Os colares das sondas de prospecção petrolíferas são fabricadas de aço inoxidável austenítico devido as suas características eletromagnéticas e de corrosão. Normalmente, a temperatura de serviço é de aproximadamente 300ºC, meio aquoso e a sonda é submetida a carregamentos cíclicos. Várias foram as tentativas de desenvolvimento de um aço que atendesse as necessidades de serviço destes colares. Neste trabalho foram determinadas as propriedades mecânicas de tração e de fadiga de baixo ciclo de um aço inoxidável austenítico do sistema Fe-Mn-Cr-N, quando ensaiado mecanicamente nas temperaturas ambiente e à 300ºC. Foi observado que os valores dos limites de escoamento e de resistência e o alongamento diminuem significativamente quando a temperatura é elevada para 300ºC. Como conseqüência destas alterações, ocorreu uma diminuição da vida em fadiga. A comparação entre as curvas tensão-deformação monotônica e cíclica mostrou que este material, ensaiado à 300ºC e nas amplitudes de deformações estudadas, apresenta amolecimento cíclico. A expressão encontrada para a relação deformação-vida é dada por &#916&#949t/2=0,0054 (2Nf)-0,064 + 0,438 (2Nf)-0,595 com ponto de transição em 2Nt = 9,5 x 103. Quanto aos métodos estimativos das propriedades mecânicas de fadiga, obtidos a partir das propriedades mecânicas de tração, foi verificado que o Método da Inclinação Universal Modificado se aproxima mais da curva experimental obtida neste trabalho. A análise fratográfica mostrou a presença de estrias no estágio II de propagação de trinca. / In this work the monotonic and low cycle fatigue mechanical properties of an Cr-Mn-N austenitic stainless steel, used to produce drill collars used for deep drilling in offshore industry, were evaluated. The low cycle fatigue testing was carried out according to the ASTM E606 standard, under strain control and R = - 1, at temperature of 300°C, which is the temperature that the drill collar reaches in service. It was observed that the yield and the ultimate tensile strength and the elongation decreased sharply with increasing temperature. As a consequence, in both high and low cycle regions, the fatigue life decreased with increasing temperature. The comparison between the stress - strain monotonic and cyclic curves, showed that this material exhibited cyclic softening for the applied strain amplitudes. The correlation between strain and number of cycles to failure was can be given by &#916&#949t/2 = 0,0054 (2Nf)-0,064 + 0,438 (2Nf)-0,595 with transition in 2Nt = 9,5x103 reverses. The experimental results were compared with some models used to predict the fatigue life based on the tensile monotonic properties. The Modified Universal Shopes a better fitting with the experimental data. The fractographic analysis showed the presence of stage II striations.

Neste trabalho foram determinadas as propriedades monotônicas e de fadiga de baixo-ciclo em chapa fina de um aço livre de intersticiais (aço IF) com adição de titânio, utilizado na indústria automobilística. Os ensaios de fadiga foram realizados sob controle de deformação com R&#949 = -1 e com o auxílio de um sistema de alinhamento de garras. O material apresenta diferentes comportamentos de fadiga nas direções transversal e longitudinal (em relação à direção de laminação). Comparação entre a curva tensão-deformação monotônica e a curva tensão-deformação cíclica mostra que os corpos de prova transversais têm endurecimento cíclico para as amplitudes de deformação estudadas. A relação deformação-vida obtida para a direção transversal é dada por &#916&#949t/2 = 0,0186(2Nf)-0,262 + 0,235(2Nf)-0,476 com ponto de transição em 2Nt = 1,4x105 reversos, não sendo possível obtê-la para a direção longitudinal devido a problemas de flambagem. Vários métodos estimativos de propriedades de fadiga a partir de propriedades monotônicas foram comparados aos resultados experimentais. Os métodos da correlação quatro pontos e inclinação universal modificada apresentando boa correlação para a região de baixo-ciclo. Análise fratográfica por microscopia eletrônica de varredura mostrou a presença de estrias de propagação do estágio II, evidenciando a alta dutilidade do material. / In the present work, the monotonic and low cycle fatigue properties of thin sheet of interstitial free steel containing titanium additions, used in the automotive industry, were investigated. Fatigue tests were conducted under deformation control (R&#949 = -1) using a grip alignment fixture. The material exhibits different fatigue behavior for the transverse and longitudinal directions (in relation to the rolling direction). A comparison between the monotonic stress-strain curve and the cyclic stress-strain curve in the transverse direction showed that the material exhibits cyclic hardening in all strain amplitudes tested. The strain-life relationship obtained for transverse direction is given by &#916&#949t/2 = 0,0186(2Nf)-0,262 + 0,235(2Nf)-0,476 with transition point in 2Nt = 1,4x105 reverses; buckling of longitudinal specimens made impossible to obtain such relationship. Several prediction methods of fatigue properties from monotonic properties were compared to the experimental results. The Four Point Correlation and the Modified Universal Slopes Methods showed a good correlation for the low cycle region. Fractographic analysis through Scanning Eletronic Microscopy showed the presence of Stage II striations, giving support to the high ductility of the material.

Os colares das sondas de prospecção petrolíferas são fabricadas de aço inoxidável austenítico devido as suas características eletromagnéticas e de corrosão. Normalmente, a temperatura de serviço é de aproximadamente 300ºC, meio aquoso e a sonda é submetida a carregamentos cíclicos. Várias foram as tentativas de desenvolvimento de um aço que atendesse as necessidades de serviço destes colares. Neste trabalho foram determinadas as propriedades mecânicas de tração e de fadiga de baixo ciclo de um aço inoxidável austenítico do sistema Fe-Mn-Cr-N, quando ensaiado mecanicamente nas temperaturas ambiente e à 300ºC. Foi observado que os valores dos limites de escoamento e de resistência e o alongamento diminuem significativamente quando a temperatura é elevada para 300ºC. Como conseqüência destas alterações, ocorreu uma diminuição da vida em fadiga. A comparação entre as curvas tensão-deformação monotônica e cíclica mostrou que este material, ensaiado à 300ºC e nas amplitudes de deformações estudadas, apresenta amolecimento cíclico. A expressão encontrada para a relação deformação-vida é dada por &#916&#949t/2=0,0054 (2Nf)-0,064 + 0,438 (2Nf)-0,595 com ponto de transição em 2Nt = 9,5 x 103. Quanto aos métodos estimativos das propriedades mecânicas de fadiga, obtidos a partir das propriedades mecânicas de tração, foi verificado que o Método da Inclinação Universal Modificado se aproxima mais da curva experimental obtida neste trabalho. A análise fratográfica mostrou a presença de estrias no estágio II de propagação de trinca. / In this work the monotonic and low cycle fatigue mechanical properties of an Cr-Mn-N austenitic stainless steel, used to produce drill collars used for deep drilling in offshore industry, were evaluated. The low cycle fatigue testing was carried out according to the ASTM E606 standard, under strain control and R = - 1, at temperature of 300°C, which is the temperature that the drill collar reaches in service. It was observed that the yield and the ultimate tensile strength and the elongation decreased sharply with increasing temperature. As a consequence, in both high and low cycle regions, the fatigue life decreased with increasing temperature. The comparison between the stress - strain monotonic and cyclic curves, showed that this material exhibited cyclic softening for the applied strain amplitudes. The correlation between strain and number of cycles to failure was can be given by &#916&#949t/2 = 0,0054 (2Nf)-0,064 + 0,438 (2Nf)-0,595 with transition in 2Nt = 9,5x103 reverses. The experimental results were compared with some models used to predict the fatigue life based on the tensile monotonic properties. The Modified Universal Shopes a better fitting with the experimental data. The fractographic analysis showed the presence of stage II striations.

This master thesis deals with steam turbine blade attachment. Main goal is to perform strength analysis of the given geometry under static and cyclic loads by FEM and software ANSYS. Every particular model is described separately with mentioning of the problems which had to be solved. To create model of material, the tensile tests has been performed and results has been evaluate. There were planned and performed the low cycle fatigue tests to create a model of ultimate states which is used to evaluate the fatigue life of the attachment. Results of the nonlinear FEM analysis is discussed and some improvements of the geometry has been proposed to achieve better state of stress. Finally, the plan of future work has been proposed.

This master’s thesis is dealing with low-fatigue behavior of magnesium alloy AZ61, prepared via squeeze casting method. The main aim of this work was to obtain the basic mechanical properties as well as the low cycle fatigue data. Additional metallographical evaluation of microstructure and fractographical analysis after fatigue tests was made.

This thesis deals with the low cycle fatigue nickel-based superalloy IN713LC with applied TBC barrier at high temperature. The theoretical part is divided into four sections. The first one focuses on description of fatigue damage. The second one provides the basic characteristics of nickel-based superalloys. The third section describes the use of the surface layers - diffusion layers and thermal barriers and the fourth section deals with the influence of these layers on fatigue properties. Experimental part is focused on the evaluation of low cycle fatigue tests and on the explanation of the mechanisms of initiation and propagation of fatigue cracks. For the experimental part, fatigue samples were prepared by vacuum precision investment casting. TBC barrier was applied by atmospheric plasma spraying and consists of two sublayers - the lower metallic bond coating type CoNiCrAlY and top ceramic coating type YSZ. Low cycle fatigue tests were conducted under strain control at controlled temperature of 900 ° C. Fractographical analysis of fracture surfaces was carried out by using light and electron microscopy. Effect of applied barrier to fatigue life was determined - the parameters of Manson-Coffin and Basquin curve. A cyclic stress-strain curve was also obtained. The curves softening / hardening and number of transit cycles were determined. The obtained parameters and values from fatigue tests were compared with available data from fatigue tests of superalloy IN713LC without the layer, as applied AlSi type diffusion layer, at high temperatures. The initiation site on the fracture surfaces was determined within the fractographic evaluation and the influence of the layer on the initiation and propagation of fatigue cracks was discussed. A helpful tool was the assessment of longitudinal sections using scanning electron microscopy.

The present diploma thesis is focused on the effect of AlCr layer on the low cycle fatigue behaviour of cast polycrystalline superalloy IN713LC at 800°C. Protective layer is made by chemical vapour deposition followed by heat treatment. Fatigue tests were conducted in strain control mode with constant total strain amplitude and strain rate. The fatigue behaviour is assessed by cyclic hardening/softening curves, cyclic stress-strain curves, Manson-Coffin curves and Basquin curves. Microstructure was observed in as-received state and also after cyclic loading by means of optical microscopy and SEM.

Conjugate heat transfer analysis has been carried out on an 89kN thrust chamber in order to evaluate whether combined discrete film cooling and regenerative cooling in a rocket nozzle is feasible. Several cooling configurations were tested against a baseline design of regenerative cooling only. New designs include combined cooling channels with one row of discrete film cooling holes near the throat of the nozzle, and turbulated cooling channels combined with a row of discrete film cooling holes. Blowing ratio and channel mass flow rate were both varied for each design. The effectiveness of each configuration was measured via the maximum hot gas-side nozzle wall temperature, which can be correlated to number of cycles to failure. A target maximum temperature of 613K was chosen. Combined film and regenerative cooling, when compared to the baseline regenerative cooling, reduced the hot gas side wall temperature from 667K to 638K. After adding turbulators to the cooling channels, combined film and regenerative cooling reduced the temperature to 592K. Analysis shows that combined regenerative and film cooling is feasible with significant consequences, however further improvements are possible with the use of turbulators in the regenerative cooling channels.

The introduction of gas-driven Otto engine and the corresponding usage of bio-fuels in heavy-duty engines will render the exhaust atmosphere more corrosive and bring a higher working temperature to exhaust manifolds. The current service material, a ferritic ductile cast iron called SiMo51, will soon meet its upper temperature limit set by the ferrite-austenite transformation at 860ºC. Three alternative materials, as well as SiMo51 serving as reference, are investigated in the present thesis emphasizing on high-temperature corrosion fatigue.  The first aim of this study is to obtain material data and give a quantitative ranking of the materials’ performance. Low-cycle fatigue (LCF) tests at 800ºC in a synthetic exhaust gas (5%O2-10%CO2-5%H2O-1ppmSO2-N2 bal.) are conducted to evaluate the materials’ performance in simulated real working scenarios, where high-temperature, corrosive atmosphere and fatigue conditions during testings are similar to the conditions experienced by the exhaust manifolds. To evaluate the individual effect from high-temperature fatigue and isolate the impact from corrosion, the materials are tested under the same settings but in an argon atmosphere. To evaluate the individual effect from high-temperature corrosion and isolate the impact from mechanical deformation, oxidation tests are carried out at 800ºC in the same synthetic exhaust gas. The second aim is to identify and understand different oxidation behavior and failure mechanisms in the materials, realized by considerable characterizations of the tested specimens. From the fatigue tests, it is found that the austenitic stainless steel HK30 has the highest fatigue resistance, followed by the austenitic cast iron Ni-resist D5S, and the ferritic ductile cast irons SiMo1000 and SiMo51, a ranking valid in both atmospheres. In the exhaust atmosphere, for instance, the improvement in fatigue strength at 15,000 cycles relative to SiMo51 are 260%, 194% and 26%, respectively. Different crack initiation and propagation mechanisms are found for the various combinations of materials and atmospheres. In the exhaust atmosphere, for instance, crack initiation is assisted by oxide intrusion in SiMo51 and crack propagation is affected by crack branching in HK30, mechanisms not observed in argon. By comparing the S-N fatigue curves in the two atmospheres, the influence of oxidation on fatigue life is evaluated. The fatigue life of the cast irons are surprisingly found to be higher in the exhaust atmosphere. Several explanations are suggested for this, considering their very different oxidation behaviors.  This study provides accurate test data that can be used to help industry avoid over-dimensioned design. The investigation of the failure mechanisms promotes better understanding of the correlation between microstructure and mechanical properties. Moreover, the combination of fatigue tests in argon, fatigue tests in exhaust and oxidation tests in exhaust, shows how corrosion and fatigue individually and synergistically affect the materials’ performance at high temperature. / <p>QC 20180917</p>

Increasing energy demand leads to two crucial problems for the whole society. One is the economic cost and the other is the pollution of the environment, especially CO2 emissions. Despite efforts to adopt renewable energy sources, fossil fuels will continue to dominate. The temperature and stress are planned to be raised to 700 °C and 35 MPa respectively in the advanced ultra-supercritical (AUSC) power plants to improve the operating efficiency. However, the life of the components is limited by the properties of the materials. The aim of this thesis is to investigate the high temperature properties of materials used for future power plants. This thesis contains two parts. The first part is about developing creep rupture models for austenitic stainless steels. Grain boundary sliding (GBS) models have been proposed that can predict experimental results. Creep cavities are assumed to be generated at intersection of subboundaries with subboundary corners or particles on a sliding grain boundary, the so called double ledge model. For the first time a quantitative prediction of cavity nucleation for different types of commercial austenitic stainless steels has been made. For growth of creep cavities a new model for the interaction between the shape change of cavities and creep deformation has been proposed. In this constrained growth model, the affected zone around the cavities has been calculated with the help of FEM simulation. The new growth model can reproduce experimental cavity growth behavior quantitatively for different kinds of austenitic stainless steels. Based on the cavity nucleation models and the new growth models, the brittle creep rupture of austenitic stainless steels has been determined. By combing the brittle creep rupture with the ductile creep rupture models, the creep rupture strength of austenitic stainless steels has been predicted quantitatively. The accuracy of the creep rupture prediction can be improved significantly with combination of the two models. The second part of the thesis is on the fatigue properties of austenitic stainless steels and nickel based superalloys. Firstly, creep, low cycle fatigue (LCF) and creep-fatigue tests have been conducted for a modified HR3C (25Cr20NiNbN) austenitic stainless steel. The modified HR3C shows good LCF properties, but lower creep and creep-fatigue properties which may due to the low ductility of the material. Secondly, LCF properties of a nickel based superalloy Haynes 282 have been studied. Tests have been performed for a large ingot. The LCF properties of the core and rim positions did not show evident differences. Better LCF properties were observed when compared with two other low γ’ volume fraction nickel based superalloys. Metallography study results demonstrated that the failure mode of the material was transgranular. Both the initiation and growth of the fatigue cracks were transgranular. / <p>QC 20160905</p>