[pt] O presente trabalho estuda a estabilidade microestrutural da liga 33 (Cr-Fe-Ni-N) em condições de trabalho, tendo em vista o desempenho das suas juntas soldadas em projetos industriais. Amostras desta liga seguiram um procedimento previamente programado de tratamentos térmicos de solubilização e envelhecimento isotérmico a 700 graus Celsius e 900 graus Celsius durante 1h, 10h e 100h. Nestas condições, foram identificados a ocorrência dos fenômenos de precipitação homogênea e heterogênea convencional, assim como da precipitação descontínua. A elucidação da cinética desta última é de particular interesse em virtude do efeito negativo nas propriedades mecânicas e desempenho de diversas ligas metálicas como elemento estrutural. Posteriormente, o material como recebido foi submetido ao processo de soldagem TIG autógena. Amostras da junta soldada passaram pelos tratamentos térmicos de solubilização e envelhecimento isotérmico a temperatura de 700 graus C durante 1 h, 10 h e 100 h, além de uma amostra ter sido envelhecida diretamente pós-soldagem durante 100h na temperatura de 700 graus Celsius. A caracterização microestrutural do material, a partir da condição como recebido, após tratamentos térmicos, como soldado e tratamentos térmicos pós-soldagem, foi realizada por microscopia ótica (MO), microscopia eletrônica de varredura (MEV) e microscopia eletrônica de transmissão convencional (MET) e na modalidade transmissão/varredura (STEM). Sempre que possível, microanálise qualitativa dos diferentes elementos micro estruturais foi levada a efeito por espectroscopia de dispersão de energia característica de raios-x (XEDS) acoplada ao MEV e ao MET/STEM. Foram realizados ensaios de microdureza para avaliar os efeitos da soldagem e dos tratamentos térmicos em todas as condições do material. Os resultados demonstram que tanto os precipitados homogêneos, heterogêneos em contornos de grão como as colônias de precipitação descontínuas são ricos em Cr. Nesta última, caracterizada por uma estrutura lamelar crescendo cooperativamente com a migração dos contornos de grão de alto ângulo, os precipitados lamelares parecem ter incorporado nitrogênio por difusão intergranular, formando Cr2N. Este fenômeno foi também detectado na junta soldada após envelhecimento direto a 700 graus Celsius durante 100h. Os resultados dos ensaios de dureza mostram o endurecimento por precipitação na liga 33 envelhecida em ambas as temperaturas utilizadas, diferentemente da junta soldada que apresentou discreta alteração de microdureza, mesmo após os tratamentos térmicos aplicados. / [en] This work studies the microstructural stability of alloy 33 (Fe-Cr-Ni-N) aiming at improving the performance of welded joints under in working conditions. Samples of this alloy followed a previously programmed procedure of homogenization and isothermal aging heat treatment at 700 degrees C and 900 degrees C for 1h, 10h and 100h. Under these conditions, the occurrence of homogeneous and heterogeneous conventional precipitation, as well as the discontinuous precipitation phenomena, were identified. The elucidation of the kinetics of the latter is of particular interest because of the well-known negative effect on the mechanical properties and performance of the several alloys applied as structural component. Subsequently, the as-received material was submitted to TIG welding process. Samples of the weld joints followed the same heat treatment schedule of homogenization and isothermal aging temperature of 700 degrees C for 1h, 10h and 100h. In addition, a welded sample was directly aged at this temperature for 100h at 700 degrees C. Microstructural characterization of the material, from the as received condition, to all post-heat treatment, as-welded and post-welding conditions was performed by optical microscopy (OM), scanning electron microscopy (SEM) and transmission electron microscopy, in the conventional (CTEM)and scanning/transmission (STEM) modes. Whenever possible, qualitative microanalysis of different microstructural elements was carried out by characteristic x-ray energy dispersive spectroscopic (XEDS) coupled to SEM and TEM/STEM. Micro-hardness tests were conducted to evaluate the effects of welding and heat treatment on the materials under all above mentioned conditions. The results demonstrate that both the homogeneous and heterogeneous precipitates at grain boundary as well as colonies of discontinuous precipitation are rich in chromium. In the latter, characterized by a lamellar structure growing cooperatively with high angle grain boundary migration, the lamellar precipitates appear to have nitrogen incorporated by inter granular diffusion mechanism, forming Cr2N.This phenomenon was also detected in the welded joint aged at 700 degrees C for 100 h. The results of the hardness tests show the precipitation hardening effect on the alloy aged at 33 at both temperatures , contrary to the welded joints where no significant change in micro-hardness were detected even after the application of heat treatments.

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One of the main sources of energy in this modern world is the gas turbine.  They reach extremely high working temperatures at peak capacity and hence require materials that can withstand the same.  Nickel-based superalloys have been widely used as working materials due to their various high-temperature properties, which help protect them from oxidation, corrosion,  and  creep.  This  high-temperature  strength  is  provided by the  gamma  prime (γ′)  phase  for  most  nickel-based  alloys.  This  study  deals  with understanding  the  effect of the mean γ′ phase size affected by different times and temperatures.  Different trial alloys have undergone different primary ageing cycles, followed by a subsequent secondary ageing  cycle.  Further,  the  mean  gamma  prime size  calculated  using  Image-Pro  coupled with  a  probability  density  function  for the mean  size  showed  significant  γ′  coarsening. Different temperatures and holding times also allowed for significant growth of secondary gamma prime structures.  These structures were found to impact the mean gamma prime size calculations significantly with their influence on the mechanical properties remaining unknown.  However, the mean gamma prime size remains similar to what was desired. / En av de viktigaste energikällorna i denna moderna värld är gasturbinen. De når extremt höga arbetstemperaturer vid toppkapacitet och kräver därför material som klarar av den höga temperaturen. Nickelbaserade superlegeringar har använts i stor utsträckning som material på grund av deras olika högtemperaturegenskaper, som hjälper till att skydda dem från oxidation, korrosion och krypning. Denna högtemperaturs hållfasthet uppnås från gamma prim-fasen (γ′) för de flesta nickelbaserade legeringar. Denna studie handlarom att förstå effekten av den genomsnittliga γ′-fasstorleken som påverkas av olika tider och temperaturer. Olika legeringar har genomgått olika primära åldringscykler, följt av en sekundär åldringscykel. Vidare visade den genomsnittliga gamma-prim storleken som beräknades med Image-Pro tillsammans med en sannolikhets densitetfunktion för medelstorleken av γ′ förgrovning. Olika temperaturer och hålltider möjliggjorde också betydande tillväxt av sekundära gamma-primstrukturer. Dessa strukturer visade sig påverka beräkningarna av den genomsnittliga gamma-primstorleken och egenskaperna av de mekaniska egenskaperna förblir okända. Den genomsnittliga gamma-primstorleken blir liknande det som var önskvärt.

<p>Thermal barrier coatings (TBCs) made of low-thermal-conductivity ceramic topcoat, metallic bond coat and metallic substrate, have been extensively used in gas turbine engines for thermal protection. Recently, additive manufacturing (AM) or 3D printing techniques have emerged as promising manufacturing techniques to fabricate engine components. The motivation of the thesis is that currently, application of TBCs on AM’ed metallic substrate is still in its infancy, which hinders the realization of its full potential.</p> <p>The goal of this thesis is to understand the processing-structure-property relationship in thermal barrier coating deposited on AM’ed superalloys.</p> <p>The APS method is used to deposit 7YSZ as the topcoat and NiCrAlY as the bond coat on TruForm 718 substrates fabricated using the direct metal laser sintering (DMLS) method. For comparison, another TBC system with the same topcoat and bond coat is deposited using APS on wrought 718 substrates. For thermomechanical property characterizations, thermal cycling, thermal shock (TS) and jet engine thermal shock (JETS) tests are performed for both TBC systems to evaluate thermal durability. Microhardness and elastic modulus at each layer and respective interfaces are also evaluated for both systems. Additionally, the microstructure and elemental composition are thoroughly studied to understand the cause for better performance of one system over the other.</p> <p>Both TBC systems showed similar performance during the thermal cycling and JETS test but TBC systems with AM substrates showed enhanced thermal durability especially in the case of the more aggressive thermal shock test. The TBC sample with AM substrate failed after 105 thermal shock cycles whereas the one with wrought substrate endured a maximum of 85 cycles after which it suffered topcoat delamination. The AM substrates also demonstrated an overall higher microhardness and elastic modulus except for post thermal cycling condition where it slightly underperformed. This study successfully demonstrated the use of AM built substrates for an improved TBC system and validated the enhanced thermal durability and mechanical properties of such a system.</p> <p>A modified YSZ TBC architecture with an intermediate Ti3C2 MXene layer is proposed to improve the interfacial adhesion at the topcoat/bond coat interface to improve the thermal durability of YSZ</p> <p>12</p> <p>TBC systems. First principles calculations are conducted to study the interfacial adhesion energy in the modified and conventional YSZ TBC systems. The results show enhanced adhesion at the bond coat/MXene interface. At the topcoat/MXene interface, the adhesion energy is similar to the adhesion energy between the topcoat and bond coat in a conventional YSZ TBC system.</p> <p>An alternative route is proposed for the fabrication of YSZ TBC on nickel base superalloy substrates by using the SPS technology. SPS offers a one-step fabrication process with faster production time and reduced production cost since all the layers of the TBC system are fabricated simultaneously. Two different TBC systems are processed using the same heating protocol. The first system is a conventional TBC system with 8YSZ topcoat, NiCoCrAlY bond coat and nickel base superalloy substrate. The second system is similar to the first but with an addition of Ti3C2 MXene layer between the topcoat and the bond coat. Based on the first principles study, addition of Ti3C2 layer enhances the adhesion strength of the topcoat/bond coat interface, an area which is highly susceptible to spallation. Further tests such as thermal cycling and thermal shock along with the evaluation of mechanical properties would be carried out for these samples in future studies to support our hypothesis.</p>

No description available.

No description available.

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>

Single crystal nickel-based superalloys are used in modern gas turbines because of their remarkable resistance to creep deformation at elevated temperatures, which is ensured by the addition of significant amounts of refractory elements. Too high concentrations of refractory elements can lead to the formation of topologically-close packed (TCP) phases during exposure to conditions of high temperature and stress which result in the degradation of the creep properties. The traditional methods for predicting the occurrence of TCP phases in Ni-based superalloys have been based on the PHACOMP and newPHACOMP methodologies which are well-known to fail with respect to new generations of alloys. In this work a novel two-dimensional structure map (Nbar, deltaV/V) for TCP phases where Nbar is the valence-electron count and deltaV/V is a compositional dependent size factor. This map is found to separate the experimental data on the TCP phases of binary, ternary and multi-component TCP phases into well-defined regions corresponding to different structure types such as A15, sigma, chi, delta, P, R, mu, and Laves. In particular, increasing size factor separates the A15, sigma and chi phases from the delta, P, R, mu phases. The structure map is then also used in conjunction with CALPHAD computations of sigma phase stability to show that the predictive power of newPHACOMP for the seven component Ni–Co–Cr–Ta–W–Re–Al system is indeed poor. In order to gain a microscopic understanding of the observed structural trends, namely the differences between the two groups of TCP structures with increasing deltaV/V and the trend from A15 to sigma to chi with increasing Nbar, the electronic structure is coarse-grained from density functional theory (DFT) to tight-binding to bond-order potentials (BOPs). First, DFT is used to calculate the structural energy differences across the elemental 4d and 5d transition metal series and the heats of formation of the binary alloys Mo-Re, Mo-Ru, Nb-Re, and Nb-Ru. These calculations show that the valence electron concentration stabilizes A15, sigma and chi but destablizes mu and Laves phases. The latter are shown to be stabilized instead by relative size difference. Second, a simple canonical TB model and in combination with the structural energy difference theorem is found to qualitatively reproduce the energy differences predicted by the elemental DFT calculations. The structural energy difference theorem rationalizes the importance of the size factor for the stability of the mu and Laves binary phases as observed in the structure map and DFT heats of formation. Finally, analytic BOP theory, is employed to identify the structural origins of the energetic differences between TCP structure-types that lead to the trends found within the two-dimensional structure map.

Ces travaux de thèse concernent l’étude du comportement thermo-physique de mélanges de polymères biosourcés chargés de poudre d’Inconel 718 mis en forme par Moulage par Injection de poudre Métallique. Des matériaux et procédés innovants pouvant permettre une amélioration du procédé ont été étudiés. L’utilisation de polyéthylène glycol (PEG), choisi pour ses propriétés de solubilité dans l’eau, et de polymères biosourcés, pour diminuer l’impact environnemental, ont été choisi. Les nuances de polymères biosourcés ont été choisies adaptées aux conditions du procédé de moulage par injection, il s’agit d’acide polylactique et de polyhydroalcanoates. De même, l’utilisation du CO2 à l’état supercritique comme solvant, a pour objectif de diminuer le temps de déliantage ainsi que d’augmenter la qualité des composants réalisés. Les résultats obtenus ont montré une dégradation du PEG et de l’acide stéarique lors des cycles de mélangeage de de moulage par injection dans les conditions d’utilisation des polymères biosourcés. L’utilisation des mélanges chargés composés de polymères biosourcés ont permis d’améliorer l’homogénéité des composants injectés, mais ont engendré des défauts lors de l’étape de déliantage. Ces défauts ont pu être éliminés par l’utilisation de CO2 à l’état supercritique comme solvant du PEG. Ce dernier procédé a permis une diminution importante du temps de déliantage ainsi qu’une amélioration de la qualité des composants finaux. Les composants densifiés possèdent les propriétés mécaniques correspondantes à l’Inconel 718. / The works done during this PhD focuses on the study of the thermo-physical behavior of bio sourced polymer blends loaded with Inconel 718 powder (feedstock) to be shaped by the Metal Injection Molding process (MIM). First, a review of the researches related to the MIM process was conducted to identify innovative materials and processes that can improve the MIM process. Thus, the use of polyethylene glycol (PEG), selected for its properties of solubility in water, and bio sourced polymers, in order to reduce the environmental impact, were selected. The bio sourced polymers have been selected in accordance with the conditions of the injection molding process, and the choice was made to use polylactic acid (PLA) and polyhydroalkanoates (PHA and PHBV). Similarly, the supercritical CO2 as solvent was chosen to reduce the time of binder removal as well as increasing the quality of components produced. Thermo-physical, mechanical and rheological characterizations were made to determine the behavior of the different feedstock formulations. The results showed a degradation of the PEG and of the stearic acid under the conditions of use of the biopolymers, during the mixing and the injection stages. The use of feedstock made of bio sourced polymers have improved the homogeneity of the injected components, but they have generated defects during the debinding step. These defects have been eliminated by the use of CO2 in the supercritical state as solvent of the PEG. This method has significantly decrease the time of binder removal and improved the quality of the final components. Finally, densified components have the mechanical properties corresponding to Inconel 718.

A superliga policristalina à base de níquel MAR-M247 foi desenvolvida na década de 70. Sua ótima composição, estabilidade microestrutural, excelente resistência à fluência e à oxidação e boa resistência à corrosão a quente faz dessa superliga uma das mais utilizadas em rotores durante os últimos 20 anos. Os objetivos do presente trabalho são a produção e caracterização microestrutural e mecânica de rotores da superliga MARM247 (10% peso Co, 10W, 8.25Cr, 5.5Al, 3Ta, 1.5Hf, 1Ti, 0.7Mo, 0.15C, 0.05Zr, 0.015B, Ni balanço). Os rotores foram obtidos pela técnica de microfusão por cera perdida na empresa Açotécnica S.A. (Jandira/SP) em diferentes temperaturas de vazamento e isolamento do molde cerâmico. Os materiais foram analisados por microscopia ótica e eletrônica de varredura (MEV/EDS), análise térmica diferencial (DTA), macro/microdureza e ensaios de tração convencional a 25oC e a 760oC. Além disso, os materiais passaram por tratamentos térmicos de solubilização e envelhecimento em diferentes temperaturas e tempos a fim de avaliar as mudanças microestruturais. Com a ajuda do software de cálculo termodinâmico Thermocalc foram feitas simulações das relações de fases utilizando a composição média da superliga MAR-M247. Os resultados permitiram obter uma condição de processamento (temperatura de vazamento e condição de isolamento) com maior quantidade de peças sem defeitos. Além disso, os experimentos permitiram definir uma condição ideal para o tratamento térmico de solubilização da superliga MAR-M247. / The polycrystalline nickel-based superalloy MAR-M247 was developed in the 1970s. Its optimal alloy composition, microstructural stability, excellent resistance to creep and oxidation and good resistance to hot corrosion make the MAR-M247 superalloy one of the alloys widely used in turbine rotors during the last 20 years. The aims of the present work are the production and the microstructural and mechanical characterization of rotors made of MAR-M247 superalloy (10 wt. % Co, 10W, 8.25Cr, 5.5Al, 3Ta, 1.5Hf, 1Ti, 0.7Mo, 0.15C, 0.05Zr, 0.015B, Ni balance). The rotors were produced by using the lost-wax technique at different pouring temperatures and isolation of the shell mold at the Açotécnica S.A. company (Jandira/SP). The materials were analyzed by optical and scanning electron microscopy (SEM/EDS), differential thermal analysis (DTA), macro/microhardness and tensile tests at 25oC and 760oC. Besides, the materials were submitted to solution and ageing treatments at different temperatures and times in order to evaluate de microstructural changes. With the aid of the thermodynamic calculation software Thermocalc, simulations of phase relations were made using the average composition of the MAR-M247 superalloy. The results allowed to obtain a processing condition (pouring temperature and isolation condition) with larger amount of rotors without defects. Moreover, the experiments allowed to define an ideal solution heat treatment condition of MAR-M247 superalloy.