Rails play a significant role in transport of goods and passengers. In Australia railway transport industry contributes 1.6% of GDP with goods and services worth $AUD 8 billion each year which includes $ AUD 0.5 billion per year in exports (Australasian Railway Authority Inc, 2002). Rail track maintenance plays an important role in reliability and safety. The Office for Research and Experiments (ORE) of the Union International des Chemins de Fer (UIC) has noted that maintenance costs vary directly (60-65 per cent) with change in train speed and axle load. It was also found that the increase in these costs with increased speed and axle load was greater when the quality of the track was lower (ORR, 1999). Failures during operation are costly to rail players due to loss of service, property and loss of lives. Maintenance and servicing keep rail tracks in operating, reliable and safe condition. Therefore, technical and economical analysis is needed by rail players to reduce maintenance cost and improve reliability and safety of rail networks. Over the past few years, there have been major advances in terms of increased speed, axle loads, longer trains, along with increased traffic density in corridors. This has led to increased risks in rail operation due to rolling contact fatigue (RCF) and rail wear. The infrastructure providers have less incentive to maintain a given infrastructure standard if its access charges are rigid and rolling stock standard is not achieved. It has been estimated that between 40 to 50 per cent of wagon maintenance costs and 25 per cent of locomotive maintenance costs are related to wheel maintenance (Railway Gazette International, 2003). The economic analysis of Malmbanan indicates that about 50% of the total cost for maintenance and renewal were related to traffic on rails and 50% not related to traffic, such as signaling, electricity and snow-clearance. The results from the analysis have made it possible for the mining company LKAB to start up the 30 Tonnes traffic with new wagons and locomotives on the Malmbanan line in year 2001 (Åhrén et al 2003). The rail infrastructure providers have challenges to maintain infrastructure due to government control on access charges and limited control on rail operations. The aim of the research is to: · Develop a maintenance cost model for optimal rail grinding for various operating conditions; and · Develop integrated rail grinding and lubrication strategies for optimal maintenance decisions. In this research real life data has been collected, new models have been developed and analysed for managerial decisions. Simulation approach is used to look into the impact on various costs such as rail grinding, operating risk, down time, inspection, replacement, and lubrication. The results of the models for costs and the effect of rail grinding and lubrication strategies are provided in this thesis. In this research rail track degradation, rail failures and various factors that influence rail degradation are analysed. An integrated approach for modelling rail track degradation, rail wear, rail grinding and lubrication is developed. Simulation model and cost models for rail grinding are developed and analysed. It has been found through this research that rail grinding at 12 MGT interval is economic decision for enhancing rail life. It was also found that lubrication is most effective compared to stop/start and no lubrication strategies in steep curves. Rail grinding strategies developed in this research have been considered by Swedish National Rail for analysing the effectiveness of their existing policies on grinding intervals. Optimal grinding and lubrication decisions have huge potential for savings in maintenance costs, improving reliability and safety and enhancing rail life.

<p>Rolling contact fatigue (RCF) is the primary mode of failure in tribological contacts like rolling-element bearings (REBs), gears, and cam-follower systems. RCF processes have a crack initiation phase followed by a propagation and coalescence phase, resulting in spalls that lead to catastrophic failure. Crack initiation is a highly localized process that is strongly influenced by the inhomogeneity of the material microstructure. Therefore, a microstructure-sensitive model is required to simulate the damage evolution and failure due to RCF loading. This document presents the development of a microstructure-based finite element (FE) framework for RCF, which accounts for the inhomogeneity of bearing steel microstructure by using an explicit definition of polycrystal topology and material anisotropy. The granular topology of the bearing steel microstructure is described using randomly generated Voronoi tessellations. A cubic elastic material definition with a random spatial orientation is specified for each Voronoi grain to simulate the material anisotropy. The Voronoi grains generated using this approach were used to model the critically stressed microstructural volume in RCF loading. A domain size study was conducted to estimate the minimum number of grains that need to be contained by the critically stressed volume such that the macroscopic material response of the polycrystalline aggregate matches the linear elastic material properties of bearing steel. The estimated critically stressed volume was then embedded into a semi-infinite domain for the FE simulation of RCF line contact loading. The RCF domains developed were then subjected to a moving Hertzian pressure over the surface to simulate a bearing load cycle. A boundary averaging scheme was used to estimate the effective stresses along the grain boundaries of the Voronoi cells. Due to the anisotropy of the polycrystalline material, local stress concentrations occur at the grain boundaries as compared to isotropic models. The resolved grain boundary stresses were used to predict critical locations for RCF crack initiation, which closely match observations from RCF bench test data. Since RCF failures typically exhibit subsurface locations for the first crack initiation, the model uses the critical resolved shear stress (RSS) reversal along the grain boundaries and the corresponding subsurface location of the maxima as the driving parameters for RCF fatigue failures. The parameters from the model were fit into a Weibull distribution to estimate the stochasticity in initiation life. The Weibull predictions corroborate well with experimentally measured RCF life scatter. The framework was then extended using a coupled damage mechanics - cohesive element method (DM-CEM) to individually model the crack initiation and propagation phases in RCF. An explicit definition of the grain boundaries was incorporated using cohesive elements. Damage is initiated at the grain boundaries by degradation of the cohesive elements and the rate of damage/degradation is used to characterize the evolution of fatigue life. The rate of damage was calculated at each grain boundary using a fatigue damage law based on the RSS reversal parameter. The model is able to simulate the crack initiation and the propagation/ coalescence phases in RCF, with distinct life estimates for each phase. This model framework is further extended to investigate the effects of lubrication conditions in RCF by integrating an elastohydrodynamic lubrication (EHL) model to simulate the pressure load with the DM-CEM model. Further improvements to the fatigue life predictions using the DM-CEM model are made by coupling it with a crystal plasticity (CP) based submodel approach to predict the crack initiation life in RCF. CP-based metrics are used to correlate the microplasticity developed under RCF loading with the formation of fatigue micro-cracks and the corresponding initiation life estimations. The resulting final spall patterns and RCF life estimates were found to match well with experimental data available in the open literature.</p> <p><br></p>

O presente trabalho destina-se à discussão sobre o cálculo de vida útil de rolamentos. Mostrando o avanço do processo de cálculo ao longo das décadas até o mais alto grau de desenvolvimento atual. A preocupação do texto é demonstrar de forma simples e objetiva as divergências que existem entre a formulação teórica e a real vida dos rolamentos, no que tange a fadiga de contato. Neste contexto foram realizados testes, em máquina especialmente destinada ao ensaio da fadiga de rolamentos. Variando-se para as duas séries de ensaios, apenas, a temperatura (aproximadamente 85°C e 110°C). Os resultados obtidos indicam que a vida real dos rolamentos apresenta grande divergência se comparada com a vida útil calculada, principalmente, no regime com maior temperatura. Atribui-se a esta disparidade, a ausência de cálculos precisos quanto à correlação da vida útil com o fator l, que é uma forma de se calcular o espaçamento entre as superfícies de contato, e o não emprego do cálculo do fator de carga, na formulação da vida útil de rolamentos. / The present work has the purpose of discussing the life of rolling bearings, describing the evolution of bearing life calculation until its current state of the art. Our focus is to demonstrate, simply and objectively, the inconsistencies occurring between the actual life of rolling bearings and their theoretical fatigue life estimation. For such purpose, tests were developed in a special bearing test rig to assess bearing fatigue. Two test sets were carried out with temperature being the only variation (approximately 85°C and 110°C). Results obtained from these tests suggest that the real life of rolling bearings is indeed very different from calculated bearing life, especially under higher temperature. Such disparity can be attributed to the lack of a precise computation of the relationship between bearing real life and the l factor - which determines the thickness of lubricant separating raceways and balls - as well as to the failure to compute the load factor in bearing life estimation.

Os processos de manufatura, bem como os parâmetros de processamento utilizados produzem diferentes resultados com relação à integridade de uma superfície. Estas alterações se refletem em mudança das propriedades da superfície, as quais podem influenciar o desempenho dos componentes. O presente trabalho estuda o efeito da integridade superficial gerada pelos processos de torneamento e retificação na resistência à fadiga de contato do aço ferramenta AISI H13. A influência do processo de usinagem e dos parâmetros de corte no estado da superfície e subsuperfície, e como estas características afetam o desempenho são determinados. Foram geradas quatro condições diferentes para as superfícies torneadas mediante a combinação de parâmetros de corte. As superfícies retificadas foram produzidas empregando as mesmas condições de retificação, com isso, obteve-se a mesma condição para todos os corpos de prova ensaiados. As características medidas da integridade superficial foram: os parâmetros de rugosidade, tensões residuais, microdureza Vickers da seção transversal e ruído magnético de Barkhausen. Foi determinado o desempenho das superfícies por fadiga de contato de rolamento, num equipamento na configuração esfera-plano. Os corpos de prova foram anéis de AISI H13 temperados e revenidos. A totalidade dos ensaios foi realizada até a ocorrência de lascamento (Spalling). Os ensaios foram realizados com lubrificação e com uma máxima pressão de contato de Hertz de 3,6 GPa. Foi observado que dependendo do nível de integridade superficial induzido pelo processo de usinagem e dos parâmetros selecionados, o desempenho da superfície em fadiga de contato de rolamento foi afetado. Contudo, as melhores condições de desempenho foram dos materiais retificados, e para os materiais torneados o melhor desempenho foi obtido com maiores velocidades de corte. / The manufacturing process and the machining parameters selected lead to different integrity of the surface, and these characteristics will influence the functional performance of the components. This study evaluated and analyzed the effect of surface integrity on the contact fatigue resistance of the H13 hot work tool steel. The surfaces were manufactured by hard turning and grinding process. Therefore, the influences of the machining process and the cutting parameters on the surface and on the subsurface layer were studied. Four different turned surfaces were obtained as a combination of cutting parameters selected for the tests. On the other hand, grinding surfaces were generated using the same machining conditions. The characteristics of surface integrity evaluated were: surface roughness parameters, residual stresses, Barkhausen noise, and microhardness of surface and sub-layers in transverse section. It was also evaluated the performance of the samples by rolling contact fatigue tests conducted in a ball on washer machine. The specimens were rings made of AISI H13 steel, which were quenched and tempered. All tests were performed until the occurrence of spalling. The tests were carried out under lubrication and with a maximum Hertz contact pressure of 3.6 GPa. Monitoring and failure detection were carried out by analyzing the changes in the vibration signal of the test machine sensors. It was observed that the performance of the surface in rolling contact fatigue resistance was affected by the level of the surface integrity, related to the machining process and the machining parameters.

Ces travaux de thèse concernent l’étude des effets des oscillations de faibles amplitudes sur la durée de vie en fatigue de contact pour des composants d’actionneurs de vol. Des outils théoriques et expérimentaux ont pour cela été employés.Un modèle semi-analytique de contact rugueux élasto-plastique a été codé puis utilisé. Celui-ci, couplé au modèle de Dang Van, a permis de réaliser une étude théorique de l’influence du sens de passage de contacts sur la durée de vie en fatigue. Une comparaison en fatigue entre mouvements continus et mouvements oscillants a ainsi pu être faite.Un banc bi-disque a été spécifiquement développé chez UTAS pour pouvoir réaliser des essais de fatigue de roulement aussi bien en mouvements continus qu’en mouvements oscillants. Des essais de lubrification ont été réalisés sur des éprouvettes en XD15NW et en CX13VD afin de caractériser le phénomène de faux effet Brinell. Des essais de fatigue en lubrification optimale ont finalement été réalisés sur les éprouvettes en XD15NW en mouvements continus et en mouvements oscillants, les résultats ont été comparés et mis en vis-à-vis avec ceux de l’analyse théorique. / This PhD thesis is a study of small reciprocating motions effects on contact fatigue life of flight actuator components. Theoretical and practical tools are used for this purpose.A semi-analytical elasto-plastic rough contact code has been implemented and, then, used. This code, associated with Dang Van model, allowed us to perform a theoretical study of rolling direction effect on fatigue life. A comparison has been made between continuous motions and reciprocating motions.A twin-disc test bench has been specifically design at UTAS to allow us to perform rolling fatigue tests with continuous motions or with reciprocating motions. Lubrications tests have been done on XD15NW and CX13VD samples in order to study false brinelling phenomenon. Finally, fatigue tests in ideal lubrication conditions have been done on XD15NW samples with continuous motions and with reciprocating motions, results have been cross-checked each other and cross-checked with theoretical results.

In this thesis, a hierarchical multiscale method was developed to predict rolling contact fatigue lives of mechanical systems. In the proposed multiscale method, the molecular modeling and simulation of lubricant was conducted to investigate the friction between rolling contact surfaces. The calculated friction coefficient was passed to the continuum model of rolling contact components to predict fatigue lives. Molecular dynamics modeling and simulation of thin film lubrication and lubricated contact surfaces were carried out to investigate mechanisms of hydrodynamic lubrication at nano-scale first. Although various lubricant alkane chains were considered in the molecular model, the chain length of eight united molecules were mainly employed in this thesis. In addition, the effects of temperature and nano-particles (debris) on the friction forces were discussed. It was found that the existing of nano-particles (debris) could increase the friction force between contact surfaces with hydrodynamic lubrication. In the continuum model of the developed multiscale method, finite element analysis was employed to predict rolling contact fatigue life of rolling contact components, including bearing and gear-tooth. Specifically, the fatigue crack initiation of bearing was studied, and then the fatigue crack initiation and propagation in gear-tooth. In addition, the enhancement of gear-tooth fatigue life by using composite patches was discussed as well. It should be noted that the friction coefficient used in the continuum model was calculated in the molecular model. It is one-way message passing in the developed multiscale method. Another continuum method was studied and developed in this thesis to provide alternate methods for the continuum model in the proposed multiscale framework. Peridynamics method has advantages in modeling and simulation of discontinuities, including cracks, over the conventional finite element methods. The applications of Peridynamics in predicting fatigue crack initiation and propagation lives were discussed in this thesis.

Rolling contact fatigue is a damage process that may arise in mechanical applications with repeated rolling contacts. Some examples are: gears; cams; bearings; rail/wheel contacts. The resulting damage is often visible with the naked eye as millimeter sized surface craters. The surface craters are here denoted spalls and the gear contact served as a case study. The work focused on the asperity point load mechanism for initiation of spalls. It was found that the stresses at asperity level may be large enough to initiate surface cracking, especially if the complete stress cycle was accounted for. The gear contact is often treated as a cylindrical contact. The thesis contains experimental and numerical results connected to rolling contact fatigue of cylindrical contacts. At the outset a stationary cylindrical contact was studied experimentally. The stationary test procedure was used instead of a rolling contact. In this way the number of contact parameters was minimized. The cylindrical contact resulted in four different contact fatigue cracks. The two cracks that appeared first initiated below the contact. The other two cracks developed at the contact surface when the number of load cycles and the contact load increased. The influence of a surface irregularity (asperity) was studied numerically with the Finite Element Method (FEM). Firstly, the stationary contact was modelled and investigated numerically. At the cylindrical contact boundary a single axisymmetric was included. The partially loaded asperity introduced a tensile surface stress, which seen from the asperity centre was radially directed. Secondly, FE simulations were performed where a single axisymmetric asperity was over-rolled by a cylindrical contact. The simulations were performed for pure rolling and rolling with slip. For both situations, tensile forward directed stresses in front of the asperity were found. The presence of slip and a surface traction greatly increased the stresses in front of the asperity. Finally, when rolling started from rest with applied slip, the distance to steady-state rolling was determined for elastic similar cylindrical rollers. / QC 20100702

Os processos de manufatura, bem como os parâmetros de processamento utilizados produzem diferentes resultados com relação à integridade de uma superfície. Estas alterações se refletem em mudança das propriedades da superfície, as quais podem influenciar o desempenho dos componentes. O presente trabalho estuda o efeito da integridade superficial gerada pelos processos de torneamento e retificação na resistência à fadiga de contato do aço ferramenta AISI H13. A influência do processo de usinagem e dos parâmetros de corte no estado da superfície e subsuperfície, e como estas características afetam o desempenho são determinados. Foram geradas quatro condições diferentes para as superfícies torneadas mediante a combinação de parâmetros de corte. As superfícies retificadas foram produzidas empregando as mesmas condições de retificação, com isso, obteve-se a mesma condição para todos os corpos de prova ensaiados. As características medidas da integridade superficial foram: os parâmetros de rugosidade, tensões residuais, microdureza Vickers da seção transversal e ruído magnético de Barkhausen. Foi determinado o desempenho das superfícies por fadiga de contato de rolamento, num equipamento na configuração esfera-plano. Os corpos de prova foram anéis de AISI H13 temperados e revenidos. A totalidade dos ensaios foi realizada até a ocorrência de lascamento (Spalling). Os ensaios foram realizados com lubrificação e com uma máxima pressão de contato de Hertz de 3,6 GPa. Foi observado que dependendo do nível de integridade superficial induzido pelo processo de usinagem e dos parâmetros selecionados, o desempenho da superfície em fadiga de contato de rolamento foi afetado. Contudo, as melhores condições de desempenho foram dos materiais retificados, e para os materiais torneados o melhor desempenho foi obtido com maiores velocidades de corte. / The manufacturing process and the machining parameters selected lead to different integrity of the surface, and these characteristics will influence the functional performance of the components. This study evaluated and analyzed the effect of surface integrity on the contact fatigue resistance of the H13 hot work tool steel. The surfaces were manufactured by hard turning and grinding process. Therefore, the influences of the machining process and the cutting parameters on the surface and on the subsurface layer were studied. Four different turned surfaces were obtained as a combination of cutting parameters selected for the tests. On the other hand, grinding surfaces were generated using the same machining conditions. The characteristics of surface integrity evaluated were: surface roughness parameters, residual stresses, Barkhausen noise, and microhardness of surface and sub-layers in transverse section. It was also evaluated the performance of the samples by rolling contact fatigue tests conducted in a ball on washer machine. The specimens were rings made of AISI H13 steel, which were quenched and tempered. All tests were performed until the occurrence of spalling. The tests were carried out under lubrication and with a maximum Hertz contact pressure of 3.6 GPa. Monitoring and failure detection were carried out by analyzing the changes in the vibration signal of the test machine sensors. It was observed that the performance of the surface in rolling contact fatigue resistance was affected by the level of the surface integrity, related to the machining process and the machining parameters.

O presente trabalho destina-se à discussão sobre o cálculo de vida útil de rolamentos. Mostrando o avanço do processo de cálculo ao longo das décadas até o mais alto grau de desenvolvimento atual. A preocupação do texto é demonstrar de forma simples e objetiva as divergências que existem entre a formulação teórica e a real vida dos rolamentos, no que tange a fadiga de contato. Neste contexto foram realizados testes, em máquina especialmente destinada ao ensaio da fadiga de rolamentos. Variando-se para as duas séries de ensaios, apenas, a temperatura (aproximadamente 85°C e 110°C). Os resultados obtidos indicam que a vida real dos rolamentos apresenta grande divergência se comparada com a vida útil calculada, principalmente, no regime com maior temperatura. Atribui-se a esta disparidade, a ausência de cálculos precisos quanto à correlação da vida útil com o fator l, que é uma forma de se calcular o espaçamento entre as superfícies de contato, e o não emprego do cálculo do fator de carga, na formulação da vida útil de rolamentos. / The present work has the purpose of discussing the life of rolling bearings, describing the evolution of bearing life calculation until its current state of the art. Our focus is to demonstrate, simply and objectively, the inconsistencies occurring between the actual life of rolling bearings and their theoretical fatigue life estimation. For such purpose, tests were developed in a special bearing test rig to assess bearing fatigue. Two test sets were carried out with temperature being the only variation (approximately 85°C and 110°C). Results obtained from these tests suggest that the real life of rolling bearings is indeed very different from calculated bearing life, especially under higher temperature. Such disparity can be attributed to the lack of a precise computation of the relationship between bearing real life and the l factor - which determines the thickness of lubricant separating raceways and balls - as well as to the failure to compute the load factor in bearing life estimation.

The aim of the work presented in this thesis is to clarify one of the most fundamental aspects of fatigue damage in bearings steels through critical experiments, in particular whether damage in the form of cracks precedes hard “white-etching matter" formation, which is carbon supersaturated nanoscaled ferrite. Heat treatments have been designed to create four different crack types and distributions: scarce martensite plate cracks, fine grain boundary cracks, abundant martensite plate cracks, and surface cracks. Subsequent rolling contact fatigue experiments showed that the amount of hard white-etching matter is higher in pre-cracked samples compared to those without prior damage and that its formation mechanism is the frictional contact of disconnected surfaces within the bulk that elevate the temperature and localise deformation. These key experiments indicate that hard white-etching matter is the consequence, not the cause, of damage. Therefore, one way to avoid white-etching matter is by increasing the toughness of the material. The macroscopically homogenous distribution of microcracks proved also to be a useful rolling contact fatigue life enhancer due to damage deflection via crack branching and a powerful trap for diffusible hydrogen. Successful trapping was corroborated by the inability of hydrogen to cause crack propagation via embrittlement or accelerate white-etching matter generation during rolling contact fatigue. By also studying the behaviour of a nanostructured bainitic steel under rolling contact fatigue, it was found that its degradation mechanism is ductile void formation at bainitic ferrite/stress-induced martensite interfaces, followed by growth and coalescence into larger voids that lead to fracture along the direction of the softer phase as opposed to the conventional damage mechanism in 52100 steel of crack initiation at inclusions and propagation. Given the relevance of phase quantification in nanobainite and the possible surface artefacts introduced by preparation, alternative methods to X-ray diffraction such as magnetic measurements were also investigated. The lack of hard white-etching matter obtained in the carbide-free nanostructured bainite led to conclude that an alternative route to mitigate hard white-etching matter could be by eliminating pre-eutectoid carbides from the microstructure, therefore restricting their dissolution and ultimate carbon supersaturation of the mechanically deformed and homogenised nanoferrite.