NiTi components are commonly subjected to thermo-mechanical heat treatments during production and fabrication. This study investigates the effects of applied strain of 0-10% and heat treatments of 300-600ºC for times of 2-30 minutes during shape-setting of Ti–50.8 at% Ni wire with a nominal diameter of 0.495 mm and an initial transition temperature, Af, of 12ºC. Strain was applied prior to heat treatments by coiling NiTi wire, essentially producing coiled springs, around different diameter steel mandrels to obtain different strain levels. The samples of NiTi wire under applied strain were heat treated in a salt bath, followed by a rapid quench. Transformation temperatures and mechanical properties were characterized using the differential scanning calorimeter and tensile tests. Changes in the Af, UTS, and elastic modulus due to ageing processes and applied strain were observed. Following theory, precipitation rates of Ni-rich phases generally increased with increased temperature (up to a certain point), time and applied strain levels. Reaction rates to achieve a particular Af might be faster than expected if the sample is under strain during the shape-setting process. Due to precipitation strengthening, an increase in UTS with increased heat treatment time was observed between 300-450°C; annealing processes dominate at higher temperatures, resulting in a decrease in UTS above 500°C. A decrease in UTS with increasing level of applied strain was observed. Trends in elastic modulus were highly inconsistent in this study. As shown by this study, applied strain in NiTi during heat treatment affects the Af and mechanical properties.

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In recent years a strong interest has been expressed to produce lighter structures.One possible solution to reduce the weight is to utilize high strength steels and use welding as the joining method. Many components experience fatigue loadingduring all or part of their life time and welded connections are often the prime location of fatigue failure. This becomes more critical in welded high strength steels as fatigue strength of welds does not increase by increasing the steel strength. A possible solution to overcome this issue is to use fatigue improvement methods.The main objectives of this project are, therefore, to increase understanding of the factors that control fatigue life and to investigate how the fatigue strength improvement methods; high frequency mechanical impact (HFMI) treatment and use of Low Transformation Temperature (LTT) consumables will affect fatigue properties of welds in high strength steels. In this regard, Gas Metal Arc Welding(GMAW) was used to produce butt and fillet welds using LTT or conventional fillers in steels with yield strengths ranging from 650-1021 MPa and T-joint weldsin a steel with 1300 MPa yield strength. The effect of HFMI on fatigue strength of the welds in 1300 MPa yield strength steels was also investigated. Butt and fillet welds in 650-1021 MPa steels were fatigue tested under constant amplitude tensile loading with a stress ratio of 0.1 while T-joints were fatigue tested under constant amplitude fully reversed bending load with a stress ratio of -1. The nominal stress approach was used for fatigue strength evaluation of butt and fillet welds whereas the effective notch stress approach was used in case of T-joints. Relative effectsof the main parameters such as residual stress and weld toe geometry influencing fatigue strength of welds were evaluated. Residual stresses were measured using X-ray diffraction for as-welded and HFMI treated welds. Neutron diffraction was additionally used to investigate the near surface residual stress distribution in 1300 MPa LTT welds.Results showed that use of LTT consumables increased fatigue strength of welds in steels with yield strengths ranging from 650-1021 MPa. For butt welds, the vii characteristic fatigue strength (FAT) of LTT welds at 2 million cycles was up to46% higher when compared to corresponding welds made with conventional fillermaterials. In fillet welds, a maximum improvement of 132% was achieved when using LTT wires. The increase in fatigue strength was attributed to the lower tensile residual stresses or even compressive stresses produced close to the weldtoe in LTT welds. Weld metals with martensite transformation start temperatures around 200 °C produced the highest fatigue strength. In 1300 MPa yield strength steel, similar FAT of 287 MPa was observed for LTT welds and 306 MPa for conventional welds, both much higher than the IIW FATvalue of 225 MPa. The relative transformation temperatures of the base and weldmetals, specimen geometry and loading type are possible reasons why the fatigue strength was not improved by use of LTT wires. Neutron diffraction showed that the LTT consumable was capable of inducing near surface compressive residual stresses in all directions at the weld toe. It was additionally found that there arevery steep stress gradients both transverse to the weld toe line and in the depth direction, at the weld toe. Due to difficulties to accurately measure residual stresses locally at the weld toe most often in the literature and recommendations residual stresses a few millimetre away from the weld toe are related to fatigue properties. However, this research shows that caution must be used when relating these to fatigue strength, in particular for LTT welds, as stress in the base materiala few millimetre from the weld toe can be very different from the stress locally at the weld toe.HFMI increased the mean fatigue strength of conventional welds in 1300 MPa steels about 26% and of LTT welds by 13%. It increased the weld toe radius slightly but produced a more uniform geometry along the treated weld toes. Large compressive residual stresses, especially in the longitudinal direction, were introduced adjacent to the weld toe for both LTT and conventional treated welds. It was concluded that the increase in fatigue strength by HFMI treatment is due to the combined effect of weld toe geometry modification, increase in surface hardness and introduction of compressive residual stresses in the treated region.It was concluded that the residual stress has a relatively larger influence than the weld toe geometry on fatigue strength of welds. This is based on the observation that a moderate decrease in residual stress of about 15% at the 300 MPa stress level had the same effect on fatigue strength as increasing the weld toe radius by approximately 85% from 1.4 mm to 2.6 mm, in fillet welds. Also, a higher fatigue strength was observed for HFMI treated conventional welds compared to as welded samples having similar weld toe radii but with different residual stresses.

A proposta da modificação química da superliga MAR-M247 através da substituição do Ta pelo Nb (em átomos) foi baseada nas seguintes informações: (1) O Nb desempenha funções muita parecidas com as do Ta nas superligas à base de Ni, como endurecedor via solução sólida da fase ? e elemento formador de fases secundárias (?? e carbonetos); (2) O Brasil tem as maiores reservas de Nb do mundo e (3) O Nb já é adicionado em diversas classes de superligas à base de Ni - fundidas convencionalmente e solidificadas direcionalmente e monocristalinas. Neste trabalho o objetivo principal foi de avaliar a viabilidade da substituição do Ta pelo Nb na superliga à base de Ni MAR-M247. As amostras da MAR-M247 e da liga modificada - MAR-M247[Nb] utilizadas na caracterização microestrutural foram obtidas por solidificação direcional no forno a vácuo do tipo forno Bridgman (Lab. de Solidificação/FEM-UNICAMP) nas seguintes condições de processamento: v = 5, 10 e 18 cm/h e G = 80°C/cm. As simulações de cálculo termodinâmico utilizando o programa Thermo-Calc foram realizadas com o objetivo de se avaliar se as temperaturas de transformação mudariam com a substituição do Ta pelo Nb. Para avaliação das propriedades mecânicas em alta temperatura e a estabilidade estrutural da superliga MAR-M247[Nb] foram realizados ensaios de fluência a 750 e 850 °C nas tensões de 840, 780 e 440 MPa. A estabilidade microestrutural da MAR-M247[Nb] foi testada por meio de ensaios de oxidação isotérmica a 1000 °C no intervalo de tempo de 30 minutos a 100 h. A substituição do Ta pelo Nb promoveu mudanças significativas principalmente nas temperaturas de formação do eutético ?/??, solvus - ?? e de fusão incipiente. As microestruturas das ligas após os experimentos de solidificação direcional a v = 5, 10 e 18 cm/h eram constituídas por dendritas da fase gama - ? e precipitados coerentes da fase gama linha - ?? (morfologia cuboidal). Na região interdendrítica da MAR-M247 e MAR-M247[Nb] solidificadas a v = 5 e 10 cm/h foram encontrados os eutéticos ?/?? e ?/Ni5(Hf,Zr). Na v = 18 cm/h a região interdendrítica era constituída apenas do eutético ?/??. A exposição a 1250 °C por 15 e 30 dias promoveu a decomposição total e a re-precipitação de carbonetos do tipo MC. No entanto, devido à contaminação por oxigênio e nitrogênio durante os tratamento térmicos, não foi atingido o equilíbrio termodinâmico em decorrência de mudanças das composições dos carbonetos MC. Nos ensaios de fluência a 750 °C, os tempos de ruptura foram de 49 h para MAR-M247 e de 39,4 h para MAR-M247[Nb] apesar dos elevados valores das tensões terem sido superestimados. A 850 °C o tempo de ruptura da MAR-M247[Nb] (trup = 359 horas) foi reduzido em 32 % em relação ao valor observado para MAR-M247 (trup = 476 horas). Os resultados dos ensaios de oxidação a 1000 °C da superliga MAR-M247[Nb] mostraram que o período transiente foi de 20 h com ganho de massa expressivo. A partir de 50 h o efeito do descolamento das camadas oxidadas durante o resfriamento das amostras foi significativo e promoveu uma variação de massa importante no intervalo de tempo de 50 a 100 h. Ensaios de oxidação em tempos mais longo deverão ser feitos para determinação da estrutura de formação das camadas e seus respectivos constituintes. / The chemistry modification in the Ni-based superalloy MAR-M247 through the replacing all Ta by Nb was based on in these statements: (1) Nb does the same function in Ni-based superalloys as Ta does, solid solution strenghtening and ?? e carbides element formers, (2) Brazil has the major ores of Nb in the world and (3) Nb has been added in all classes of Ni superalloy conventional casting, columnar and single crystal processed by directional solidification. In this study the main focus was to evaluate the feasibility of replacing Ta by Nb in the Ni - based superalloy MAR-M247. The samples of MAR-M247 and the Nb modified MAR-M247[Nb] were produced by directional solidification in a Bridgman vacuum furnace at the Solidification Research Lab/FEM - UNICAMP) in the following processing conditions: v = 5, 10 and 18 cm/h and G = 80 °C/cm. The thermodynamic simulations using Thermo-Calc program were performed to evaluate whether or not the transformation temperatures would change with the replacing of Ta by Nb. For the evaluation of mechanical properties at high temperature were performed creep rupture tests at 750 and 850 °C under the stress values of 840, 780 and 440 MPa. The isotermal oxidation tests at 1000 °C were done during the time interval of 30 min to 100 h. The replacing of Ta by Nb promoted some changes in eutectic-?/??, ??-solvus and incipient melting temperatures. After the directional solidification experiments at the v = 5, 10 and 18 cm/h the microstructural characterization has shown that for all condition the microstructures were composed by dendrites - ? and ?? - cuboidal precipitates in it. In the interdendritic region was observe the ?/?? and ?/Ni5(Hf,Zr) eutectics for v = 5 and 10 cm/h and only the ?/?? eutectics for v = 18 cm/h. The exposure at 1250 °C for the extended times promoted the formation of fine MC carbides but the equilibrium compositions have not been achieved due to the oxygen and nitrogen contamination. In the creep rupture tests at 750 °C the MAR-M247[Nb] have shown more shorter lifetime than the MAR-M247 even with overestimated tensile stress. At 850 °C the lifetime for MAR-M247[Nb] (trup = 359 h) was reduced by 32 % compared to the MAR-M247 (trup = 476 h). It was discussed that the changes in the composition of the ? phase induced Ta by Nb replacing which would led to the weakness of matrix in the MAR-M247[Nb]. The samples were oxidized at 1000 °C showed 20 h to the transient period and significant weight gain in that time. However at the extended period the weight gain had changed significantly and was precluded to predict the structure formation of oxides layer properly.

A proposta da modificação química da superliga MAR-M247 através da substituição do Ta pelo Nb (em átomos) foi baseada nas seguintes informações: (1) O Nb desempenha funções muita parecidas com as do Ta nas superligas à base de Ni, como endurecedor via solução sólida da fase ? e elemento formador de fases secundárias (?? e carbonetos); (2) O Brasil tem as maiores reservas de Nb do mundo e (3) O Nb já é adicionado em diversas classes de superligas à base de Ni - fundidas convencionalmente e solidificadas direcionalmente e monocristalinas. Neste trabalho o objetivo principal foi de avaliar a viabilidade da substituição do Ta pelo Nb na superliga à base de Ni MAR-M247. As amostras da MAR-M247 e da liga modificada - MAR-M247[Nb] utilizadas na caracterização microestrutural foram obtidas por solidificação direcional no forno a vácuo do tipo forno Bridgman (Lab. de Solidificação/FEM-UNICAMP) nas seguintes condições de processamento: v = 5, 10 e 18 cm/h e G = 80°C/cm. As simulações de cálculo termodinâmico utilizando o programa Thermo-Calc foram realizadas com o objetivo de se avaliar se as temperaturas de transformação mudariam com a substituição do Ta pelo Nb. Para avaliação das propriedades mecânicas em alta temperatura e a estabilidade estrutural da superliga MAR-M247[Nb] foram realizados ensaios de fluência a 750 e 850 °C nas tensões de 840, 780 e 440 MPa. A estabilidade microestrutural da MAR-M247[Nb] foi testada por meio de ensaios de oxidação isotérmica a 1000 °C no intervalo de tempo de 30 minutos a 100 h. A substituição do Ta pelo Nb promoveu mudanças significativas principalmente nas temperaturas de formação do eutético ?/??, solvus - ?? e de fusão incipiente. As microestruturas das ligas após os experimentos de solidificação direcional a v = 5, 10 e 18 cm/h eram constituídas por dendritas da fase gama - ? e precipitados coerentes da fase gama linha - ?? (morfologia cuboidal). Na região interdendrítica da MAR-M247 e MAR-M247[Nb] solidificadas a v = 5 e 10 cm/h foram encontrados os eutéticos ?/?? e ?/Ni5(Hf,Zr). Na v = 18 cm/h a região interdendrítica era constituída apenas do eutético ?/??. A exposição a 1250 °C por 15 e 30 dias promoveu a decomposição total e a re-precipitação de carbonetos do tipo MC. No entanto, devido à contaminação por oxigênio e nitrogênio durante os tratamento térmicos, não foi atingido o equilíbrio termodinâmico em decorrência de mudanças das composições dos carbonetos MC. Nos ensaios de fluência a 750 °C, os tempos de ruptura foram de 49 h para MAR-M247 e de 39,4 h para MAR-M247[Nb] apesar dos elevados valores das tensões terem sido superestimados. A 850 °C o tempo de ruptura da MAR-M247[Nb] (trup = 359 horas) foi reduzido em 32 % em relação ao valor observado para MAR-M247 (trup = 476 horas). Os resultados dos ensaios de oxidação a 1000 °C da superliga MAR-M247[Nb] mostraram que o período transiente foi de 20 h com ganho de massa expressivo. A partir de 50 h o efeito do descolamento das camadas oxidadas durante o resfriamento das amostras foi significativo e promoveu uma variação de massa importante no intervalo de tempo de 50 a 100 h. Ensaios de oxidação em tempos mais longo deverão ser feitos para determinação da estrutura de formação das camadas e seus respectivos constituintes. / The chemistry modification in the Ni-based superalloy MAR-M247 through the replacing all Ta by Nb was based on in these statements: (1) Nb does the same function in Ni-based superalloys as Ta does, solid solution strenghtening and ?? e carbides element formers, (2) Brazil has the major ores of Nb in the world and (3) Nb has been added in all classes of Ni superalloy conventional casting, columnar and single crystal processed by directional solidification. In this study the main focus was to evaluate the feasibility of replacing Ta by Nb in the Ni - based superalloy MAR-M247. The samples of MAR-M247 and the Nb modified MAR-M247[Nb] were produced by directional solidification in a Bridgman vacuum furnace at the Solidification Research Lab/FEM - UNICAMP) in the following processing conditions: v = 5, 10 and 18 cm/h and G = 80 °C/cm. The thermodynamic simulations using Thermo-Calc program were performed to evaluate whether or not the transformation temperatures would change with the replacing of Ta by Nb. For the evaluation of mechanical properties at high temperature were performed creep rupture tests at 750 and 850 °C under the stress values of 840, 780 and 440 MPa. The isotermal oxidation tests at 1000 °C were done during the time interval of 30 min to 100 h. The replacing of Ta by Nb promoted some changes in eutectic-?/??, ??-solvus and incipient melting temperatures. After the directional solidification experiments at the v = 5, 10 and 18 cm/h the microstructural characterization has shown that for all condition the microstructures were composed by dendrites - ? and ?? - cuboidal precipitates in it. In the interdendritic region was observe the ?/?? and ?/Ni5(Hf,Zr) eutectics for v = 5 and 10 cm/h and only the ?/?? eutectics for v = 18 cm/h. The exposure at 1250 °C for the extended times promoted the formation of fine MC carbides but the equilibrium compositions have not been achieved due to the oxygen and nitrogen contamination. In the creep rupture tests at 750 °C the MAR-M247[Nb] have shown more shorter lifetime than the MAR-M247 even with overestimated tensile stress. At 850 °C the lifetime for MAR-M247[Nb] (trup = 359 h) was reduced by 32 % compared to the MAR-M247 (trup = 476 h). It was discussed that the changes in the composition of the ? phase induced Ta by Nb replacing which would led to the weakness of matrix in the MAR-M247[Nb]. The samples were oxidized at 1000 °C showed 20 h to the transient period and significant weight gain in that time. However at the extended period the weight gain had changed significantly and was precluded to predict the structure formation of oxides layer properly.