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Overview
62 Articles

Published in last 50 years

Related Topics

  • Prior Austenite Grain
  • Prior Austenite Grain
  • Duplex Microstructure
  • Duplex Microstructure
  • Austenite Grain
  • Austenite Grain
  • Equiaxed Grain
  • Equiaxed Grain
  • Lamellar Colonies
  • Lamellar Colonies
  • Lath Martensite
  • Lath Martensite
  • Alpha Grains
  • Alpha Grains
  • Prior Grain
  • Prior Grain

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Nanoindentation mechanical properties on spark plasma sintered 48Ti-48Al-2Cr-2Nb alloy

This study aims to investigate the microstructure, plastic (H) properties, elastic (E) properties, reduced elastic (Er) properties the strain-to-break parameter (H/Er), and the resistance to plastic deformation parameter (H3/Er2) of the Ti-48Al-2Cr-2Nb alloy by use of scanning electron microscopy, nanoindentation and micro-indentation techniques. The results show that the sintering parameters had significant effect on the resulting microstructure. Desirable mechanical properties were obtained with the sample sintered at temperature of 1200 °C, pressure of 50 MPa, holding time of 7.5 min and a heating rate of 50 °C/min which had a near lamellar structure, resulting from the grain boundary pinning effect of the fine equiaxed gamma grains and the impartation of ductility due to the coarsened lamellar colonies. The nano-hardness and elastic modulus were observed to be about 4GPa and 31GPa for the near lamellar microstructure, respectively, with the microhardness of about 4.4GPa. While the duplex and the near gamma microstructures possessed the least nano-hardness (3.65–3.78GPa) and elastic modulus (3.6–29.5GPa) with the exception of sample sintered at temperature of 1150 °C, pressure of 50 MPa, holding time of 7.5 min and a heating rate of 100 °C/min., with nano-hardness and elastic modulus of 4.05GPa and 31.25GPa, respectively, however it had the lowest micro-hardness of 2.7GPa. Furthermore, the ratios H/Er and H3/Er2 values were observed to be greater for the same sample suggesting good wear resistance of the alloy.

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  • Materials Today: Proceedings
  • Oct 22, 2020
  • Mahlatse R Mphahlele + 3
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Effect of Cooling Rate on Microstructure of Rejuvenated Fe-Ni Based Superalloys

Fe-Ni based superalloys have been widely used in land-base gas turbine application. The turbine blade was in service for 50,000 h at high temperature and stresses. When subjected to long-term exposure at high temperature, the microstructure lost its best mechanical properties due to the microstructural instability. The aim of this research is to understand the effect of cooling rate on gamma (γ) grain size and gamma prime (γ’) particle size, morphology, and its volume fraction in rejuvenated Fe-Ni based superalloys. The alloys were solutionized above the γ’ solvus temperature at 1125 °C for 2 h for homogenization and cooling to room temperature at different cooling rates. The alloys were experienced with furnace cooling, air cooling, oil quenching, and water quenching. Microstructural analyses were investigated. Grain size, morphology, volume fraction of γ’ precipitates were investigated. Preliminary mechanical properties such as microhardness was conducted.

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  • Key Engineering Materials
  • Aug 1, 2020
  • Kittawat Srimark + 2
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Enhancing the creep resistance of electron beam melted gamma Ti–48Al–2Cr–2Nb alloy by using two-step heat treatment

Electron beam melted Ti–48Al–2Cr–2Nb alloy has undesirable creep resistance due to a near-gamma structure that is not proper for creep. We aimed to control the microstructure of EBM-built Ti–48Al–2Cr–2Nb using two-step heat treatment to improve the high-temperature (750 °C) creep resistance while also maintaining room-temperature ductility. As a result of two-step heat treatment, heat-treated EBM-built Ti–48Al-2r-2Nb alloy has a nearly lamellar microstructure with a thin lamellar structure and fine equiaxed gamma grains. High-temperature creep resistance was significantly improved after two-step heat treatment by inducing a thin lamellar structure. Room temperature ductility was also maintained even while containing a lamellar structure.

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  • Intermetallics
  • Mar 14, 2020
  • Young-Kyun Kim + 2
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Effects of Heat Treatment on Microstructural Modification of As-Cast Gamma-TiAl Alloy

Effects of normalizing and annealing treatments on the microstructure of Ti-48Al-2Cr-2Nb (at.%) were investigated. Normalizing processes were done at 1385 ± 5 °C in α-phase domain with the heating rate of 10 °C/min, the average cooling rate of 30 °C/min, and the holding times of 5, 10, 15, 20, and 25 min. The annealing process was done at the same temperature and heating rate, the holding time of 15 min, and the average cooling rate of 2 °C/min. Microstructures, phases, and hardness levels were studied by optical and field emission electron microscopic observations, x-ray diffractometry (XRD), and microhardness testing, respectively. Also, crystallographic texture variations were analyzed by means of texture coefficient and XRD results. Experimental results showed a linear direct relationship between treatment time and grain size, up to 15 min. A linear reversed behavior was observed for longer times. The untreated alloy consisted of γ and α2 phases with a columnar morphology with the length of about 300 μm. A near-lamellar microstructure with equiaxed gamma grains, Widmansttaten, and laminar γ + α2 colonies was obtained by the normalizing process. The maximum reduction of the grain size was about 70%, as achieved by normalizing with the 15 min holding time. A texture-free microstructure was acquired by normalizing treatment in comparison with strong texture of the as-cast and annealed alloys.

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  • Journal of Materials Engineering and Performance
  • Apr 26, 2016
  • Mehdi Ahmadi + 2
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Characterization of Plastic Flow Pertinent to the Evolution of Bulk Residual Stress in Powder-Metallurgy, Nickel-Base Superalloys

The plastic-flow behavior which controls the formation of bulk residual stresses during final heat treatment of powder-metallurgy (PM), nickel-base superalloys was quantified using conventional (isothermal) stress-relaxation (SR) tests and a novel approach which simulates concurrent temperature and strain transients during cooling following solution treatment. The concurrent cooling/straining test involves characterization of the thermal compliance of the test sample. In turn, this information is used to program the ram-displacement-vs-time profile to impose a constant plastic strain rate during cooling. To demonstrate the efficacy of the new approach, SR tests (in both tension and compression) and concurrent cooling/tension-straining experiments were performed on two PM superalloys, LSHR and IN-100. The isothermal SR experiments were conducted at a series of temperatures between 1144 K and 1436 K (871 °C and 1163 °C) on samples that had been supersolvus solution treated and cooled slowly or rapidly to produce starting microstructures comprising coarse gamma grains and coarse or fine secondary gamma-prime precipitates, respectively. The concurrent cooling/straining tests comprised supersolvus solution treatment and various combinations of subsequent cooling rate and plastic strain rate. Comparison of flow-stress data from the SR and concurrent cooling/straining tests showed some similarities and some differences which were explained in the context of the size of the gamma-prime precipitates and the evolution of dislocation substructure. The magnitude of the effect of concurrent deformation during cooling on gamma-prime precipitation was also quantified experimentally and theoretically.

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  • Metallurgical and Materials Transactions A
  • Jul 8, 2015
  • S L Semiatin + 4
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Microelectrochemical Investigation of Pit Initiation Site on Austenitic Cast Stainless Steel

Austenitic cast stainless steels are widely used as valves, pumps, and connecting tubes but sometimes suffer from pitting corrosion in chloride-containing environments, such as sea water. The corrosion behavior of cast stainless steels is being studied by immersion tests in acidic FeCl3 solutions; however, electrochemical investigations in near-neutral solutions are need to ascertain the corrosion mechanisms in the actual environments. For austenitic cast stainless steels, the primary ferrite solidification mode is effective for reducing the susceptibility of solidification cracking 1, so that the steels generally contain delta-ferrite phases. In this case, the solidification starts with the formation of primary delta-ferrite, and then the ferrite transforms to gamma-phase (austenite) during cooling. It is known that phosphorus and sulfur segregate at the delta/ gamma grain boundaries, and the segregation tends to cause corrosion, such as intergranular corrosion and pitting. Microelectrochemical techniques are successfully applied to investigate the pit initiation site on stainless steels.2-4 A small electrode area is suitable for studying the initiation site and morphology of corrosion, since the ratio of the dissolution to background currents is relatively high, and the polarization can be stopped at the very beginning of the corrosion processes. In this study, a microelectrochemical approach was applied to elucidating the initiation site of pitting for austenitic cast stainless steels. The effect of grain boundary segregation on pitting was also studied. A 20-kg ingot of austenitic cast stainless steel (0.007%C, 0.81%Si, 0.82%Mn, 0.028%P, <0.001%S, 8.1%Ni, 18.7%Cr, <0.01%Mo, <0.01%Cu, 0.001%Al, 0.0042%N, 0.0029%O was prepared by vacuum induction melting. To eliminate the effects of sensitization and sulfide inclusion on pitting, carbon and sulfur contents were lowered. The volume of delta-ferrite was around 15% at room temperature, and a small amount of Al-Mn oxide inclusion existed. The specimens (15 × 25 × 5 mm blocks) were taken from the center of the ingot and were used as-cast without any heat-treatment. The specimen surface was polished down to 1 μm diamond paste. The potentiodynamic anodic polarization curves were measured in a naturally aerated 0.1 M NaCl solution at 298 K. The electrode area was changed from 0.02 mm2 to 100 mm2. The pitting potential of the steel was 0.35 V (vs. Ag/AgCl, 3.33 M KCl), when the electrode area was 1 cm2. In the macroscopic measurements, the initiation site of pit was not identified, since a large pit with a diameter of ca. 100 μm was generated. The electrode area was then reduced to 0.02 mm2 (ca. 150 μm square); however, no pit was observed even when the electrode area contained the delta/gamma grain boundaries. It was suggested that the initiation sites for pitting were sparsely distributed in the steel. On the basis of the size of the delta-ferrite, the electrode area was adjusted to 1 mm2. Figure 1 shows the anodic polarization curves and the surface appearances of the sites of pitting before and after the polarization. A meta-stable pit was generated. In Fig. 1, the pit was initiated at the oxide inclusion located at the delta/gamma grain boundary. It was confirmed in the separate experiments that the metastable pit was also initiated at the delta/gamma grain boundary at which no inclusion was located. A scanning electron microscope (SEM) and a scanning transmission electron microscope (STEM) equipped with an energy-dispersive X-ray spectroscopy(EDS) system were employed to analyze the phosphorus and sulfur segregation at the grain boundary. Figure 2 exhibits the SEM/STEM images and EDS analysis of the grain boundary at which the metastable pit was initiated (Fig. 1). It was clear that phosphorus and sulfur were segregated at the delta/gamma grain boundary. Figure 3 shows the results of segregation analysis of the delta/gamma grain boundary at which no pit was initiated. No segregation of phosphorus and sulfur was detected in this case. It was clear that the pit initiation sites of austenitic cast stainless steel were the grain boundaries of the delta/gamma phases, and the segregation of phosphorus and sulfur was proven to cause the pit initiation in chloride environments. References; 1. V. Kujanpää, N. Suutala, T. Takalo, and T. Moiso, Weld. Res. Int., 9, 55 (1979). 2. I. Muto, Y. Izumiyama, and N. Hara, J. Electrochem. Soc., 154, C439 (2007). 3. A. Chiba, I. Muto, Y. Sugawara, and N. Hara, J. Electrochem. Soc., 159, C341 (2012). 4. A. Chiba, I. Muto, Y. Sugawara, and N. Hara, J. Electrochem. Soc., 160, C511 (2013). Figure 1

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  • Electrochemical Society Meeting Abstracts
  • Jul 7, 2015
  • Asako Otake + 4
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In situ observation of fatigue crack initiation and propagation behavior of a high-Nb TiAl alloy at 750°C

In this paper, the fatigue crack initiation and propagation behavior of a high-Nb TiAl alloy with nearly lamellar microstructure was studied by in situ scanning electron microscope observation at 750 °C. Dog-bone shaped specimens with a single-edge notch were used in the test. The results showed that the fatigue crack initiated first at the central portion of the notch, and then shifted to the edge portion. As the cycle numbers went on increasing, these cracks joined together and formed a main fatigue crack, which could propagate along the surface of the specimen. During the fatigue crack propagation two or three propagation stages were found depending on the microstructure of the crack tip. When the fatigue crack was parallel to the lamellar laths, it exhibited the rapid, steady and accelerated propagation stages successively, while when the fatigue crack was perpendicular to the lamellar laths, it exhibited only the steady and accelerated propagation stages, with no rapid propagation stage being found. In these different propagation stages the fatigue crack propagation rates were different and depended intensively on the lamellar laths orientation, lamellar colony size, equiaxed gamma grains and peak stress intensity factor K max . Based on the experimental data it was concluded that the fatigue crack initiation lifetime was much longer than the propagation lifetime for the single-edge notched specimens at 750 °C.

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  • Materials Science and Engineering: A
  • Nov 10, 2014
  • Zhang Min + 5
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Evolution of lamellar structure in Ti–47Al–2Nb–2Cr–0.2W alloy sheet

The Ti–47Al–2Nb–2Cr–0.2W alloy sheets were obtained by hot pack rolling. The as-rolled sheet has an inhomogeneous duplex microstructure composed of elongated gamma grains and lamellar colonies. Heat treatments were conducted on the as-rolled sheets. The results show that the microstructures with different sizes and grain boundary morphologies were developed after different heat treatments. A coarse fully lamellar structure can be refined if the heating time, together with the cooling rate, is appropriately controlled. The grain growth exponent is found to be approximately 0.2, and the activation energy of grain boundary migration of the alloy is around 225 kJ/mol.

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  • Transactions of Nonferrous Metals Society of China
  • May 1, 2013
  • Bin Lu + 6
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Plastic Flow and Microstructure Evolution during Thermomechanical Processing of a PM Nickel-Base Superalloy

Plastic flow and microstructure evolution during sub- and supersolvus forging and subsequent supersolvus heat treatment of the powder-metallurgy superalloy LSHR (low-solvus, high-refractory) were investigated to develop an understanding of methods that can be used to obtain a moderately coarse gamma grain size under well-controlled conditions. To this end, isothermal, hot compression tests were conducted over broad ranges of temperature [(1144 K to 1450 K) 871 °C to 1177 °C] and constant true strain rate (0.0005 to 10 s−1). At low temperatures, deformation was generally characterized by flow softening and dynamic recrystallization that led to a decrease in grain size. At high subsolvus temperatures and low strain rates, steady-state flow or flow hardening was observed. These latter behaviors were ascribed to superplastic deformation and microstructure evolution characterized by a constant grain size or concomitant dynamic grain growth, respectively. During supersolvus heat treatment following subsolvus deformation, increases in grain size whose magnitude was a function of the prior deformation conditions were noted. A transition in flow behavior from superplastic to nonsuperplastic and the development during forging at a high subsolvus temperature of a wide (possibly bi- or multimodal) gamma-grain-size distribution having some large grains led to a substantially coarser grain size during supersolvus annealing in comparison to that produced under all other forging conditions.

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  • Metallurgical and Materials Transactions A
  • Mar 6, 2013
  • S L Semiatin + 6
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Microstructure and mechanical properties of Ti–45Al–5.5(Cr,Nb,B,Ta) alloy sintered at different SPS temperatures

TiAl alloy bulk samples with the composition of Ti–45Al–5.5(Cr,Nb,B,Ta) (mole fraction, %) were prepared by high energy mechanical milling and spark plasma sintering (SPS) and then heat treatment. The microstructure and mechanical properties after heat treatment of TiAl alloy prepared by SPS at different temperatures were studied. The results showed that the morphology of high energy mechanically milled powder was irregular and the average grain size was about decades micrometers. X-ray diffraction analysis showed that the mechanically milled powder was composed of two phases of TiAl and Ti3Al. The main phase of TiAl and few phases of Ti3Al and TiB2 were observed in the SPS bulk samples of Ti–45Al–5.5(Cr,Nb,B,Ta) alloy. For samples sintered at 900 °C and 1000 °C, the microstructure was duplex structure with some fine equiaxed gamma grains and thin needly TiB2 phases. With the SPS temperature increasing from 900 °C to 1000 °C, the micro-hardness was changed little, the compression strength increased from 1812 MPa to 2275 MPa and the compression ratio increased from 22.66% to 25.59%. The fractography results showed that the compression fracture transform of the SPS Ti–45Al–5.5(Cr,Nb,B,Ta) alloy was rgranular rupture.

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  • Transactions of Nonferrous Metals Society of China
  • Dec 1, 2012
  • Shu-Long Xiao + 4
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The effect of microstructure on creep behavior of a powder metallurgy (PM) beta gamma alloy

Pre-alloyed beta gamma titanium aluminide powder with a nominal composition of TiAl-2Nb-2Mo (G2) is consolidated by hot isostatic pressing. After consolidation, a step cooled heat treatment is performed to homogenize the material and produce a fully lamellar microstructure. Various aging heat treatments are then performed to form interfacial beta phase precipitates along lamellar interfaces. The step cooled heat treatment produces a relatively fine microstructure with an average lamellar grain size of 40 μm. The aging heat treatments generate beta phase precipitates along lamellar grain boundaries as well as along lamellar interfaces, and result in limited lamellar degradation and grain growth. However, coarse intergranular grains consisting of beta and gamma grains form during aging. Constant load tensile creep tests are performed on step cooled heat treated and aged specimens. Primary creep resistance, generally, improves with aging time, even with interfacial precipitation, and the limited lamellar degradation occurs with aging. However, total creep life of aged samples decreases with aging time. The microstructures of the tested specimens are characterized and related to the creep behaviour of the TiAl-2Nb-2Mo alloy in the un-aged and aged conditions.

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  • Journal of Mechanical Science and Technology
  • Jul 1, 2012
  • D Y Seo + 5
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Microstructure Evolution during Supersolvus Heat Treatment of a Powder Metallurgy Nickel-Base Superalloy

Microstructure evolution during the supersolvus heat treatment of a powder-metallurgy, low-solvus, high-refractory (LSHR) superalloy was established. For this purpose, three lots of LSHR with varying initial carbon/boron composition and thermomechanical history were subjected to a series of short-time (induction) and long-time (furnace) heat treatments followed by scanning electron microscopy/electron backscatter diffraction and quantitative metallography. The size of the (pinned) gamma grains exhibited a limited dependence on heating rate and soak time at peak temperature, and it was generally smaller than the predictions based on the classic Smith-Zener model. The differences were rationalized in terms of stereological and pinning-particle location effects. Observations of limited coarsening of the carbide/boride pinning particles were interpreted in the context of prior experimental observations and a modified Lifshitz-Slyosov-Wagner model applied previously for the coarsening of compound phases in steels.

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  • Metallurgical and Materials Transactions A
  • Jan 6, 2012
  • S L Semiatin + 6
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Disordered bcc γ-phase to δ-phase transformation in Zr-rich U-Zr alloy

The transformation mechanism of hexagonal delta phase from the disordered bcc gamma phase has not been reported before in the Zr-rich U–Zr alloy system. With the help of X-ray diffraction, transmission electron microscopy (TEM) and high-resolution TEM analyses it was shown that the gamma to delta conversion takes place by the lattice collapse mechanism of omega transformation. It was also ascertained that a higher aging temperature or time promotes the growth of all four variants of the delta phase within a parent gamma grain. In addition, ab initio electronic structure calculations showed that the bcc to hexagonal transformation, involving partial ordering of the parent bcc phase followed by (111) plane collapse, is energetically favorable.

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  • Philosophical Magazine
  • Aug 21, 2011
  • C.B Basak + 4
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The Microstructural Evolution of Inconel Alloy 740 During Solution Treatment, Aging, and Exposure at 760 °C

In this study, the microstructural evolution of Inconel alloy 740 during solution treatment and aging was characterized using optical and scanning electron microscopy. During double solution heat treatment, carbon is liberated from the dissolution of MC carbides during the first solution treatment at 1150 °C, and fine MC carbides are precipitated on gamma grain boundaries during the second solution treatment at 1120 °C. Due to the concurrent decrease in carbon solubility and the increase in the contribution of grain boundary diffusion at lower temperatures, the MC carbides on the gamma grain boundaries provide a localized carbon reservoir that aids in M23C6 carbide precipitation on gamma grain boundaries during exposure at 760 °C. The γ′ phase, which is the key strengthening phase in alloy 740, is incorporated into the alloy microstructure during aging at 850 °C. The main source of microstructural instability observed during exposure at 760 °C was the coarsening of the γ′ phase.

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  • Journal of Materials Engineering and Performance
  • Aug 10, 2010
  • Christopher J Cowen + 2
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Why power per unit length of weld does not characterize a weld?

A number of publications have characterized low-alloy steel welds by specifying the power per unit length. This paper uses a 3D numerical model to compute the transient temperature and evolution of the microstructure in six welds with the same weld power per unit length of weld but with different weld powers. The results show that the welds have large differences in their transient temperature field and the fields for phase fractions of gamma, martensite, bainite and ferrite–pearlite phases. Also the gamma phase grain size and hardness profiles are quite different. The reason for the differences is that with high welding speeds, the heat flows primarily in the two-dimensions that are normal to the weld path and cools more slowly near the weld pool than in welds made with low welding speeds where the heat flows in three-dimensions and cools more quickly. However, there is a region in the heat-affected zone farther from the weld pool where the time to cool is higher at lower powers and lower welding speeds. The longer times at higher temperatures causes more growth of gamma grain size. The larger gamma grain size reduces the density of nuclei for the austenite to ferrite transformation and thus more gamma can be present when the martensite start transformation is reached. At low weld powers, the hardened zone is wider, deeper and shorter but the maximum hardness is attained in the highest power welds in the coarse grained heat-affected zone that is primarily a martensite and bainite microstructure. This paper studies the extent to which the ratio of power per unit length of weld is not a unique descriptor of a weld.

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  • Computational Materials Science
  • Feb 24, 2010
  • John Goldak + 2
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High temperature fretting fatigue behavior of IN100

Fretting fatigue behavior of a nickel-base superalloy, IN100, was investigated at 600 °C. Fretting fatigue tests were conducted at various stress levels using cylinder-on-flat contact configuration. Effects of microstructure were also investigated by varying the gamma grain size (3 μm versus 7 μm). Additionally, effects of contact load were studied. Furthermore, plain fatigue tests of IN100 with two microstructures were also conducted. Fretting reduced the strength/life in comparison to those of the plain fatigue almost equally in both microstructures. Increase of contact load reduced the fretting fatigue strength/life. An increase of the gamma grain size decreased the fretting fatigue strength/life of IN100. Fracture surfaces of the 3 μm grain microstructure showed intergranular and tortuous crack path while the 7 μm grain microstructure had transgranular and relatively smoother crack path. Fractographic analysis indicated that the 3 μm grain microstructure had a higher resistance to the fretting fatigue crack nucleation and initiation as well as to the crack growth in comparison to the 7 μm grain microstructure, which was in agreement with the observed plain and fretting fatigue behaviors. Furthermore, plain and fretting fatigue performances improved at 600 °C in comparison to room temperature with both microstructures.

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  • International Journal of Fatigue
  • Feb 1, 2010
  • S Mall + 4
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Effects of microstructure on fretting fatigue behavior of IN100

Fretting fatigue behavior of a nickel-base superalloy, IN100, was investigated at room temperature. Two microstructures of IN100 were tested which varied primarily by the gamma grain size (3 μm versus 7 μm). Fretting fatigue tests were conducted at various stress levels using cylinder-on-flat contact configuration. An increase in the grain size was associated with decrease in the fretting fatigue strength/life of IN100. Microscopic analysis showed that the 3 μm grain microstructure provided a higher microstructural barrier to the fretting fatigue crack nucleation and initiation. On the other hand, the 7 μm grain microstructure had a higher intrinsic crack growth resistance due to the tortuous crack path requiring more energy. These features were in agreement with the plain fatigue where fine microstructures generally provide higher resistance to crack initiation but reduce crack propagation resistance while coarse microstructures have the opposite behavior.

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  • Materials Science and Engineering: A
  • Nov 10, 2009
  • S Mall + 3
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Weldability of Nickel-Free Austenitic Stainless Steel Thin Sheet by Small-Scale Resistance Spot Welding

The feasibility and microstructural development of high-nitrogen-containing nickel-free austenitic stainless steel by small-scale resistance spot welding were studied. Almost fully austenitic cellular microstructure was developed in weld nuggets because the cooling rate of approximately 10 5 Ks � 1 was much faster than that in conventional fusion welding processes. Only a small amount of delta ferrite was formed at the gamma grain boundary in the weld, and chromium nitride precipitation was observed both in the gamma grains and at the grain boundary. No significant defects and sensitization were observed in the weld nugget and in the heat affected zone, respectively, and an adequate joint strength was obtained. [doi:10.2320/matertrans.MRA2008285]

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  • MATERIALS TRANSACTIONS
  • Jan 1, 2008
  • Shinji Fukumoto + 3
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Numerical Model of Solidification Structure Formation in Fe&amp;ndash;C Alloy with Peritectic Transformation

A numerical model was developed for the simulation of structure formation during the solidification of an Fe–C alloy with peritectic transformation. In this model, the front tracking method was used to simulate the dendrite growth of primary δ phase and subsequent peritectic transformation. Diffusion in liquid and solid, mass conservation at the solid/liquid interface and local equilibrium at the solid/liquid interface with consideration of curvature undercooling were solved to determine the positions of the solid/liquid and δ/γ interfaces. A simulation was carried out for the growth of many primary δ dendrites to simulate the formation of initial gamma grain structure. The simulated results showed that the number of the initial gamma grain depends on the nucleation mechanism of gamma phase during peritectic reaction.

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  • ISIJ International
  • Jan 1, 2008
  • Minoru Yamazaki + 3
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Application of Fractional Design of Experiments to the Optimisation of the Hardness and Microstructure of Duplex Cast Rolls

AbstractIn the present paper, the results of a fractional design of experiments (DOE) with 16 experiments for 7 factors and resolution IV are presented. The goal was to identify the active roll manufacturing factors that influence roll barrel hardness after a double tempering treatment, the primary austenite grain size and its volume fraction, and the volume fraction of ledeburite in the outer ring layer of duplex work rolls made of Nihard cast iron. As a primary conclusion, both the total Si percentage and the amount of SiCaMn inoculant added to the ladle were found to have a significant effect on the volume fraction of ledeburite. The statistical analysis also showed that high Si percentages and heavier ring roll layer weights were the significant factors promoting the increase in the size of the gamma grains. High Si contents present in the melt and the addition of SiCaMn as inoculant seem to have a counter effect whereby the volume fraction of stable eutectic gamma increases and the volume fraction of proeutectic gamma decreases, with a positive balance for the sum of these austenites of different origins. Finally, the factors that have an influence on roll barrel hardness are those factors that promote the chill effect, such as low Si content, small amounts of liquid being poured into the mould to build up the outer ring layer, and the use of moulds without insulating sleeves.

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  • Practical Metallography
  • Nov 1, 2007
  • J Asensio-Lozano + 1
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