The Ph.D. thesis is focused on a surface degradation mechanisms under combined heat and mechanical load. The objects of examination are work rolls from hot rolling mill which suffer such a load. In first chapter, the hot rolling process, the design, the manufacturing process and present materials of work rolls are described. The state-of-the-art study of work roll surface degradation mechanisms – wear, oxidation, thermal and contact fatigue are described in the second chapter. The characterization, the formation, the mechanisms of progression and the effects of each surface degradation mechanism is described step by step. The state-of-the-art study of analytical and numerical models which are related to hot rolling process is described in third chapter together with their limitations and flaws. The next chapters contain design of an analytical, an optimized macroscopic and a microscopic model for study of the work roll stress state. The macroscopic and the microscopic model is based on finite element method and they are implemented in ANSYS Programming Design Language. The models are used to process several case study which are based on previous experimental work of the Heat transfer and fluid flow laboratory. The results from case studies specify and expand the knowledge of work roll stress state. The results show the portion of each loading factor on the whole stress state. In addition, time and depth depended distribution of stress state is presented. The results from macrosferic model illustrate the cause of spalling and a rupture of the work roll. The results from the microsferic model show the cause of creation of the to-surface-parallel cracks within carbides of high chromium irons. Last chapter summarized of all results gathered from case studies together with the goals for further research definition. The necessary steps for further cognition are stated. The thesis contains a large set of appendixes with deeper discussion of several related topics. These appendixes represent the one third of whole the thesis.

No description available.

The effect of thermal-cycling-induced microcracking in fiber-reinforced polymer matrix composites is studied. Specific attention is focused on microcrack density as a function of the number of thermal cycles, and the effect of microcracking on the dimensional stability of composite materials. Changes in laminate coefficient of thermal expansion (CTE) and laminate stiffness are of primary concern. Included in the study are materials containing four different Thornel fiber types: a PAN-based T50 fiber and three pitch-based fibers, P55, P75, and P120. The fiber stiffnesses range from 55 Msi to 120 Msi. The fiber CTE's range from -0.50x10⁻⁶/°F to -0.80x10⁻⁶/°F. Also included are three matrix types: Fiberite's 934 epoxy, Amoco's ERL1962 toughened epoxy, and YLA's RS3 cyanate ester. The lamination sequences of the materials considered include a cross-ply configuration, [0/90]2s, and two quasi-isotropic configurations, [0/+45/-45/90]s and [0/+45/90/-45]s. The layer thickness of the materials range from a nominal 0.001 in. to 0.005 in. In addition to the variety of materials considered, three different thermal cycling temperature ranges are considered. These temperature ranges are ±250°F, ±150°F, and ±50°F. The combination of these material and geometric parameters and temperature ranges, combined with thermal cycling to thousands of cycles, makes this one of the most comprehensive studies of thermal-cycling-induced microcracking to date. Experimental comparisons are presented by examining the effect of layer thickness, fiber type, matrix type, and thermal cycling temperature range on microcracking and its influence on the laminates. Results regarding layer thickness effects indicate that thin-layer laminates microcrack more severely than identical laminates with thick layers. For some specimens in this study, the number of microcracks in thin-layer specimens exceeds that in thick-layer specimens by more than a factor of two. Despite the higher number of microcracks in the thin-layer specimens, small changes in CTE after thousands of cycles indicate that the thin-layer specimens are relatively unaffected by the presence of these cracks compared to the thick-layer specimens. Results regarding fiber type indicate that the number of microcracks and the change in CTE after thousands of cycles in the specimens containing PAN-based fibers are less than in the specimens containing comparable stiffness pitch-based fibers. Results for specimens containing the different pitch-based fibers indicate that after thousands of cycles, the number of microcracks in the specimens does not depend on the modulus or CTE of the fiber. The change in laminate CTE does, however, depend highly on the stiffness and CTE of the fiber. Fibers with higher stiffness and more negative CTE exhibit the lowest change in laminate CTE as a result of thermal cycling. The overall CTE of these specimens is, however, more negative as a result of the more negative CTE of the fiber. Results regarding matrix type based on the ±250°F temperature range indicate that the RS3 cyanate ester resin system exhibits the greatest resistance to microcracking and the least change in CTE, particularly for cycles numbering 3000 and less. Extrapolations to higher numbers of cycles indicate, however, that the margin of increased performance is expected to decrease with additional thermal cycling. Results regarding thermal cycling temperature range depend on the matrix type considered and the layer thickness of the specimens. For the ERL1962 resin system, microcrack saturation is expected to occur in all specimens, regardless of the temperature range to which the specimens are exposed. By contrast, the RS3 resin system demonstrates a threshold effect such that cycled to less severe temperature ranges, microcracking does not occur. For the RS3 specimens with 0.005 in. layer thickness, no microcracking or changes in CTE are observed in specimens cycled between between ±150°F or ±50°F. For the RS3 specimens with 0.002 in. layer thickness, no microcracking or changes in CTE are observed in specimens cycled between ±50°F.. Results regarding laminate stiffness indicate negligible change in laminate stiffness due to thermal cycling for the materials and geometries considered in this investigation. The study includes X-ray examination of the specimens, showing that cracks observed at the edge of the specimens penetrate the entire width of the specimen. Glass transition temperatures of the specimens are measured, showing that resin chemistry is not altered as a result of thermal cycling. Results are also presented based on a one-dimensional shear lag analysis developed in the literature. The analysis requires material property information that is difficult to obtain experimentally. Using limited data from the present investigation, material properties associated with the analysis are modified to obtain reasonable agreement with measured microcrack densities. Based on these derived material properties, the analysis generally overpredicts the change in laminate CTE. Predicted changes in laminate stiffness show reasonable correlation with experimentally measured values. / Ph. D.

The coupling resulting from the mutual influence of material thermal and mechanical parameters is examined in the thermal stress analysis of a long, hollow, multilayered, isotropic composite cylinder subjected to sudden axisymmetric external and internal temperature. The method of complex frequency response functions together with the Fourier transform technique is utilized. Because coupling parameters for some composite materials, such as carbon-carbon, are very small, the effect of coupling is neglected in the orthotropic thermal stress analysis. The stress distributions in long, hollow, multilayered orthotropic cylinders subjected to sudden axisymmetric temperature loading combined with dynamic pressure as well as asymmetric temperature loading are also obtained. The method of Fourier series together with Laplace transform is utilized in solving the heat conduction equation and thermal stress analysis. The inertial term is considered and the perturbation technique is applied to cylinders subjected to dynamic pressure loading. For brittle materials, like carbon-carbon composite, the strength variability is represented by two or three parameter Weibull distributions. The “weakest link" principle which takes into consideration both the applied stresses and the effected volume of material is used in the reliability analyses for both the isotropic and orthotropic carbon-carbon composite cylinders. The complex frequency response analysis is performed on a long hollow multilayed orthotropic cylinder under asymmetrical thermal load. Both deterministic and random thermal stress and reliability analyses can be based on the results of this frequency response analysis. The stress and displacement distributions and reliability of rocket motors under static or dynamic line loads are analyzed by an elasticity approach. Rocket motors are modeled as long hollow multilayered cylinders with an air core, a thick isotropic propellant inner layer and a thin orthotropic kevlar-epoxy case. The case is treated as a single orthotropic layer or a ten layered orthotropic structure. Five material properties and the load are treated as random variables with normal distributions when the reliability of the rocket motor is analyzed by the first-order, second-moment method (FOSM). / Ph. D. / incomplete_metadata

Published Article / This paper is based on tests performed on die component specimens manufactured by EOS-DMLS (direct metal laser sintering) and LENS (laser engineered net shape) RP (rapid prototyping) technology platforms, as well as manufactured specimens machined out of preferred standard hot work steel DIN 1.2344. These specimens resemble typical components used in metal high pressure die casting tool sets. The specimens were subjected to a programme of cyclic immersion in molten aluminium alloy and cooling in water-based die release medium. The heat checking and soldering phenomena were analyzed through periodic inspections, monitoring crack formation and evidence of surface washout. At the end of the thermal tests, mechanical strength and hardness tests were performed to assess toughness and core resistance variations in relation to the initial conditions. Finally metallographic investigations were performed through optical microscopy on all the specimens considered. The outcomes of this research will be presented and used by the CSIR for further development and application of the assessed EOS-DMLS and LENS rapid prototyping technologies in rapid die manufacturing techniques and die design principles, including time and economic feasibility criteria to be applied when considering rapid die manufacture.

O processo de injeção sob pressão de ligas de alumínio é empregado para a produção de peças diversas, destinadas principalmente à indústria automobilística. Dentre as principais vantagens deste processo, destaca-se a possibilidade de produção de peças complexas, com seções delgadas, e a alta velocidade de produção. Apesar desses pontos positivos, o reduzido tempo de ciclo e as elevadas temperaturas (~ 700°C) envolvidas promovem danos por fadiga térmica na superfície de trabalho das matrizes. Após milhares de peças produzidas, surgem trincas em regiões críticas, que crescem com o aumento da produção até atingirem condições que inviabilizam o uso da matriz, levando ao seu fim de vida. Na última década, novos aços de alta tenacidade e melhor resistência a quente, bem como tratamentos termoquímicos como a nitretação sob plasma vêm sendo aplicados em tais matrizes, retardando significativamente o fim de vida. Neste contexto, o presente trabalho visou estudar o fim de vida de matrizes de fundição sob pressão, relacionando-o aos aspectos microestruturais da superfície nitretada, tensões residuais inseridas durante processo de nitretação e as condições do processo de fundição. Para o estudo, os aços AISI H13, AISI H11 com redução do teor de Si e AISI H10 modificado, foram temperados e revenidos para dureza na faixa de 44 a 46 HRC e posteriormente nitretados sob plasma em diversas condições de temperatura, tempo e composição da atmosfera gasosa. Foram feitos ensaios de medições de tensões residuais, perfis de dureza, metalografia e difração de Raios-X. Para o estudo de fadiga térmica, foi utilizado o software DEFORM 3DTM para simular os danos ocasionados pelos mecanismos de fadiga térmica nas superfícies das matrizes com a presença e ausência de camada nitretada. Os resultados obtidos mostraram que a variação dos parâmetros de nitretação, tais como: tempo, temperatura e percentual de nitrogênio, afetam o perfil de dureza e de tensões residuais presentes na camada nitretada, bem como os microconstituintes da camada nitretada. Também foi verificado que a variação dos teores de elementos de liga de aços ferramenta para trabalho a quente em relação ao H13, mudam o perfil de dureza e de tensões residuais de compressão das camadas nitretadas. O material nitretado, após ser submetido em temperatura elevada, apresenta redução no nível de tensões residuais de compressão, ocorrendo processo de alívio de tensões. O mesmo efeito não é tão fortemente verificado no perfil de dureza do material. Deste modo, foi possível verificar que nos primeiros ciclos de injeção de alumínio, os mecanismos responsáveis por retardar a nucleação das trincas térmicas são a presença de tensões residuais de compressão na superfície do material e maior dureza local, dada pela maior dureza a quente existente no perfil de dureza da camada nitretada. Para estágios mais avançados de ciclagem térmica, apenas a maior dureza local será responsável por retardar a nucleação das trincas térmicas. A simulação demonstrou que o dano gerado durante processo de fadiga térmica é mais intenso no processo em que a matriz permanece exposta por tempos mais longos em elevadas temperaturas. O conhecimento destas características pode auxiliar a retardar o dano na superfície da matriz, via alterações do processo de fundição, ou das características dos aços ferramenta, dada pela tenacidade e resistência a quente da liga empregada na matriz, ou dos tratamentos térmicos e ou dos tratamentos de superfície, como a nitretação sob plasma, aplicados às matrizes. / The process of pressured injection of aluminum alloys is made use of in the production of sundry parts, meant mainly for the automotive industry. Among the main advantages of such process there stands out the possibility of production of complex parts, with thin sections, and at a high output speed. Despite these positive points, the reduced cycle time and high temperatures (~ 700°C) involved cause damage due to the thermal fatigue on the working surface of dies. After a great number of parts made there appear cracks in these areas that grow with the production increase up to reaching conditions that make the use of the die no longer viable, thus leading to its death. In the last decade, new unyielding, better heat resistant steels, as well as thermochemical treatments like plasma nitriding, have been applied to such dies, significantly hindering their death. In this context, the present paper has aimed at studying the death of pressured die casting by relating it to the microstructural aspects of the surface, residual tensions inserted during the nitriding process and the die casting conditions. For the study, AISI H13, AISI H11 with Si content reduction, and DIN WNr. 1.2367 steels were quenched and tempered to hardness in the range of 44 to 46 HRC and later subjected to plasma nitriding in different conditions of temperature, time, and gas atmosphere composition. Measurement tests of residual tensions, hardness profiles, metallography, and X-Ray diffraction have been carried out. For the thermal fatigue study, the software DEFORM 3D has been used to simulate damages caused by the thermal fatigue on the surface of dies in the presence or absence of surface nitriding. Results obtained have shown that the variation of nitriding parameters, such as time, temperature, and nitrogen percent, affect the hardness and residual tension profiles present in the surface nitriding, as well as in its microcomponents. It has also been ascertained that the variation of content of elements of steel tool alloys for heat work in relation to H13 one changes the profile of hardness and residual tensions of compression of nitriding treated surface. The resulting material, after being subjected to high temperature, presents a reduction of level in the residual tensions of compression, bringing about a process of tensions relief. The same effect is not so strongly verified in the material hardness profile. Accordingly, it has been possible to ascertain that in the first cycles of aluminum injection, the mechanisms responsible for slowing down the nucleation of thermal cracks are the presence of residual compression tensions on the material surface and higher spot hardness, given the higher heated hardness existing in the hardness profile of nitriding treated surface. For more advanced thermal cycling stages just the higher spot hardness will account for hindering the nucleation of thermal cracks. The simulation has demonstrated that the thermal fatigue process is more intense in process in which the die is exposed to high temperature for a longer time. The knowledge of these characteristics may help hinder the die surface damage through modifications in the casting process, or in the characteristics of tool steel (given the toughness and heat resistance of the alloy used in the die), or in the thermal treatments, or in the surface treatments, like plasma nitriding applied to dies.

Σκοπός της παρούσας διπλωματικής εργασίας είναι η μελέτη της επίδρασης της θερμικής κόπωσης στη μηχανική συμπεριφορά κοκκωδών συνθέτων υλικών πολυμερικής μήτρας ενισχυμένης με κόκκους ελαιοπυρήνα υπό μορφή σκόνης. Τα σύνθετα υλικά που κατασκευάσθηκαν μελετήθηκαν πειραματικά και τα αποτελέσματα αναλύθηκαν και προβλέφθηκαν θεωρητικά. Αρχικά πραγματοποίηθηκε η κατασκευή των συνθέτων υλικών σε διάφορες περιεκτικότητες σε κόκκους ελαιοπυρήνα. Από τον μηχανικό χαρακτηρισμό με στατικά πειράματα κάμψης τριών σημείων όλων των συνθέτων υλικών που κατασκευάστηκαν, διαπιστώθηκε η ενισχυτική ικανότητα του ελαιοπυρήνα σε μορφή σκόνης όταν αυτή χρησιμοποιείται ως υλικό ενίσχυσης για την κατασκευή συνθέτων υλικών. Ενώ, στη συνέχεια μελετήθηκε και η επίδραση της θερμικής κόπωσης στη μηχανική συμπεριφορά των συνθέτων υλικών που κατασκευάστηκαν. Τέλος, εφαρμόστηκαν δύο διαφορετικά μοντέλα πρόβλεψης του μέτρου ελαστικότητας συναρτήσει της περιεκτικότητας καθώς και της εναπομείνουσας αντοχής και δυσκαμψίας συναρτήσει των κύκλων θερμικής κόπωσης και έγινε σύγκριση των πειραματικών αποτελεσμάτων με τις αντίστοιχες προβλέψεις. Από τη σύγκριση αυτή παρατηρούμε ότι τα θεωρητικά μοντέλα που εφαρμόστηκαν που είναι το Μ.P.M (Modulus Predictive Model) και το R.P.M (Residual Properties Model) έδωσαν πολύ καλές προβλέψεις για την μεταβολή των ιδιοτήτων. Σαν γενικό συμπέρασμα από την παρούσα εργασία προκύπτει το γεγονός ότι το φθηνό και ελαφρύ υλικό του ελαιοπυρήνα μπορεί να χρησιμοποιηθεί αποτελεσματικά σαν υλικό ενίσχυσης ρητινών με πολύ καλά αποτελέσματα ενίσχυσης. / The aim of the present master thesis is to investigate the effect of thermal fatigue on the mechanical properties of particulate composites reinforced with olive pit’s powder. The composites materials that have been manufactured were investigated both; experimentally and theoretically. First, we manufactured composites reinforced with olive pits at different volume fractions of the filler particles. From the mechanical characterization of the materials investigated by means of static three-point bending experiments. It was found that the olive pits can reinforce the mechanical properties of composites materials when used as reinforced fillers. Next, the effect of thermal fatigue on the mechanical behaviour of the composites materials was investigated and theoretical predictions for their properties with and without thermal fatigue were made. More precisely, the Μ.P.M (Modulus Predictive Model) and the R.P.M (Residual Properties Model) models have been applied. A fair aggreement between experimental findings and theoretical predictions was found in all cases.

To meet the requirements of miniaturization and multifunction in microelectronics, understanding of their reliability and performance has become an important research subject in order to characterise electronics served under various loadings. Along with the demands of the increasing miniaturization of electronic devices, various properties and the relevant thermo-mechanical-electrical response of the lead-free solder joints to thermal cycling and electro-migration become the critical factors, which affect the service life of microelectronics in different applications. However, due to the size and structure of solder interconnects in microelectronics, traditional methods based on experiments are not applicable in the evaluation of their reliability under complex joint loadings. This thesis presents an investigation, which is based on finite-element method, into the performance of lead-free solder interconnects under thermal fatigue and electro-migration, specifically in the areas as follows: (1) the investigation of thermal-mechanical performance and fatigue-life prediction of flip-chip package under different sizes to achieve a further understanding of IMC layer and size effects of a flip chip package under thermal cycling; (2) the establishment of a numerical method, simulating void-formation/crack-propagation based on the results of finite-element analysis, to allow the prediction of crack evolution and failure time for electro-migration reliability of solder bumps; (3) the establishment of a flow-based algorithm for combination effects of thermal-mechanical and electro-migration that was subsequent implemented in to an FE model to evaluate the reliability assessment of service lives associated with a flip chip package.

O processo de injeção sob pressão de ligas de alumínio é empregado para a produção de peças diversas, destinadas principalmente à indústria automobilística. Dentre as principais vantagens deste processo, destaca-se a possibilidade de produção de peças complexas, com seções delgadas, e a alta velocidade de produção. Apesar desses pontos positivos, o reduzido tempo de ciclo e as elevadas temperaturas (~ 700°C) envolvidas promovem danos por fadiga térmica na superfície de trabalho das matrizes. Após milhares de peças produzidas, surgem trincas em regiões críticas, que crescem com o aumento da produção até atingirem condições que inviabilizam o uso da matriz, levando ao seu fim de vida. Na última década, novos aços de alta tenacidade e melhor resistência a quente, bem como tratamentos termoquímicos como a nitretação sob plasma vêm sendo aplicados em tais matrizes, retardando significativamente o fim de vida. Neste contexto, o presente trabalho visou estudar o fim de vida de matrizes de fundição sob pressão, relacionando-o aos aspectos microestruturais da superfície nitretada, tensões residuais inseridas durante processo de nitretação e as condições do processo de fundição. Para o estudo, os aços AISI H13, AISI H11 com redução do teor de Si e AISI H10 modificado, foram temperados e revenidos para dureza na faixa de 44 a 46 HRC e posteriormente nitretados sob plasma em diversas condições de temperatura, tempo e composição da atmosfera gasosa. Foram feitos ensaios de medições de tensões residuais, perfis de dureza, metalografia e difração de Raios-X. Para o estudo de fadiga térmica, foi utilizado o software DEFORM 3DTM para simular os danos ocasionados pelos mecanismos de fadiga térmica nas superfícies das matrizes com a presença e ausência de camada nitretada. Os resultados obtidos mostraram que a variação dos parâmetros de nitretação, tais como: tempo, temperatura e percentual de nitrogênio, afetam o perfil de dureza e de tensões residuais presentes na camada nitretada, bem como os microconstituintes da camada nitretada. Também foi verificado que a variação dos teores de elementos de liga de aços ferramenta para trabalho a quente em relação ao H13, mudam o perfil de dureza e de tensões residuais de compressão das camadas nitretadas. O material nitretado, após ser submetido em temperatura elevada, apresenta redução no nível de tensões residuais de compressão, ocorrendo processo de alívio de tensões. O mesmo efeito não é tão fortemente verificado no perfil de dureza do material. Deste modo, foi possível verificar que nos primeiros ciclos de injeção de alumínio, os mecanismos responsáveis por retardar a nucleação das trincas térmicas são a presença de tensões residuais de compressão na superfície do material e maior dureza local, dada pela maior dureza a quente existente no perfil de dureza da camada nitretada. Para estágios mais avançados de ciclagem térmica, apenas a maior dureza local será responsável por retardar a nucleação das trincas térmicas. A simulação demonstrou que o dano gerado durante processo de fadiga térmica é mais intenso no processo em que a matriz permanece exposta por tempos mais longos em elevadas temperaturas. O conhecimento destas características pode auxiliar a retardar o dano na superfície da matriz, via alterações do processo de fundição, ou das características dos aços ferramenta, dada pela tenacidade e resistência a quente da liga empregada na matriz, ou dos tratamentos térmicos e ou dos tratamentos de superfície, como a nitretação sob plasma, aplicados às matrizes. / The process of pressured injection of aluminum alloys is made use of in the production of sundry parts, meant mainly for the automotive industry. Among the main advantages of such process there stands out the possibility of production of complex parts, with thin sections, and at a high output speed. Despite these positive points, the reduced cycle time and high temperatures (~ 700°C) involved cause damage due to the thermal fatigue on the working surface of dies. After a great number of parts made there appear cracks in these areas that grow with the production increase up to reaching conditions that make the use of the die no longer viable, thus leading to its death. In the last decade, new unyielding, better heat resistant steels, as well as thermochemical treatments like plasma nitriding, have been applied to such dies, significantly hindering their death. In this context, the present paper has aimed at studying the death of pressured die casting by relating it to the microstructural aspects of the surface, residual tensions inserted during the nitriding process and the die casting conditions. For the study, AISI H13, AISI H11 with Si content reduction, and DIN WNr. 1.2367 steels were quenched and tempered to hardness in the range of 44 to 46 HRC and later subjected to plasma nitriding in different conditions of temperature, time, and gas atmosphere composition. Measurement tests of residual tensions, hardness profiles, metallography, and X-Ray diffraction have been carried out. For the thermal fatigue study, the software DEFORM 3D has been used to simulate damages caused by the thermal fatigue on the surface of dies in the presence or absence of surface nitriding. Results obtained have shown that the variation of nitriding parameters, such as time, temperature, and nitrogen percent, affect the hardness and residual tension profiles present in the surface nitriding, as well as in its microcomponents. It has also been ascertained that the variation of content of elements of steel tool alloys for heat work in relation to H13 one changes the profile of hardness and residual tensions of compression of nitriding treated surface. The resulting material, after being subjected to high temperature, presents a reduction of level in the residual tensions of compression, bringing about a process of tensions relief. The same effect is not so strongly verified in the material hardness profile. Accordingly, it has been possible to ascertain that in the first cycles of aluminum injection, the mechanisms responsible for slowing down the nucleation of thermal cracks are the presence of residual compression tensions on the material surface and higher spot hardness, given the higher heated hardness existing in the hardness profile of nitriding treated surface. For more advanced thermal cycling stages just the higher spot hardness will account for hindering the nucleation of thermal cracks. The simulation has demonstrated that the thermal fatigue process is more intense in process in which the die is exposed to high temperature for a longer time. The knowledge of these characteristics may help hinder the die surface damage through modifications in the casting process, or in the characteristics of tool steel (given the toughness and heat resistance of the alloy used in the die), or in the thermal treatments, or in the surface treatments, like plasma nitriding applied to dies.

The aim of this diploma thesis is to describe the causes and mechanisms of degradation processes that affect the surface of tools made of tool steel and to design and verify a practical solution that would lead to higher resistance of tools to these processes. Chapters in the theoretical part deal with fracture behavior of the material and the possibilities of its elimination, the experimental part includes testing of the effect of coating on the durability of hot forming tools.