Inverse segregation in directionally solidified Al-Cu-Ti alloys with equiaxed grains

Directionally solidified Al-4 wt pct Cu-0.2 wt pct Ti alloy ingots with equiaxed structures were analyzed for solute distribution. Inverse segregation was found to exist, and the extent of segregation in the first 50 pct of the ingot solidified agreed well with that calculated from inverse segregation theory based on the flowback of enriched liquid. However, at higher points in the ingot, the solute distribution deviated from the theoretical one. Also, more and bigger shrinkage pores existed in the equiaxed grained ingot than in a columnar grained ingot. It is suggested that the formation of randomly distributed, equiaxed grains restricts the flowback of enriched interdendritic liquid much more than the formation of columnar grains where interdendritic channels exist. In an equiaxed grained ingot solidified vertically from the bottom upward, the hydrostatic pressure becomes insufficient to cause complete flowback of enriched liquid in the latter stages of solidification. This effect causes porosity in the ingot and a solute distribution which deviates from that predicted by the theory of inverse segregation.     

Electrical conductivity in directionally solidified lead-9 and -20 wt pct copper alloys

Composites consisting of aligned copper dendrites in a lead matrix have been produced by directional solidification processing for potential application as grids in lead-acid batteries. To promote a uniform composite of aligned copper dendrites in a protective lead matrix, two alloy compositions, Pb-9 and -20 wt pct Cu, have been directionally solidified through a temperature gradient,G _l of 4.5 Kmm^-1 at constant growth velocities which ranged from 1 to 100 μm s^-1. With slow growth rates (≲10 μm s^-1 ), the copper dendrites were generally columnar and continuous along the sample length; at higher velocities (≳60 μm s^-1), they assumed an intricate and equiaxed morphology. In accordance with copper content and growth rate, the electrical conductivity of the directionally solidified composites was found to be as much as a 2.5 times that of pure lead. The results are compared with that predicted by a model based on a geometrical dendrite. Formerly Doctoral Student, Department of Materials Science and Engineering, Vanderbilt University.Seoul Korea. This paper is based on work leading to the successful completion of his Ph.D. degree at Vanderbilt University.     

Evolution of microstructure and tensile strength of rapidly solidified Al-4.7 pct Zn-2.5 pct Mg-0.25 pct Zr-X wt pct Mn alloys

Analytical transmission electron microscopy and thermal analysis of as-extruded Al-4.7 pct Zn-2.5 pct Mg-0.2 pct Zr-X wt pct Mn alloys, with Mn contents ranging from 0.5 to 2.5 wt pct, were carried out to elucidate the microstructural change and accompanying mechanical properties during subsequent heat treatments. The as-extruded alloy was fabricated from rapidly solidified powder and consisted of a fine, metastable manganese dispersoid and the ternary eutectic T phase (Al₂Mg₃Zn₃). Solution heat treatment resulted in the formation of the stable Al₆Mn phase and complete dissolution of the T phase. Formation of stable Al₆Mn was made by two routes: by phase transition from metastable Mn dispersoids which already existed, and from the supersaturated solid solution by homogeneous nucleation. The density of the Al₆Mn phase increased with the addition of manganese, while the shape and average size remained unchanged. A significant increase in the hardness was observed to coincide with the formation of the Al₆Mn phase. Similarly, the tensile strength increased further after the aging treatment, and the increment was constant over the content of Mn in the alloy, which was explained by the contribution from the same amount of precipitates, MgZn₂. Results of thermal analysis indicated that the dissolution of the T phase started near 180 °C and that formation of Al₆Mn occurred at about 400 °C, suggesting that further enhancement of strength is possible with the modification of the heat-treatment schedule.     

The unidirectional solidification of Al-4 wt pct Cu ingots in microgravity

Three Al-4 wt pct Cu alloy ingots, 10 mm in diameter and 25-mm long, were unidirectionally solidified in microgravity during the flight of a sounding rocket, with solidification rates of about 1.6×10⁻⁴ m/s and temperature gradients of about 2600 K/m. The apparatus was comprised of three muffle furnaces, which melted the ingots prior to the launch of the rocket. Unidirectional solidification of the ingots was accomplished by chill plates attached to the furnaces, which were withdrawn from the ingots during the microgravity portion of the flight, bringing the chill plates into contact with the bases of the capsules containing the ingots. Solidification was complete in less than 4 minutes. For comparison, several ground-based ingots were solidified in unit gravity under similar conditions. Metallographic analysis of the solidified ingots showed that the macrostructures of the unit-gravity and microgravity ingots were similar, all exhibiting columnar grains. However, the microstructures were significantly different, with the microgravity ingots exhibiting primary dendrite spacings about 40 pct larger than the unit-gravity ingots and secondary dendrite arm spacings about 85 pct larger. The larger dendrite spacings for the ingots solidified in microgravity are explained by lower dendrite growth velocities. The absence of convective mixing in the microgravity ingots slightly increased temperature gradients in the liquid portion of the alloy during solidification, which resulted in decreased growth velocities. K.N. TANDON, formerly Associate Professor, Materials Engineering Laboratory, Department of Mechanical and Industrial Engineering, University of Manitoba     

Tensile properties of directionally solidified Al-Si eutectic

Al-Si eutectic alloys have been directionally solidified in a horizontal resistance heated furnace. The temperature gradient, G, ahead of the solid/liquid interface was kept fairly constant at 80°c/cm, while the growth rate,R, was varied between 0.28 and 131 μm/s. Microstructural studies show a definite alignment of the rod-like Si at low growth rates. At growth rates higher than 14 /μm/s the microstructures appear irregular, although some preferential orientation of the Si rods parallel to the growth direction can be observed. Tensile tests show higher values in both yield and ultimate strengths than was found in previous investigations, most likely due to the careful sample preparation prior to testing in the present work. The yield strength increases with the growth rate up to about 14 /μm/s, and only a slight increase is observed at higher rates. The ultimate strength also increases with the growth rate, but shows less tendency toward saturation. Superposition of hardness and yield data show excellent correlation, while comparison between hardness and ultimate strength shows higher hardness than ultimate values with decreasing growth rates. Formerly Metallurgist with Materials and Molecular Research Division, Lawrence Berkeley Laboratory.     

The anisotropy of Al-4 wt pct Cu single crystals tested in plane-strain compression

Plane-strain compression tests were made on Al-4 wt pct Cu single crystals of various orientations in solution-treated and overaged conditions. Shear stress-shear strain curves were constructed using the appropriate Taylor factors, corrected for lattice rotation and observed lateral spreading. These results are compared with data from an earlier study on crystals of the same alloy aged to produce θ′. The anisotropy of the shear stress-shear strain curves was found to be the greatest in the normally aged material (θ′) and the least in the overaged material (θ). Suphal P. Agrawal was formerly Post-Doctoral Research Associate     

An analysis of the microstructure of rapidly solidified Al-8 wt pct Fe powder

Rapidly solidified powders of Al-8 wt pct Fe exhibit four distinct microstructures with increasing particle diameter in the size range of 5 μm to 45 μm: microcellular α-Al; cellular α-Al; a-Al + Al₆Fe eutectic; and Al₃Fe primary intermetallic structure. Small powder particles (~10 μm or less) undercool significantly prior to solidification and typically exhibit a two-zone microcellular-cellular structure in individual powder particles. In the two-zone microstructure, there is a transition from solidification dominated by internal heat flow during recalescence with high growth rates (microcellular) to solidification dominated by external heat flow and slower growth rates (cellular). The origin of the two-zone microstructure from an initially cellular or dendritic structure is interpreted on the basis of growth controlled primarily by solute redistribution. Larger particles experience little or no initial undercooling prior to solidification and do not exhibit the two-zone structure. The larger particles contain cellular, eutectic, or primary intermetallic structures that are consistent with growth rates controlled by heat extraction through the particle surface (external heat flow).     

Microstructure and corrosion behavior of as-cast and heat-treated Al-4.5 Wt pct Cu-2.0 wt pct Mn alloys

The microstructure and corrosion behavior of as-cast and heat-treated Al-4.5 pct Cu-2.0 pct Mn alloy specimens solidified at various cooling rates were investigated. The equilibrium phases Al₆Mn and θ-Al₂Cu, which are observed in the conventionally solidified alloy in the as-cast condition, were not detected in rapidly solidified (melt-spun) material. Instead, the ternary compound Al₂₀Cu₂Mn₃ was present in addition to the α phase, which was present in all cases. The morphological and kinetic nature of corrosion was investigated metallographically and through potentiostatic techniques in 3.5 wt pct NaCl aqueous solution. Corrosion of the as-cast material was described by two anodic reactions: corrosion of the intermetallic phases and pitting of the α-Al solid solution. The corrosion rate increased with cooling rate from that for the furnace-cooled alloy to that for the copper mold-cast alloy and, subsequently, decreased in the rapidly solidified alloy. In the heat-treated material, corrosion could be described by two anodic reactions: corrosion of Al₂₀Cu₂Mn₃ precipitate particles and pitting of the α-Al matrix. S.M. Skolianos, formerly Graduate Student, Department of Metallurgy, University of Connecticut     

The quench sensitivity of cast Al-7 wt pct Si-0.4 wt pct Mg alloy

The effect of quenching condition on the mechanical properties of an A356 (Al-7 wt pct Si-0.4 wt pct Mg) casting alloy has been studied using a combination of mechanical testing, differential scanning calorimetry (DSC), and transmission electron microscopy (TEM). As the quench rate decreases from 250 °C/s to 0.5 °C/s, the ultimate tensile strength (UTS) and yield strength decrease by approximately 27 and 33 pct, respectively. The ductility also decreases with decreasing quench rate. It appears that with the peak-aged condition, both the UTS and yield strength are a logarithmic function of the quench rate,i.e., UTS orσ _y =A logR +B. The termA is a measure of quench sensitivity. For both UTS and yield strength of the peak-aged A356 alloy,A is approximately 32 to 33 MPa/log (°C/s). The peak-aged A356 alloy is more quench sensitive than the aluminum alloy 6063. For 6063,A is approximately 10 MPa/log (°C/s). The higher quench sensitivity of A356 is probably due to the high level of excess Si. A lower quench rate results in a lower level of solute supersaturation in the α-Al matrix and a decreased amount of excess Si in the matrix after quenching. Both of these mechanisms play important roles in causing the decrease in the strength of the peak-aged A356 with decreasing the quench rate.     

Microstructural and compositional transients during accelerated directional solidification of Al-4.5 wt pct Cu

The transient behavior of mushy-zone velocities, primary dendrite arm spacings, and microsegregation effects have been investigated for an Al-4.5 wt pct Cu alloy by instantaneous velocity changes in a standard Bridgman furnace. After suddenly imposed velocity changes, the mushy-zone velocities, dendrite arm spacings, and compositions exponentially adjust to new steady-state values. Good agreement was found between the transient mushy-zone positions and velocities and predictions from the theoretical model of Saitou and Hirata. The primary dendrite arm spacings appear to adjust to changed velocity conditions about as rapidly as the mushy-zone velocity adjusts. Steady-state arm spacings agree very well with corresponding steady-state data from the literature. However, the observed composition profiles in the dendrite core and the interdendritic liquid appear to adjust more slowly than the corresponding adjustment of the mushy-zone velocity and arm spacings. Our observation of the sluggish response of the compositional profiles is consistent with an estimated Lewis number of 9.4 × 10³ for the aluminum-copper system. The diffusivity of heat, thus, greatly exceeds the diffusivity of solute in this system. These results indicate that testing for the steady state during directional solidification experiments by looking for constant primary dendrite arm spacings can lead to errors, since the microsegregation profiles adjust more slowly than the spacings. It is suggested that constancy of composition also be tested for critical experiments investigating steady-state microsegregation effects.     

Fatigue crack growth rates and fracture toughness of rapidly solidified Al-8.5 pct Fe-1.2 pct V-1.7 pct Si alloys

The room-temperature fatigue crack growth rates (FCGR) and fracture toughness were evaluated for different crack plane orientations of an Al-8.5 Pct Fe-1.2 Pct V-1.7 Pct Si alloy produced by planar flow casting (PFC) and atomized melt deposition (AMD) processes. For the alloy produced by the PFC process, properties were determined in six different orientations, including the short transverse directions S-T and S-L. Diffusion bonding and adhesive bonding methods were used to prepare specimens for determining FCGR and fracture toughness in the short transverse direction. Interparticle boundaries control fracture properties in the alloy produced by PFC. Fracture toughness of the PFC alloy varies from 13.4 MPa√m to 30.8 MPa√m, depending on the orientation of the crack plane relative to the interparticle boundaries. Fatigue crack growth resistance and fracture toughness are greater in the L-T, L-S, and T-S directions than in the T-L, S-T, and S-L orientations. The alloy produced by AMD does not exhibit anisotropy in fracture toughness and fatigue crack growth resistance in the as-deposited condition or in the extruded condition. The fracture toughness varies from 17.2 MPa√m to 18.5 MPa√m for the as-deposited condition and from 19.8 MPa√m to 21.0 MPa√m for the extruded condition. Fracture properties are controlled by intrinsic factors in the alloy produced by AMD. Fatigue crack growth rates of the AMD alloy are comparable to those of the PFC alloy in the L-T orientation. The crack propagation modes were studied by optical metallographic examination of crack-microstructure interactions and scanning electron microscopy of the fracture surfaces.     

Substructure and dispersion hardening in aged,cold worked,and annealed Al-4 wt pct Cu alloy

Electron microscopy and X-ray line profile analyses have been employed to define the microstructures and substructures of pure aluminum and an overaged Al-4 wt pct Cu alloy after various thermomechanical treatments. Tensile tests were performed on the same materials, and the results have been interpreted in terms of structure. A given cold rolling reduction of the aged Al-4 wt pct Cu alloy produced a much higher dislocation density and a less cellular substructure than the same treatment produced in pure aluminum of comparable initial grain size. Annealing after cold work produced similar responses in both the pure metal and the alloy. For the aged alloy in the as-rolled, or rolled-and-annealed condition, dispersion strengthening and substructure strengthening were found to be linearly additive, and they accounted for virtually all the observed tensile yield strength. Substructure strengthening has been discussed in terms of the relation between dislocation density and the spacing and nature of the substructure boundaries.     

Elevated temperature deformation behavior of an Al-8.4 wt pct Fe-3.6 wt pct Ce alloy

The elevated temperature deformation characteristics of a rapidly solidified Al-8.4 wt pct Fe-3.6 wt pct Ce alloy have been investigated. Constant true strain rate compression tests were performed between 523 and 823 K at strain rates ranging from 10⁻⁶ to 10⁻³ s⁻¹. At temperatures below approximately 723 K, the alloy is significantly stronger than oxide dispersion strengthened (ODS) aluminum. However, at higher temperatures, the strength of the Al-Fe-Ce alloy falls rapidly with increasing temperature while ODS aluminum exhibits an apparent threshold stress. It is shown that particle coarsening cannot fully account for the reduction in strength of the Al-Fe-Ce alloy at elevated temperatures. The true activation energy for deformation of the Al-Fe-Ce alloy at temperatures between 723 and 773 K is significantly greater than that for self-diffusion in the matrix. This is unlike the behavior of ODS alloys, which contain nondeformable particles and exhibit true activation energies close to that for self-diffusion in the matrix. Since abnormally high true activation energies for deformation are also exhibited by materials containing deformable particles, such as γ^′ strengthened superalloys, it is concluded that elevated temperature deformation in ythe Al-Fe-Ce alloy involves deformation of both the matrix and the precipitates. The loss of strength of the Al-Fe-Ce alloy appears to be related to a reduction in strength of at least some of the second phase particles at temperatures above 723 K. Formerly Research Assistant, Department of Materials Science and Engineering, Stanford University.     

Prevention of macrosegregation in squeeze casting of an Al-4.5 wt pct Cu alloy

The squeeze casting of an Al-4.5 wt pct Cu alloy was carried out to investigate the conditions for the formation and the prevention of macrosegregation. The effects of the process parameters, applied pressure, die temperature, pouring temperature, delay time, and humidity on the formation of macrosegregation were investigated in correlation with the evolution of macrostructure and shrinkage defects. Two critical applied pressures were defined: one is the critical applied pressure, P _SC , under which shrinkage defects form, and the other is the critical applied pressure, P _MS , above which macrosegregates form in the squeeze castings. A quantitative diagram describing the optimum process conditions was proposed for obtaining sound squeeze castings. It was found that the pouring temperature, the die temperature, the delay time, and the humidity are closely related to the two critical applied pressures P _SC and P _MS , in different manners. It was concluded that sound castings without macrosegregation and shrinkage defects can only be obtained when the applied pressure is in the range of P _SC <P<P _MS .     

A structural investigation of multiple aging of Al-7 wt pct Zn-2.3 wt pct Mg

A transmission electron microscopy study of the structural changes which attend aging at 180°C with and without pre-aging at 100°C was conducted on a high purity aluminum alloy containing 6.8 pct Zn and 2.3 pct Mg. The refinement in precipitate dispersion accompanying multiple aging is caused by the operation of aging sequences which differ from those occurring in material given the single age at 180°C only. The high nucleation rate which occurs during the low temperature pre-aging treatment is responsible for the observed precipitate refinement. The results of this investigation appear to agree favorably with the Pashleyet al. model of multiple aging.     

Defects formed during quenching in Al-4 pct Cu

Thin foils of Al-4 pct Cu alloys were examined by transmission electron microscopy in the as-quenched and the aged states in an attempt to clarify the mechanism of the prolonged low-temperature aging phenomenon in these alloys known as the slow reaction. The asquenched microstructure is found to consist of bands of vacancy clusters or small dislocation loops with helical dislocations sometimes associated with them. It is postulated that these defects are formed by the interaction of vacancy agglomerates and dislocations during the quench. The contrast images associated with the defects are found to vary in radius from approximately 15 to 85 Â, and in density roughly from 1 to 5 x 10¹⁵/cm³. These results are consistent with the calculations of Okamoto and Kimura, who showed that the slow reaction could best be explained as being caused by supersaturated vacancies in equilibrium with the surface tension of defects of this size. As the slow reaction proceeds, these vacancies are annihilated at permanent sinks, and this disturbance of equilibrium causes the defects to emit vacancies and, hence, shrink and disappear completely in the aged state.     

Mechanical properties and fracture behavior of an ultrafine-grained Al-20 wt pct Si alloy

The effect of powder particle size on the microstructure, mechanical properties, and fracture behavior of Al-20 wt pct Si alloy powders was studied in both the gas-atomized and extruded conditions. The microstructure of the as-atomized powders consisted of fine Si particles and that of the extruded bars showed a homogeneous distribution of fine eutectic Si and primary Si particles embedded in the Al matrix. The grain size of fcc-Al varied from 150 to 600 nm and the size of the eutectic Si and primary Si was about 100 to 200 nm in the extruded bars. The room-temperature tensile strength of the alloy with a powder size <26 μm was 322 MPa, while for the coarser powder (45 to 106 μm), it was 230 MPa. The tensile strength of the extruded bar from the fine powder (<26 μm) was also higher than that of the Al-20 wt pct Si-3 wt pet Fe (powder size: 60 to 120 μm) alloys. With decreasing powder size from 45 to 106 μm to <26 μm, the specific wear of all the alloys decreased significantly at all sliding speeds due to the higher strength achieved by ultrafine-grained constituent phases. The thickness of the deformed layer of the alloy from the coarse powder (10 μm at 3.5 m/s) was larger on the worm surface in comparison to the bars from the fine powders (5 μm at 3.5 m/s), attributed to the lower strength of the bars with coarse powders.