965 resultados para martensitic transformation temperatures
Resumo:
Samples of sintered AISI 316L stainless steel were plasma nitrided in a mixture of H-2-20% N-2, for 3 or 4 h. The treatment temperature was selected in 400-550 degreesC interval, in steps of 50 degreesC. X-ray diffraction (glancing angle geometry-GAXRD), conversion electron Mossbauer spectroscopy (CEMS), optical microscopy and Vickers microhardness were used as analytical techniques. For T greater than or equal to 500 degreesC and t = 4 h, a 40-mum layer is formed. The GAXRD results showed a transformation of the austenite gamma phase to the martensite in the sinterization process and showed as well, that the gamma' (Fe4N) phase is the predominant nitride besides small amounts of epsilon-Fe2N, gamma(N) CrN, Cr2O3 and the fcc nitrogen supersatured solid phase gamma(N). The CrN phase seems to decrease with temperature while the gamma(N) phase fraction is almost less than or equal to10%, independently on the temperature. The CEMS results indicated that while the gamma(N) fraction decreases with temperature of plasma nitriding, the gamma' fraction increases proportionally. (C) 2003 Elsevier B.V. All rights reserved.
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New classes of martensitic stainless steels, with low carbon levels, have been developed aiming to meet the needs of the petroleum industry segment. However, their use has been restricted due to the fact it is a recent development and many of its properties are still under investigation. This work determines the values of initial and final temperatures for the austenitic transformation and the initial and final temperatures of martensitic formation for alloy 13Cr2Ni0,1C, by means of dilatometric tests under continuous cooling. Based on these results the optimized conditions for quench and temper heat treatments were obtained. The microstructural characterization of the alloys under coarse fusion condition was carried out by optical microscopy and the presence of delta-ferrite in the martensitic matrix was observed.
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An experimental and numerical study of ballistic impacts on steel plates at various temperatures (700ºC, 400ºC and room temperature) has been carried out. The motivation for this work is the blade‐off event that may occur inside a jet engine turbine. However, as a first attempt to understand this complex loading process, a somewhat simpler approach is carried out in the present work. The material used in this study is the FV535 martensitic stainless steel, which is one of the most commonly used materials for turbine casings. Based on material test data, a Modified Johnson‐Cook (MJC) model was calibrated for numerical simulations using the LS‐DYNA explicit finite element code (see Figure 1). To check the mesh size sensitivity, 2D axisymmetric finite element models with three different mesh sizes and configurations were used for the various temperatures. Two fixed meshes with 64 and 128 elements over the 2mm thick plate and one mesh with 32 elements over the thickness with adaptive remeshing were used in the simulations. The formation of adiabatic shear bands in the perforation process has been found critical in order to achieve good results. Adiabatic shear bands are formed by the temperature rise due to the accumulation of plastic strain during impact (see Figure 2). The influence of the thermal softening in the plastic model has hence been analyzed for the room temperature impact tests, where the temperature gradient is highest
Flow and fracture behaviour of FV535 steel at different triaxialities, strain rates and temperatures
Resumo:
The new generation jet engines operate at highly demanding working conditions. Such conditions need very precise design which implies an exhaustive study of the engine materials and behaviour in their extreme working conditions. With this purpose, this work intends to describe a numerically-based calibration of the widely-used Johnson–Cook fracture model, as well as its validation through high temperature ballistic impact tests. To do so, a widely-used turbine casing material is studied. This material is the Firth Vickers 535 martensitic stainless steel. Quasi-static tensile tests at various temperatures in a universal testing machine, as well as dynamic tests in a Split Hopkinson Pressure Bar, are carried out at different triaxialities. Using ABAQUS/Standard and LS-DYNA numerical codes, experimental data are matched. This method allows the researcher to obtain critical data of equivalent plastic strain and triaxility, which allows for more precise calibration of the Johnson–Cook fracture model. Such enhancement allows study of the fracture behaviour of the material across its usage temperature range.
Resumo:
O desenvolvimento dos aços inoxidáveis Super-Martensíticos (SM) nasce da necessidade de implementar novas tecnologias, mais econômicas e amigáveis ao meio ambiente. Os aços inoxidáveis SM são uma derivação dos aços inoxidáveis martensíticos convencionais, diferenciando-se basicamente no menor teor de carbono, na adição de Ni e Mo. Foram desenvolvidos como uma alternativa para aços inoxidáveis duplex no uso de dutos para a extração de petróleo offshore em meados dos anos 90. Para que esses aços apresentem as propriedades mecânicas de resistência à tração e tenacidade é necessário que sejam realizados tratamentos de austenitização, seguido de têmpera, e de revenimento, onde, particularmente para este último, há várias opções de tempos e temperaturas. Como os tratamentos térmicos geram as propriedades mecânicas através de transformações de fase (precipitação) podem ocorrer alterações da resistência à corrosão. São conhecidos os efeitos benéficos da adição de Nb em aços inoxidáveis tradicionais. Por isso, o objetivo desta pesquisa foi estudar aços inoxidáveis SM contendo Nb. Foi pesquisada a influência da temperatura de revenimento sobre a resistência à corrosão de três aços inoxidáveis SM, os quais contêm 13% Cr, 5% Ni, 1% a 2% Mo, com e sem adições de Nb. No presente trabalho, foram denominados de SM2MoNb, SM2Mo e SM1MoNb, que representam aços com 2% Mo, 1% Mo e 0,11% Nb. Dado que os principais tipos de corrosão para aços inoxidáveis são a corrosão por pite (por cloreto) e a corrosão intergranular (sensitização), optou-se por determinar os Potenciais de Pite (Ep) e os Graus de Sensitização (GS) em função da temperatura de revenimento. Os aços passaram por recozimento a 1050°C por 48 horas, para eliminação de fase ferrita delta. Em seguida foram tratados a 1050 °C por 30 minutos, com resfriamento ao ar, para uniformização do tamanho de grão. A estrutura martensítica obtida recebeu tratamentos de revenimento em temperaturas de: 550 °C, 575 °C, 600 °C, 625 °C, 650 °C e 700 °C, por 2 horas. O GS foi medido através da técnica de reativação eletroquímica potenciodinâmica na versão ciclo duplo (DL-EPR), utilizando-se eletrólito de 1M H2SO4 + 0,01M KSCN. Para determinar o Ep foram realizados ensaios de polarização potenciodinâmica em 0,6M NaCl. Os resultados obtidos foram discutidos através das variações microestruturais encontradas. Foram empregadas técnicas de microscopia ótica (MO), microscopia eletrônica de varredura (MEV), simulação termodinâmica de fases através do programa Thermo-Calc e determinação de austenita revertida mediante difração de raios X (DRX) e ferritoscópio. A quantificação da austenita por DRX identificou que a partir de 600 °C há formação desta fase, apresentando máximo em 650 °C, e novamente diminuindo para zero a 700 °C. Por sua vez, o método do ferritoscópio detectou austenita nas condições em que a analise de DRX indicou valor nulo, sendo as mais críticas a do material temperado (sem revenimento) e do aço revenido a 700 °C. Propõe-se que tais diferenças entre os dois métodos se deve à morfologia fina da austenia retida, a qual deve estar localizada entre as agulhas de martensita. Os resultados foram discutidos em termos da precipitação de Cr23C6, Mo6C, NbC, fase Chi, austenita e ferrita, bem como das consequências do empobrecimento em Cr e Mo, gerados por tais microconstituintes. São propostos três mecanismos para explicar a sensitização: o primeiro é devido a precipitação de Cr23C6, o segundo a precipitação de fase Chi (rica em Cr e Mo) e o terceiro é devido a formação de ferrita durante o revenimento. O melhor desempenho quanto ao GS foi obtido para os revenimentos a 575 °C e 600°C, por 2 horas. Os resultados de Ep indicaram que o aço SM2MoNb, revenido a 575°C, tem o melhor desempenho quanto à resistência à corrosão por cloreto. Isso associado ao baixo GS coloca este aço, com este tratamento térmico, numa posição de destaque para aplicações onde a resistência à corrosão é um critério de seleção de material, uma vez que, segundo a literatura a temperatura de 575 °C está no intervalo de temperaturas de revenimento onde são obtidas as melhores propriedades mecânicas.
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The rheology of 10 Australian honeys was investigated at temperatures -15C to 0C by a strain-controlled rheometer. The honeys exhibited Newtonian behavior irrespective of the temperature, and follow the Cox-Merz rule. G/G' and omega are quadratically related, and the crossover frequencies for liquid to solid transformation and relaxation times were obtained. The composition of the honeys correlates well (r(2) > 0.83) with the viscosity, and with 24 7 data sets (Australian and Greek honeys), the following equation was obtained: mu = 1.41 x 10(-17) exp [-1.20M + 0.01F - 0.0G + (18.6 X 10(3)/T)] The viscosity of the honeys showed a strong dependence on temperature, and four models were examined to describe this. The models gave good fits (r(2) > 0.95), but better fits were obtained for the WLF model using T-g of the honeys and mu(g) = 10(11) Pa.s. The WLF model with its universal values poorly predicted the viscosity, and the implications of the measured rheological behaviors of the honeys in their processing and handling are discussed.
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The preparation and characterization of two new neutral ferric complexes with desolvation-induced discontinuous spin-state transformation above room temperature are reported. The compounds, Fe(Hthpy)(thpy).CH3OH.3H2O (1) and Fe(Hmthpy)(mthpy).2H2O (2), are low-spin (LS) at room temperature and below, whereas their nonsolvated forms are high-spin (HS), exhibiting zero-field splitting. In these complexes, Hthpy, Hmthpy, and thpy, mthpy are the deprotonated forms of pyridoxal thiosemicarbazone and pyridoxal methylthiosemicarbazone, respectively; each is an O,N,S-tridentate ligand. The molecular structures have been determined at 100(1) K using single-crystal X-ray diffraction techniques and resulted in a triclinic system (space group P1) and monoclinic unit cell (space group P21/c) for 1 and 2, respectively. Structures were refined to the final error indices, where RF = 0.0560 for 1 and RF = 0.0522 for 2. The chemical inequivalence of the ligands was clearly established, for the "extra" hydrogen atom on the monodeprotonated ligands (Hthpy, Hmthpy) was found to be bound to the nitrogen of the pyridine ring. The ligands are all of the thiol form; the doubly deprotonated chelates (thpy, mthpy) have C-S bond lengths slightly longer than those of the singly deprotonated forms. There is a three-dimensional network of hydrogen bonds in both compounds. The discontinuous spin-state transformation is accompanied with liberation of solvate molecules. This is evidenced also from DSC analysis. Heat capacity data for the LS and HS phases are tabulated at selected temperatures, the values of the enthalpy and entropy changes connected with the change of spin state were reckoned at DeltaH = 12.5 0.3 kJ mol-1 and DeltaS = 33.3 0.8 J mol-1 K-1, respectively, for 1 and DeltaH = 6.5 0.3 kJ mol-1 and DeltaS = 17.6 0.8 J mol-1 K-1, respectively, for 2
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We report a multi-wavelength Raman spectroscopy study of the structural changes along the thermal annealing pathway of a poly(furfuryl alcohol) (PFA) derived nanoporous carbon (NPC). The Raman spectra were deconvoluted utilizing G, D, D′, A and TPA bands. The appropriateness of these deconvolutions was confirmed via recovery of the correct dispersive behaviours of these bands. It is proposed that the ID/IG ratio is composed of two parts: one associated with the extent of graphitic crystallites (the Tuinstra–Koenig relationship), and a second related to the inter-defect distance. This model was used to successfully determine the variation of the in-plane size and intra-plane defect density along the annealing pathway. It is proposed that the NPC skeleton evolves along the annealing pathway in two stages: below 1600 °C it was dominated by a reduction of in-plane defects with a minor crystallite growth, and above this temperature growth of the crystallites accelerates as the in-plane defect density approaches zero. A significant amount of transpolyacetylene (TPA)-like structures was found to be remaining even at 2400 °C. These may be responsible for resistance to further graphitization of the PFA-based carbon at higher temperatures.
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The behavior of the hydroxyl units of synthetic goethite and its dehydroxylated product hematite was characterized using a combination of Fourier transform infrared (FTIR) spectroscopy and X-ray diffraction (XRD) during the thermal transformation over a temperature range of 180-270 degrees C. Hematite was detected at temperatures above 200 degrees C by XRD while goethite was not observed above 230 degrees C. Five intense OH vibrations at 3212-3194, 1687-1674, 1643-1640, 888-884 and 800-798 cm(-1), and a H2O vibration at 3450-3445 cm(-1) were observed for goethite. The intensity of hydroxyl stretching and bending vibrations decreased with the extent of dehydroxylation of goethite. Infrared absorption bands clearly show the phase transformation between goethite and hematite: in particular. the migration of excess hydroxyl units from goethite to hematite. Two bands at 536-533 and 454-452 cm(-1) are the low wavenumber vibrations of Fe-O in the hematite structure. Band component analysis data of FTIR spectra support the fact that the hydroxyl units mainly affect the a plane in goethite and the equivalent c plane in hematite.