METALLURGICAL AND MATERIALS TRANSACTIONS A
ABSTRACTS
Volume 28A, No. 6, June 1997

This Month Featuring: Alloy Phases, Transformations, Mechanical Behavior, Welding & Joining, Solidification, Composite Materials. View June 1997 Contents.

ALLOY PHASES

Study of Inclusions in a Failed Aero-Engine Component
A. TAUQIR, I. SALAM, F.H. HASHMI, and A.Q. KHAN
The cause of the fatigue failure in the retaining ring of the compressor region of an aero-engine turbine was found to be the presence of a high concentration of nonmetallic inclusions. The results of chemical analysis were used to estimate the phases present. The most frequently observed inclusions were spinel solid solutions of the type MO · N2O3, where M = Fe, Mn, or Mg and N = Cr or Al. The detrimental inclusions were corundum, calcium aluminates, cristobalite, and silicates. The most detrimental phases were traced on the surfaces of the specimens fractured using impact loading; the comparison is being made with the polished surfaces and the tensile specimen fracture surfaces. The inclusions in the failed retaining ring were compared with the ones in a similar component obtained from a used engine. In the case of the latter, a large number of fine and elongated (Mn, Cr, Fe)S inclusions were present along with spinels. The nondeformable, rigid oxide particles are considered more undesirable than the sulfides as far as fatigue life of the component is concerned. It has been reported that the presence of sulfides may eliminate the stresses due to oxides.

TRANSFORMATIONS

The Effect of Strontium on the Mg2Si Precipitation Process in 6201 Aluminum Alloy
M.H. MULAZIMOGLU, A. ZALUSKA, F. PARAY, J.E. GRUZLESKI
A transmission electron microscopy (TEM) study of a 6201 aluminum alloy to which controlled strontium additions were made has revealed important differences compared to the same alloy free of strontium. In the as-cast state, strontium favors the formation of -AlFeSi (Al8Fe2Si) rather than -AlFeSi (Al5FeSi) phase, resulting in a greater quantity of excess silicon present in the strontium- treated alloy. During heat treatment, the excess silicon allows a greater density of finer "-Mg2Si precipitates to form, leading to increased tensile strength values and increased electrical resistivity. Strontium also retards the growth of the precipitates formed during heat treatment and inhibits formation of the equilibrium -Mg2Si phase. As a result, the strontium-treated alloy exhibits a resistance to overaging.

MECHANICAL BEHAVIOR

Fatigue Crack Growth through Alloyed Niobium, Nb-Cr2Nb, and Nb-Nb5Si3 In Situ Composites
DAVID L. DAVIDSON
Fatigue cracks were grown through several niobium-based materials. For Nb-Cr-Ti composition materials, the single-phase alloy represented the matrix of two in situ composites with about 22 and 38 vol pct Cr2Nb. Grain boundaries were coated with intermetallic in the lower-volume fraction material, while the 38 vol pct Cr2Nb composite consisted of mainly spherical, dispersed intermetallic. The Nb-10Si composite was composed of about 28 vol pct primary Nb5Si3, with most of the matrix alloy in "fiberlike" shapes due to extrusion. Crack growth rates through the composites were generally faster than for unalloyed Nb, roughly in proportion to the volume fraction of intermetallic, although differences in microstructure make this comparison difficult. The presence of intermetallic greatly alters deformation of material near the crack tip. Particles of Cr2Nb were broken during the crack growth process, leading to increased crack growth rates. These results suggest microstructural modifications that could be expected to enhance fatigue crack growth resistance.

Solidification Structure and Abrasion Resistance of High Chromium White Irons
Ö.N. DOAN, J.A. HAWK, and G. LAIRD II
Superior abrasive wear resistance, combined with relatively low production costs, makes high Cr white cast irons (WCIs) particularly attractive for applications in the grinding, milling, and pumping apparatus used to process hard materials. Hypoeutectic, eutectic, and hypereutectic cast iron compositions, containing either 15 or 26 wt pct chromium, were studied with respect to the macrostructural transitions of the castings, solidification paths, and resulting microstructures when poured with varying superheats. Completely equiaxed macrostructures were produced in thick section castings with slightly hypereutectic compositions. High-stress abrasive wear tests were then performed on the various alloys to examine the influence of both macrostructure and microstructure on wear resistance. Results indicated that the alloys with a primarily austenitic matrix had a higher abrasion resistance than similar alloys with a pearlitic/bainitic matrix. Improvement in abrasion resistance was partially attributed to the ability of the austenite to transform to martensite at the wear surface during the abrasion process.

Modeling Solid Solution Strengthening in Nickel Alloys
H.A. ROTH, C.L. DAVIS, and R.C. THOMSON
The yield stress of multicomponent nickel solid solution alloys has not been modeled in the past with respect to the effects of composition and temperature. There have been investigations of the effect on the yield stress of solutes in binary systems at a fixed temperature, but the effects on the yield stress of multiple solute elements and temperature changes have not been investigated. In this article, two different forms of the trough model are considered for nickel-base alloys to determine the most applicable model for solid solution strengthening in the system. The yield stresses of three binary nickel-chromium and three ternary nickel alloys were determined at a range of temperatures. The yield stress of the alloys was then modeled using the Feltham equation. The constants determined in fitting the Feltham equation to the experimental data were then applied to other experimental solid solution alloys and also to published information on commercial solid solution nickel alloys. It was found that the yield stress of the nickel solid solution alloys could be modeled successfully using the Feltham equation.

Fractal Fracture and Transformation Toughening in CuNiAl Single Crystal
C.H. SHEK, G.M. LIN, J.K.L. LAI, and Z.F. TANG
The fracture toughness JIc() and fractal dimension Df of fractured surfaces of CuNiAl single crystal have been measured at temperatures in the range 20°C to 120°C, in which thermoelastic martensitic transformation takes place. The parent phase has higher fracture toughness than the martensite phase due to stress-induced transformation. The relationship between JIc() and Df has been studied. It was found that log JIc() is linearly related to Df if the failure involves a single mechanism. The slope of the plot may either be positive or negative for brittle or ductile failure, respectively. The difference in the JIc()-Df correlation can be understood in terms of the micromechanism of fracture.

The Entering Behavior of Environmental Gases into the Plastic Zone around Fatigue Crack Tips in Titanium
M. SHIMOJO, R. IGUCHI, T.H. MYEONG, and Y. HIGO
Fatigue crack growth tests were performed on titanium in vacuum, a nitrogen gas, inert gases (helium and argon), and air. Fracture surface morphologies were different from each other even if these environments were mild. Microcracks which were parallel to the striations were observed on the fracture surfaces, and the frequency of them increased with the environment becoming active (He < N2 < Air). These results suggest that the environment has some effects on the deformation behavior in the plastic zone at the crack tip. The concentration of nitrogen in the plastic zone around a crack surface tested in nitrogen was analyzed using electron probe microanalysis (EPMA). The concentration of nitrogen in the plastic zone, especially in the cyclic plastic zone, increased significantly. The result indicates that nitrogen may be adsorbed on the fresh surfaces produced at the crack tip during loading and diffuse into the cyclic plastic zone with cyclic dislocation movement. Considering all the results, it can be thought that atoms of environmental gases including argon, as well as nitrogen, have some effects on the chemical composition of the cyclic plastic zone.

Creep and Low-Cycle Fatigue Behavior of Ferritic Fe-24Cr- 4Al Alloy in the Dynamic Strain Aging Regime: Effect of Aluminum Addition
S.C. TJONG and S.M. ZHU
Creep and low-cycle fatigue behavior of ferritic Fe-24Cr-4Al alloy was studied in the temperature range of 673 to 873 K, where dynamic strain aging (DSA) occurrence was found. The DSA of the alloy manifested in the form of serrated flow, negative strain rate sensitivity, and the peak or plateau in the variations of yield strength (YS) and ultimate tensile strength (UTS) with temperature. The characteristic creep behavior of the alloy was experimentally verified as that for a class I solid solution. However, this ferritic alloy showed an anomalous high stress exponent (n = 5.7) and high activation energy (Qc = 285 kJ/mol) of the secondary creep, which were commonly exhibited by class II solid solutions. During cyclic deformation, the alloy displayed serration in the stress-strain hysteresis loops, increased cyclic hardening, and enhanced planarity of dislocations. On the basis of the observed experimental results and proper analysis, it was proposed that there was strong elastic interaction between solute aluminum atoms and dislocations in the DSA temperature domain. The anomalous creep and fatigue features were interpreted in terms of the interaction of aluminum with the dislocations.

Effects of Microstructure on the Fracture Toughness of Ti3Al-Based Titanium Aluminides
X. WU and P. BOWEN
The influence of microstructure on the fracture toughness of Ti-23Al-9Nb-2Mo-1Zr-1.2Si (at. pct) and Ti-23Al-11Nb-0.9Si (at. pct) Ti3Al-based alloys has been investigated. Basket-weave microstructures comprising different volume fractions of 2 and retained phases were produced by systematic heat treatments. Besides the volume fraction of the retained phase, the average size of the laths has also been used to characterize these microstructures. The toughness of both alloys was examined at room temperature, and the brittle transgranular fracture modes were found to be controlled by microstructure. However, the toughness is not determined solely by the volume fraction of the retained phase, and a linear relationship has been obtained between the fracture toughness and the average size of the retained laths. It appears therefore that the toughness of Ti3Al-based alloys at room temperature is controlled primarily by the width of retained laths rather than by the retained volume fraction.

WELDING & JOINING

Effects of Applied Pressure on the Brazing of Superplastic INCONEL 718 Superalloy
M.S. YEH and T.H. CHUANG
A superplastic INCONEL 718 superalloy was brazed with a Ni-P and a Ni-Cr-P amorphous filler metal. The effects of applied pressure on the bonding strength, microhardness, and corrosion resistance were studied. The results showed that the brazements with Ni-Cr-P filler metal have higher bonding strength and better corrosion resistance than those with Ni-P filler metal using a conventional brazing method without applied pressure. When brazing was conducted under applied pressure, the bonding strength increased with applied pressure for the brazements with both filler metals. This was caused by a decrease of intermetallic phase through ejection of the liquid phase enriched with melting temperature depressants in the molten filler metals from the joint clearance. Corrosion tests show that these brazements failed at the brazed joint and at the grain boundaries in the region adjacent to the brazement.

SOLIDIFICATION

An Analytical Model for Optimal Directional Solidification using Liquid Metal Cooling
T.J. FITZGERALD AND R.F. SINGER
In what follows, a model is developed that describes the optimal processing parameters for directional solidification using liquid metal cooling (LMC). The model considers a sample with a flat geometry and, as a first approximation, can be used to treat the flat sections of a turbine blade. The model predicts (1) the optimal withdrawal rate of the casting from the hot zone, (2) the temperature gradient in the liquid at the solidification interface, and (3) the temperature profile along the length of the casting. The model is then used to perform a sensitivity analysis of the LMC process. Cooling bath temperature, baffle thickness, shell thickness, and shell thermal conductivity are shown to have a strong influence on system performance.

COMPOSITE MATERIALS

Phase Reaction and Diffusion Path of the SiC/Ti System
M. NAKA, J.C. FENG, and J.C. SCHUSTER
Bonding of SiC to SiC was conducted using Ti foil at bonding temperatures from 1373 to 1773 K in vacuum. The total diffusion path between SiC and Ti was investigated in detail at 1673 K using Ti foil with a thickness of 50µm. At a bonding time of 0.3 ks, TiC at the Ti side and a mixture of Ti5Si3Cx and TiC at the SiC side were formed, yielding the structure sequence of -Ti/Ti + TiC/Ti5Si3Cx + TiC/SiC. Furthermore, at the bonding time of 0.9 ks, a Ti5Si3Cx layer phase appeared between SiC and the mixture of Ti5Si3Cx and TiC. Upon the formation of Ti3SiC2 (T phase) after the bonding time of 3.6 ks, the complete diffusion path was observed as follows: -Ti/Ti + TiC/Ti5Si3Cx + TiC/Ti5Si3Cx/Ti3SiC2/SiC. The activation energies for growth of TiC, Ti5Si3Cx, and Ti3SiC2 were 194, 242, and 358 kJ/mol, respectively.

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