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A need has been established in industry and academic publications to link an engine's maintenance costs throughout its operational life to its design as well as its operations and operating conditions. The established correlations between engine operation, design and maintenance costs highlight the value of establishing a satisfactory measure of the relative damage due to different operating conditions (operational severity). The methodology developed in this research enables the exploration of the causal, physics-based relationships underlying the statistical correlations in the public domain and identifies areas for further investigation. This thesis describes a physics-based approach to exploring the interactions, for commercial aircraft, of engine design, operation and through life maintenance costs. Applying the "virtual-workshop" workscoping concept to model engine maintenance throughout the operating life captures the maintenance requirements at each shop visit and the impact of a given shop visit on the timing and requirements for subsequent visits. Comparisons can thus be made between the cost implications of alternative operating regimes, flight profiles and maintenance strategies, taking into account engine design, age, operation and severity. The workscoping model developed operates within a physics-based methodology developed collaboratively within the research group which encompasses engine performance, lifing and operational severity modelling. The tool-set of coupled models used in this research additionally includes the workscoping maintenance cost model developed and implements a simplified 3D turbine blade geometry, new lifing models and an additional lifing mechanism (Thermo-mechanical fatigue (TMF)). Case studies presented model the effects of different outside air temperatures, reduced thrust operations (derate), flight durations and maintenance decisions. The use of operational severity and exhaust gas temperature margin deterioration as physics based cost drivers, while commonly accepted, limit the comparability of the results to other engine-aircraft pairs as the definition of operational severity, its derivation and application vary widely. The use of a single operation severity per mission based on high pressure turbine blade life does not permit the maintenance to vary with the prevalent lifing mechanism type (cyclic/steady state).

<p>I både kvalitets- och kontrollarbete finns det behov att kunskapsmässigt komma så nära verkligheten som möjligt vid fastställande av defektparametrar för oförstörande provning (OFP). Orsaken är att olika acceptanskrav och bedömningsgränser är svåra att klarlägga när man inte kan förlita sig på att uppgifter är realistiska. I projektet har olika erfarenheter använts för att få en bättre helhetsbild i området för defektparametrar och oförstörande provning.</p><p>Denna rapport redovisar den inledande delen av forskning och utvecklingsprojektet PLANT 2, där olika defektparametrar kartlagts och en teoretisk bedömning utförts med avseende på hur signalsvaret påverkas för OFP-metoderna virvelström (ET) och ultraljudsprovning (UT) i form av puls-eko (PE) och ”time-of-flight-diffraction” (TOFD).</p><p>Definitionen av redovisade defektparametrar följer i stort SKI-rapport 95:70 [1]. Defektparametrar i denna rapport redovisas i bilaga 1.</p><p>Vid bedömningen av defektparametrarnas inverkan på OFP-tekniker, har drift¬inducerande defekter och tillverkningsdefekter hanterats separat. För de driftinducerande defekterna delades bedömningen upp i en generell och en specifik bedömning. De defektparametrar som bedöms specifikt och klassats att påverka signalsvaret betydligt bör vara av mest intresse i nästkommande etapp. Följande defektparametrar bedömdes påverka signalsvaret betydligt:</p><p>• Form i ytan, antal sprickor och avstånd i gatstensmönster</p><p>(vid termisk ut¬mattning)</p><p>• Form i djupled</p><p>• Sprickbredd vid sprickspets och sprickspetsradie</p><p>För tillverkningsdefekter bedömdes defektparametrarnas form i djupled och geometri påverka signalsvaret betydligt för defekttyperna slagg och bindfel.</p><p>Vid utvärdering av UT-PE och UT-TOFD teknikerna överensstämde resultatet helt med den teoretiska bedömningen. För ET-tekniken stämde endast en av tre defektparametrar överens med den teoretiska bedömningen.</p> / <p>In quality control of defect parameters for Non-Destructive Testing (NDT) it’s essential to have good knowledge about the defects. The reason is that different acceptance criteria and assessments must be based on defects that correspond to real defects. In this project different experience has been analyzed to get a better overview between defect parameters and non-destructive testing.</p><p>This report shows the beginning of the research & development project PLANT 2. There are different flaw parameters that have been mapped and a theoretical assessment has been performed with regard to how the signal response is influenced by the NDT techniques eddy current, ultrasonic pulse echo and ultrasonic time-of-flight-diffraction.</p><p>The definition of the reported flaw parameters does in general follow the one presented in SKI-report 95:70 [1]. The actual flaw parameters in this report are presented in appendix 1.</p><p>In the assessment of the influences on the NDT techniques with regard to flaw parameters, service-induced flaws and manufactured flaws have been separated in to two categories. The service-induced flaws have further on been separated in a general and a specific assessment. Those flaw parameters that have been assessed to be specific and classified to influence the signal response considerably should be the ones of most interest in future studies. The following flaw parameters were assessed to affect the signal response considerably:</p><p>• Macroscopic shape in the surface direction, number of cracks</p><p>and cobblestone stone pattern distance (for thermal fatigue)</p><p>• Macroscopic shape in the through thickness direction</p><p>• Crack width at the crack tip and the crack tip radius</p><p>For flaws caused by the manufacturing process, type slag and lack of fusion, the flaw parameters “Macroscopic shape in the through thickness direction” and “the geometry” were influenced by the signal response considerably.</p><p>In the evaluation of signal response with the UT pulse echo and UT TOFD techniques, the result corresponded to the theoretical assessment. For the eddy current technique only one of three flaw parameters corresponded to the theoretical assessment.</p>

I både kvalitets- och kontrollarbete finns det behov att kunskapsmässigt komma så nära verkligheten som möjligt vid fastställande av defektparametrar för oförstörande provning (OFP). Orsaken är att olika acceptanskrav och bedömningsgränser är svåra att klarlägga när man inte kan förlita sig på att uppgifter är realistiska. I projektet har olika erfarenheter använts för att få en bättre helhetsbild i området för defektparametrar och oförstörande provning. Denna rapport redovisar den inledande delen av forskning och utvecklingsprojektet PLANT 2, där olika defektparametrar kartlagts och en teoretisk bedömning utförts med avseende på hur signalsvaret påverkas för OFP-metoderna virvelström (ET) och ultraljudsprovning (UT) i form av puls-eko (PE) och ”time-of-flight-diffraction” (TOFD). Definitionen av redovisade defektparametrar följer i stort SKI-rapport 95:70 [1]. Defektparametrar i denna rapport redovisas i bilaga 1. Vid bedömningen av defektparametrarnas inverkan på OFP-tekniker, har drift¬inducerande defekter och tillverkningsdefekter hanterats separat. För de driftinducerande defekterna delades bedömningen upp i en generell och en specifik bedömning. De defektparametrar som bedöms specifikt och klassats att påverka signalsvaret betydligt bör vara av mest intresse i nästkommande etapp. Följande defektparametrar bedömdes påverka signalsvaret betydligt: • Form i ytan, antal sprickor och avstånd i gatstensmönster (vid termisk ut¬mattning) • Form i djupled • Sprickbredd vid sprickspets och sprickspetsradie För tillverkningsdefekter bedömdes defektparametrarnas form i djupled och geometri påverka signalsvaret betydligt för defekttyperna slagg och bindfel. Vid utvärdering av UT-PE och UT-TOFD teknikerna överensstämde resultatet helt med den teoretiska bedömningen. För ET-tekniken stämde endast en av tre defektparametrar överens med den teoretiska bedömningen. / In quality control of defect parameters for Non-Destructive Testing (NDT) it’s essential to have good knowledge about the defects. The reason is that different acceptance criteria and assessments must be based on defects that correspond to real defects. In this project different experience has been analyzed to get a better overview between defect parameters and non-destructive testing. This report shows the beginning of the research &amp; development project PLANT 2. There are different flaw parameters that have been mapped and a theoretical assessment has been performed with regard to how the signal response is influenced by the NDT techniques eddy current, ultrasonic pulse echo and ultrasonic time-of-flight-diffraction. The definition of the reported flaw parameters does in general follow the one presented in SKI-report 95:70 [1]. The actual flaw parameters in this report are presented in appendix 1. In the assessment of the influences on the NDT techniques with regard to flaw parameters, service-induced flaws and manufactured flaws have been separated in to two categories. The service-induced flaws have further on been separated in a general and a specific assessment. Those flaw parameters that have been assessed to be specific and classified to influence the signal response considerably should be the ones of most interest in future studies. The following flaw parameters were assessed to affect the signal response considerably: • Macroscopic shape in the surface direction, number of cracks and cobblestone stone pattern distance (for thermal fatigue) • Macroscopic shape in the through thickness direction • Crack width at the crack tip and the crack tip radius For flaws caused by the manufacturing process, type slag and lack of fusion, the flaw parameters “Macroscopic shape in the through thickness direction” and “the geometry” were influenced by the signal response considerably. In the evaluation of signal response with the UT pulse echo and UT TOFD techniques, the result corresponded to the theoretical assessment. For the eddy current technique only one of three flaw parameters corresponded to the theoretical assessment.

Conselho Nacional de Desenvolvimento Científico e Tecnológico / Non carious cervical lesions (NCCLs) are routine findings in clinical practice and are described as the loss of tooth tissue close to the cementum enamel junction. NCCLs have multifactorial etiology with main factors involved are stress, biocorrosion and friction. The different associations of these factors can lead to the weakening of the tooth structure in the cervical region, generating NCCLs. The aim of this study was to evaluate the association of etiologic factors (stress, biocorrosion and friction) on the microstructural formation of NCCLs, using finite element analysis, laser confocal microscopy and computed microtomography (micro-CT). Two three dimensional (3D), linear and elastic models of mandibular premolars were generated for stress distribution evaluation, using the finite element analysis (FEA). Two oblique loadings (50 N), were applied on the buccal cusp slope of the model. The occlusal loading (CO) was applied on the grinding region of the buccal cusp and the buccal loading (CV) on the smooth region of the same cusp. Both loads were applied at 45&#778; to the tooth long axis, simulating mandibular excursive movements. The displacement restriction was applied on the base and lateral surface of the model and the results were analyzed by the maximum principal criteria. Then, for analysis by confocal microscopy, forty intact human mandibular premolars were selected and allocated randomly into four groups, according to the factor association type (n=10): (TB) stress-biocorrosion, (TF) stress-friction, (BF) biocorrosion-friction, and (TBF) stress-biocorrosion-friction. In each group, the challenges were performed in an alternate way. The stress was simulated by cyclic fatigue loading, with specimens positioned in mechanical fatigue machine and subjected to oblique load (50N), on the smooth region of the buccal cusp for 6 x 105 cycles. The biocorrosive challenge was performed using the application of hydrochloric acid (2mL/10s). The friction (abrasion) was reproduced by using electric/powered toothbrushes (300g/20s), with Colgate Total 12 toothpaste. The roughness surface, angle and height of steps were measured before and after the treatments, using a 3D laser confocal microscope. The data were analyzed using the paired t-test, two-way analysis of variance and Tukey s test (&#945;=0.05). Then, three specimens of each group were taken to a micro-CT for the qualitative analyses. The CV loading promoted higher concentration of tensile stress in the cervical region compared to CO. The presence of biocorrosion was an important factor to roughness changes and abrasion promoted similar behavior among the groups. The TBF association promoted the greatest alterations in tooth structures. Enamel and dentin showed distinct performance according to the different interactions. The FEA results presented relationship with the experimental findings for TF,TB, TBF groups. The TBF was the more influent association on the microstructural formation of NCCLs, for enamel. For dentin, the association of at least two factors was sufficient to generate significant tissue degradation. All studied associations of etiological factors showed potential to promote NCCLs formation. / As lesões cervicais não cariosas (LCNCs) são achados rotineiros na prática clínica odontológica e são descritas como a perda de tecido dentário próximo à junção amelo cementária (JAC). Essas lesões apresentam etiologia multifatorial e tem como principais fatores envolvidos nesse processo tensão, biocorrosão e fricção. As associações desses fatores levam ao enfraquecimento da estrutura dental na região cervical, promovendo o surgimento de LCNCs. O objetivo deste estudo foi avaliar o efeito das associações de fatores etiológicos (tensão, biocorrosão e fricção) na formação microestrutural de LCNCs, empregando método de elementos finitos (MEF), microscopia confocal a laser e microtomografia computadorizada (micro-CT). Dois modelos tridimensionais (3D), lineares e elásticos de pré-molares inferiores foram gerados para análise do padrão de distribuição de tensões na região cervical, pelo método de elementos finitos (MEF). Dois tipos de cargas de 50N, foram aplicadas obliquamente a cúspide vestibular do modelo. A carga oclusal (CO), foi aplicada na vertente triturante da cúspide vestibular e a carga vestibular (CV), na vertente lisa da mesma cúspide. As cargas foram posicionadas a 45º do longo do eixo do dente, e simularam interferências oclusais nos movimentos excursivos da mandíbula. A restrição do deslocamento foi realizada na base e laterais do modelo e a análise dos resultados conduzida por meio do critério de Tensão Máxima Principal. Para a análise por microscopia confocal, quarenta pré-molares inferiores humanos hígidos foram selecionados e distribuídos aleatoriamente em quatro grupos, de acordo com as seguintes associações de fatores (n=10): tensão-biocorrosão (TB), tensão-fricção (TF), e biocorrosão-fricção (BF) e tensão-biocorrosão-fricção (TBF). Para cada grupo, os desafios foram realizados de forma alternada. A tensão foi simulada por meio de ciclagem mecânica, com os espécimes posicionados em máquina de fadiga cíclica e submetidos a carregamentos oblíquos de 50N, na frequência de 2Hz, na vertente lisa e na vertente triturante da face vestibular, por 6 x 105 ciclos. Os desafios biocorrosivos foram realizados pela aplicação de 2mL de ácido hidroclorídrico por 10s. E os desafios de fricção (abrasão) foram reproduzidos com escovas elétricas (300g / 20s), com a utlização de pasta Colgate Total 12. A rugosidade da superfície, ângulo e altura dos degraus foram medidos antes e após os tratamentos, utilizando microscópio confocal a laser 3D. Para avaliação da distribuição e homogeineidade dos dados, foram realizados os testes de Shapiro Wilk e Levene. E posteriormente, aplicados o teste t-pareado, análise de variância em fator (ANOVA) e teste de Tukey (&#945; = 0,05). Em seguida, três amostras de cada grupo foram analisadas no micro-CT para as análises qualitativas de perda estrutural. O CV promoveu maior concentração de tensões de tração na região cervical do que o CO. A presença da biocorrosão foi fator importante na alteração de rugosidade e a abrasão resultou em comportamento semelhante entre os grupos. A associação TBF promoveu as maiores alterações nas estruturas dentais. Esmalte e dentina mostraram desempenho distinto de acordo com as diferentes interações. Foi verificada relação entre os resultados gerados pelo MEF e os achados experimentais para os grupos TF, TBF, TB. O grupo TBF foi mais influente na formação microestrutural das LCNCs, para esmalte. Para dentina, a associação de pelo menos dois fatores foi suficiente para gerar degradação significativa de tecido na região cervical. Todos as associações de fatores estudadas mostraram potencial para promover a formação de LCNCs. / Mestre em Odontologia

Electrical machines in electrified heavy-duty vehicles are subjected to dynamic temperature loadings during normal operation due to the different driving conditions. The Electrical Insulation System (EIS) in a stator winding is aged as an effect of these dynamic thermal loads. The thermal loads are usually high constant temperatures and thermal cycling. The high average constant thermal load is well-known in the electrical machine industry but little is known about the effect of temperature cycling. In this project, the ageing of the EIS in stator windings due to temperature cycling is examined. In this project, computational simulations of different simplified models that represent the electrical insulation system are made to analyse the thermo-mechanical stresses that is induced due to thermal cycling. Furthermore, a test object was designed and simulated to replicate the stress levels obtained from the simulations. The test object is to ease the physical testing of electrical insulation system. Testing a complete stator takes time and has the disadvantage of having a high mass, therefore a test object is designed and a test method is provided. The results from the finite element analysis indicate that the mechanical stresses induced will affect the lifetime of the electrical insulation system. A sensitivity study of several thermal cycling parameters was performed, the stator core length, the cycle rate and the temperature cycle amplitude. The results obtained indicate that the stator core length is too short to have a significant effect on the thermo-mechanical stresses induced. The results of the sensitivity study of the temperature cycle rate and the temperature cycle amplitude showed that these parameters increase the thermo-mechanical stresses induced. The results from the simulations of the test object is similar to the results from the simulations of the stator windings, which means that the tests object is valid for testing. The test method that is most appropriate is the power cycling test method, because it replicates the actual application of stator windings. The thermally induced stresses exposing the slot insulation exceeds the yield strength of the material, therefore plastic deformation may occur only after one thermal cycle. The other components in the stator are exposed to stresses below the yield strength. The thermally induced stresses exposing the slot insulation are high enough to low cycle fatigue the electrical insulation system, thus thermo-mechanical fatigue is an ageing factor of the electrical insulation system.

Tato diplomová práce se zabývá posouzením tepelně-mechanické únavy výfukového potrubí. Nejprve byla provedena rešeršní studie, ve které je rozebrán fenomén tepelně-mechanické únavy. Byly prezentovány hlavní mechanismy poškození a přístupy k jejich modelování. Diskutována byla i specifická chování materiálu vystavenému tepelně-mechanickému zatěžování. Byl vypracován přehled vhodných modelů materiálu a modelů únavové životnosti společně s algoritmem predikce tepelně-mechanické únavy komponenty. Poté byl tento teoretický základ aplikován na praktický případ výfukového potrubí podléhajícího tepelně-mechanickému zatěžování. Dva tepelně závislé elasto-plastické modely materiálu byly nakalibrovány a validovány na základě experimentálních dat. Byl vytvořen diskretizovaný konečnoprvkový model sestavy výfukového potrubí. Model tepelných okrajových podmínek byl předepsán na základě výpočtů ustáleného sdruženého přestupu tepla. Slabě sdružená tepelně-deformační úloha byla vyřešena metodou konečných prvků pro oba modely materiálů. Bylo použito paradigma nesvázaného modelu únavy, které je vhodné pro nízkocyklovou únavu. Životnost byla tedy vyhodnocena jako součást post-procesoru. Použity byly dva modely únavové životnosti – energeticky založený model a deformačně založený model. Získané hodnoty životnosti byly porovnány vzhledem k použitým modelům materiálu a modelům únavové životnosti. Nakonec jsou diskutovány závěry této práce, oblasti dalšího výzkumu a navrženy možnosti na zlepšení použitých přístupů.

<p dir="ltr">In structural metallic components, a material’s lifecycle begins with the processing route, to produce a desired structure, which dictates the in-service performance. The variability of microstructural features as a consequence of the processing route has a direct influence on the properties and performance of a material. In order to correlate the influence processing conditions have on material performance, large test matrices are required which tend to be time consuming and expensive. An alternative route to avoid such large test matrices is to incorporate physics-based process modeling and lifing paradigms to better understand the performance of structural materials. By linking microstructural information to the material’s lifecycle, the processing path can be modified without the need to repeat large-scale testing requirements. Additionally, when a materials system is accurately modeled throughout its lifecycle, the performance predictions can be leveraged to improve the design of materials and components.</p><p dir="ltr">Ni-based superalloys are a material class widely used in many critical aerospace components exposed to coupling thermal and mechanical loads due to their increased resistance to creep, corrosion, oxidation, and strength characteristics at elevated temperatures. Many Ni-based superalloys undergo high-temperature forging to produce a desired microstructure, targeting specific strength and fatigue properties in order to perform under thermo-mechanical loads. When in-service, these alloys tend to fail as a consequence of thermo-mechanical fatigue (TMF) from either inclusion- or matrix- driven failure. In order to produce safer, cheaper and more efficient critical aerospace components, the micromechanical deformation and damage mechanisms throughout a Ni-based superalloy’s lifecycle must be understood. This research utilizes process modeling as a tool to understand the damage and deformation of inclusions in a Ni-200 matrix throughout radial forging as a means to optimize the processing conditions for improved fatigue performance. In addition, microstructural sensitive performance modeling for a Ni-based superalloy is leveraged to understand the influence TMF has on damage mechanisms.</p><p dir="ltr">The radial forging processing route requires both high temperatures and large plastic deformation. During this process, non-metallic inclusions (NMIs) can debond from the metallic matrix and break apart, resulting in a linear array of smaller inclusions, known as stringers. The evolution of NMIs into stringers can result in matrix load shedding, localized plasticity, and stress concentrations near the matrix-NMI interface. Due to these factors, stringers can be detrimental to the fatigue life of the final forged component. By performing a finite element model of the forging process with cohesive zones to simulate material debonding, this research contributes to the understanding of processing induced deformation and damage sequences on the onset of stringer formation for Alumina NMIs in a Ni-200 matrix. Through a parametric study, the interactions of forging temperature, strain rate, strain per pass, and interfacial decohesion on the NMI damage evolution metrics are studied, specifically NMI particle separation, rotation, and cavity formation. The parametric study provides a linkage between the various processing conditions parameters influence on detrimental NMI morphology related to material performance.</p><p dir="ltr">The microstructural characteristics of Ni-based superalloys, as a consequence of a particular processing route, creates a variability in TMF performance. The micromechanical failure mechanisms associated with TMF are dependent on various loading parameters, such as temperature, strain range, and strain-temperature phasing. Insights on the complexities of micromechanical TMF damage are studied via a temperature-dependent, dislocation density-based crystal plasticity finite element (CPFE) model with uncertainty quantification. The capabilities of the model’s temperature dependency are examined via direct instantiation and comparison to a high-energy X-ray diffraction microscopy (HEDM) experiment under coupled thermal and mechanical loads. Unique loading states throughout the experiment are investigated with both CPFE predictions and HEDM results to study early indicators of TMF damage mechanisms at the grain scale. The mesoscale validation of the CPFE model to HEDM experimental data provides capabilities for a well-informed TMF performance paradigm under various strain-temperature phase profiles. </p><p dir="ltr">A material’s TMF performance is highly dependent on the temperature-load phase profile as a consequence of path-dependent thermo-mechanical plasticity. To investigate the relationship between microstructural damage and TMF phasing effects, the aforementioned CPFE model investigates in-phase (IP) TMF, out-of-phase (OP) TMF, and iso-thermal (ISO) loading profiles. A microstructural sensitive performance modeling framework with capabilities to isolate phasing (IP, OP, and ISO) effects is presented to locate fatigue damage in a set of statistically equivalent microstructures (SEMs). Location specific plasticity, and grain interactions are studied under the various phasing profiles providing a connection between microstructural material damage and TMF performance.</p>