificação e a evolução microestrutural do aço Hadfield (composição química de 13% de Mn, 1,2% de C e 0,65% de Si). Foram fundidos os corpos de prova de aço Hadfield sem refino e refinado pela adição de Hf, ambos com a composição química de acordo com a norma ASTM A128 - grau B2. Os corpos de prova foram submetidos ao tratamento térmico de solubilização à temperatura de 1120oC por 10 horas. A caracterização macroestrutural mostrou que o aço Hadfield com adição de Hf apresenta tamanho do grão austenítico cinco vezes menor (600 µm) do que o aço Hadfield sem refino (de 3000 µm para 600 µm), sendo que este resultado foi confirmado pela técnica de EBSD (Electron backscatter diffraction). Os resultados do ensaio de tração dos corpos de prova para as duas condições mostraram que as propriedades de limite de escoamento (6%), tenacidade (88%), resistência à tração (37%), e do coeficiente de encruamento (30%) do aço Hadfield refinado aumentaram em relação ao aço Hadfield sem refino. A energia absorvida no impacto aumentou de 156 J/cm2 para 179 J/cm2 com o refino do tamanho de grão austenítico. A lei de Hall-Petch foi utilizada para explicar o efeito do refino de grão no limite de escoamento, mas não pode ser usada para explicar o aumento na resistência a tração, tenacidade, e as mudanças no coeficiente de encruamento. A caracterização microestrutural das amostras rompidas em tração e impacto mostrou que a fração de maclas aumentou em 46% (em tração) e 45% (no impacto) para o aço Hadfield refinado em comparação com o aço Hadfield sem refino. Os resultados da caracterização microestrutural dos corpos de prova rompidos no ensaio de tração e impacto indicam que o mecanismo de deformação plástica por maclação foi mais atuante com o refino do grão austenítico. / The tensile and impact properties of Hf-refined Hadfield steel were compared to the properties of non-refined Hadfield steel. Simulations in Thermo-Calc software were made in order to study the solidification and microstructural evolution of a Hadfield steel (13% Mn, 1.2% C and 0.65% Si). Samples of non-refined and refined Hadfield steel (with addition of 0.1% of H), both with chemical composition as described in ASTM A128- grade B2, were cast and subjected to a solution heat treatment at 1100oC for 10 hours, followed by water quenching. Macrostructural characterization showed that the refined Hadfield steel featured an austenitic grain size equal to 600 ?m, five times smaller than the grain size of the non-refined Hadfield steel (3000 µm). These results were confirmed by EBSD (Electron backscatter diffraction) analysis. The tensile test results showed an increase in the values of the yield stress (6%), the fracture toughness (88%), the tensile strength (37%) and the strain hardening coefficient (30%) with the reduction on the austenitic grain size from 3000 µm to 600 µm. Additionally, the value of the absorbed energy of the impact test was improved from 156 J/cm2 to 179J/cm2 with reduction on the grain size. The Hall-Petch law was used to explain the small increase of 8% in the value of the yield stress with the grain refinement, but this law could not be used to explain the increase in the values of the fracture toughness, the tensile strength and the strain hardening coefficient. The microstructural characterization of the fractured test-pieces after tensile and impact testing showed that the values of the fraction of mechanical twins (definer) in the plastically deformed microstructure near the fracture surfaces of the refined condition increased by 45% when compared to the non-refined condition. These results indicated that the austenitic grain refinement of the Hadfield steel changed the plastic deformation mechanism, favoring the activation of the plastic deformation by twinning mechanism and, therefore, increasing the values of the fracture toughness (~88%), the ultimate tensile strength (~30%), the strain-hardening coefficient (~30%) and the absorbed energy during Charpy-test (~15%).