Oxidation of a Commercial Nickel-Based Superalloy under Static Loading

The current demands of the aviation industry for increased gas-turbine efﬁciency necessitate higher turbine entry temperatures, requiring that alloys exhibit superior oxidation resistance. The synergistic effects of oxidation and mechanical stresses pose a complex issue. The purpose of the current research was to examine the effects of stress on the oxidation and oxygen transport in a commercial nickel-based superalloy. Fine grain RR1000 in both polished and shot-peened conditions was studied for classic (zero load) and statically loaded conditions using integrated two-stage isotopic tracing combined with focused-ion-beam secondary ion mass spectrometry (FIB-SIMS). Cr 2 O 3 external oxide formed with semicontinuous TiO 2 above and below. Preferential grain boundary Al 2 O 3 internal oxide formation, c ¢ -dissolution, and recrystallization occurred subsurface. Oxidation mechanisms were dominated by anionic/cat-ionic growth in the external oxide with inward oxygen transport, initially through the partially unprotective external oxide, then along internal oxide/ alloy interfaces. Loading did not inﬂuence the oxidation products formed but did bring about expedited oxidation kinetics and changes to the oxide morphology. The oxygen diffusivity D O * ( 9 10 (cid:2) 13 cm 2 s (cid:2) 1 ) ranged from 0.39 for the polished alloy to 3.7 for the shot-peened condition under compressive stress. Arguably, the most signiﬁcant effects took place in the subsurface regions. Increased oxidation kinetics were attributed to the development of fast cation diffusion paths as the alloy deformed by creep.


INTRODUCTION
Increased turbine entry temperatures (TETs) for improved turbine efficiency push Ni-based superalloys to their operational limits. Higher temperatures require excellent alloy degradation resistance in oxidizing environments to meet the operational service life of the component. Failure to meet this requirement results in excessive oxidation, which reduces the component's ability to maintain its mechanical integrity. The oxidation resistance will depend on the ability of the alloys to form, and maintain, a compact and adherent scale that will protect the alloy from further oxidation attack. 1 Loss of the protective oxide scale becomes problematic as it exposes the parent alloy to further oxidation attack. Stresses in the oxide scale due to intrinsic growth stresses, thermal stresses, or externally applied stresses all increase the likelihood of scale failure. 2,3 The influence of environmental factors on alloy stability at elevated temperatures is now of great importance, in both new alloy design, and those currently in service. The distinct characteristics of the oxide formed and its kinetics depend on several variables, including composition, microstructure, environment, temperature, and surface condition. The surface condition of the alloy plays an important role in its resistance against oxidationinduced damage. 4,5 Shot-peening is a widely used surface treatment primarily sought for its ability to offset high mechanical loads at the surface, but shotpeening effects could be both beneficial and detrimental to an alloy's long-term integrity because the process itself imposes high levels of surface and subsurface deformation.
For disk applications, the composition of the class of nickel-based alloys normally permits the forma-tion of a continuous chromia healing layer beneath the transient oxides that rapidly form from the less noble alloy components. The formation of this layer should prevent further oxidation attack as it acts as a barrier between the metal and the exposure environment; however, further attack can occur at either the oxide/gas or the metal/oxide interfaces, if either the metal cations or oxygen anions penetrate the layer. The latter case is known as internal oxidation and is often the main cause of oxidation failures. 6 In addition to the above, and of particular importance to nickel-based alloys, is the depletion of Ni 3 Al precipitate-forming elements from the alloy to form oxidation products themselves. Consequently, a subsurface depleted zone develops that ultimately weakens the near surface of the alloy and reduces the load bearing cross section of the component. Further consequences of compositional changes in the subsurface include void formation, volume changes, alloy-scale interface stability and phase transformations. Each of these relate to the different rates at which the various components in the alloy oxidize. In addition to this microstructural instability, as the oxide continues to grow, the stress required to crack the oxide decreases, 2,3 and the likelihood of further exposure of the base alloy to the environment increases.
This investigation reveals the oxidation behavior of the fine-grain (FG) polycrystalline nickel superalloy fine grain RR1000 in both the polished shotpeened surface conditions at temperatures in the range 700-800°C both without applied load, termed classic oxidation conditions, and under a static bending load. The oxidation and oxidation-induced microstructural changes have been investigated using several analytical techniques and are discussed using the exposure at 800°C as an illustration in this article. The different methodologies have allowed for quantification and characterization of the governing mechanisms pertaining to the surface and subsurface oxidation processes.

EXPERIMENTAL Alloy
The FG RR1000 material studied was produced via a powder metallurgy route followed by extrusion, forging, and a two-step heat treatment to achieve the desired fine-grained microstructure, c' size and volume fraction. Table I gives the nominal alloy composition (in wt.%) and reveals the various components added to maintain a combination of strength, damage tolerance, and creep resistance. 7 Hardy et al. 7 provided a detailed rationale for each of the elements added and their limitations in the alloy design.

Oxidation Experiments
Exposures made use of a customized isotopic exchange facility, which permitted careful control of the exposure environment. This particular setup facilitated the use of the 18 O 2 isotope in two-stage isotopic exposure experiments. The samples were first exposed in research-grade oxygen (referred to as 16 O 2 ) at pO 2 = 200 mbar. The exchange furnace was reevacuated before introducing the 18 O 2 -enriched oxygen also at pO 2 = 200 mbar. The samples were then quench-cooled in air by rolling off the exchange furnace. Bending oxidation under combined isotopic oxidation conditions used a bespoke bending rig based on a simple bent beam test where the load is applied to the ends of the test sample. All specimens were loaded to a nominal stress of 850 MPa, which is below the yield stress at 800°C. To achieve the desired stress required application of the following relationship: 8 where H is the distance between two ends of the holder required to achieve the desired stress r; L and t are the length and thickness of the specimen, respectively; E(T) is the Young's modulus at temperature T; and k is an empirical constant equal to 1.28. This relationship then states that achieving the desired load requires a measurement of H only. Measurement of H was accomplished using a calibrated digital Vernier caliper with an accuracy of ±0.01 mm. Table II provides the sample dimensions and holder separation as well as the elastic strain as calculated for the 850 MPa applied stress and the Young's modulus for the 800°C exposures.

Characterization
Oxide cross-section preparation, imaging, and focused-ion-beam secondary ion mass spectrometry (FIB-SIMS) used an FEI FIB-200 SIMS workstation (FEI Company, Hillsboro, OR) equipped with a quadrupole detector as described by McPhail. 9 Cross-sectioning applied various milling angles, ranging from 15°to 30°to the surface to produce ramped cross sections of the external oxide (EO) and oxidation-affected zone (OAZ). Note that the OAZ may contain internal oxidation (IO), c¢-dissolution (GPD), and recrystallization (RX). Imaging used a 50-pA gallium primary ion beam current in both ion-induced secondary electron (IISEI) and total positive ion (TPII) modes with at least two cross sections analyzed at each temperature and time.
The SIMS maps were collected for 16 O À and 18 O À isotopes. Mapping used beam currents of 100-300 pA depending on the sample analyzed; at these currents, the beam has a diameter 20-30 nm. A raster of 256 9 221 pixels achieved suitable lateral resolution for all specimens while limiting the beam-induced damage. Samples were also examined in a Zeiss Auriga (Carl Zeiss, Oberkochen, Germany) fitted with an Oxford Instruments SMax 80 EDX detector (Oxford Instruments, Oxfordshire, U.K.) to evaluate the oxide compositions.

Classic Oxidation
Ion imaging provided useful, complementary information from the sectioned samples. Figure 1 shows the typical oxide cross-sectional morphology of polished (Fig. 1a) and shot-peened ( Fig. 1b Fig. 2 presents a schematic diagram showing the features observed in the oxidized samples of FG RR1000. The micrographs demonstrate the similarity in the oxide morphologies produced between the two surface finishes; however, the severity of the oxidation damage incurred after shot-peening increases particularly in the subsurface region.
The external oxide growth observed in both the polished and shot-peened alloys follows that observed for other superalloys of similar compositions tested at equivalent temperatures. [10][11][12][13][14] Energy-dispersive x-ray analyses showed that the overall oxide morphology from the external scale to internal oxides of Cr 2 O 3 /TiO 2 in the outer scale to Al 2 O 3 internally agrees with the expected thermodynamic behavior; however, and in contrast to the thermodynamic predictions, the alloy formed an outer layer of TiO 2 , believed to be at the expense of its oxidation resistance. 14,15 Cationic diffusion is inferred from the known transport mechanisms for Cr 2 O 3 growth 16,17 and from the fact that titanium must diffuse outwards to form above the outer scale. This requires titanium diffusion through the chromia and an adequate solubility of the chromium sublattice.
In support of this, Naoumidis et al. 18 previously reported a solubility of 18% on the chromium sublattice at 1000°C. Although the temperatures are considerably higher than those examined in this article, titanium is still expected to have a large enough solubility to facilitate titanium diffusion to the surface.
FIB-SIMS mapping shows the relative distributions of the 16 O and 18 O species in the oxide cross sections for the image presented in Fig. 1a. The pixel intensities have been normalized to the maximum counts in each array. The 16 O À map following exposure at 800°C for 120 h represents the oxide growth that occurs in the first part of the two-stage exposure (72 h). The maps confirm the existence of the external scale with the internal oxides directly   16,17,21,22 which is consistent with the observations that the Cr 2 O 3 normally grows through outward cationic growth (i.e., p-type behavior). 16 Therefore, the oxide grows through simultaneous countercurrent transport of inwardly diffusing oxygen anions and outwardly diffusing titanium and chromium cations.

Oxidation Under Bending Load
Bending loads do not influence the nature of the oxidation products formed but do cause significant morphological changes in the shot-peened alloy derivative at 800°C. The external bending load induced changes to the oxide morphology in both the polished (Fig. 4) and shot-peened (Fig. 5) samples following exposure at 800°C for 120 h. In the case of the polished sample, for example, Fig. 4a outlines how the external oxides now form subsurface protrusions, consisting largely of Cr 2 O 3 .
As with the samples tested under classic oxidation conditions, shot-peened samples exhibited clear differences in the oxide and near-surface morphology under the influence of an external load compared to the polished samples, with the most notable morphological difference observed in the subsurface of the compressively loaded side of the bending specimen. Concerning the external oxide,   18 O À of the oxide cross section given in Fig. 1a for the polished condition after exposure 800°C for 120 h. Fig. 4 shows that the alloy undergoes more extensive and continuous TiO 2 formation under compressive loads. In the case of the shot-peened alloy (Fig. 5), a continuous oxide layer forms beneath the external oxide but separated from the external oxide by an intermediate internal oxidation/recrystallized layer. This continuous oxide layer forms under both loading conditions at 800°C, but is more extensive under compression (Fig. 5a). The presence of such a layer does not prevent grain boundary internal oxide precipitation deeper into the alloy. Under compressive loads, isolated precipitates connect to the continuous oxide layer by fine ligaments. The tensile-loaded specimen exhibits relatively more extensive internal oxidation below this layer. The 16 O À and 18 O À maps for each surface and loading condition confirm the countercurrent transport mechanism previously described for classic oxidation, with the example of the shot-peened sample given in Fig. 6 (compression) and Fig. 7 (tension). The 18 O À distribution throughout the entirety of the external oxide corroborates the inward oxygen (anionic) diffusion and outward cation diffusion to form the external TiO 2 and Cr 2 O 3 external scale. Anionic diffusion through the bulk alloy itself takes place initially along the grain boundaries of the parent alloy, where the internal oxides nucleate, with the interface of the grain boundary oxides and the parent/recrystallized grains providing a fast diffusion path for oxygen transport in the alloy. As with the unloaded specimens, the enhanced oxygen diffusivity along these interfaces expedites the grain boundary internal oxidation rate. [23][24][25] The overall depth of the scale and internal oxide region did not significantly differ between compression and tension for the shot-peened condition. The 16 O À map for the shot-peened compressive specimen (Fig. 6a), however, reveals a subtle difference in the normalized intensity across the external oxide. This is visualized as a layer of low 16 O À intensity (labelled 1) below a layer of higher 16 O À intensity (labeled 2); the dashed white line defines the interface of these two layers. This boundary coincides with the interface of the rutile and chromia layers seen in Fig. 5b and, therefore, relates to the different secondary ion yields of the chromia and rutile. The 18 O À map (Fig. 6b), however, does not demonstrate this layering. Below the external scale, the internal oxides that reside among the intermediate recrystallized layer demonstrate both 16 O and 18 O enrichment. The continuous layer is also separable into two layers of contrasting 16 O À intensity, where the dashed green line (Fig. 6a) defines the interface of these two regions; however, the region having the higher 16 O À signal (labeled 3) sits above that of lower intensity area. As with the external oxide, the 18 O À distribution (Fig. 6b) does not show this separation in the  continuous layer. The sustained 18 O À signal in the grain boundary internal oxides illustrates the continued oxygen diffusion through the continuous layer. The 16 O À map corresponding to oxidation under tension (Fig. 7a) demonstrates a similar layering in the external oxide (see the dashed white line) but not in the continuous oxide layer. For both surface conditions, this layered structure indicates the temporal evolution of the structure, with the intermediate chromia-rich and TiO 2 layers forming early in the exposure in both cases, with some internal oxides, particularly in the tension side. Internal oxides (Fig. 7b) form predominately in the second stage of the oxidation exposure, with the continuous layer in the compressive region ( Fig. 7b).

Oxygen Tracer Diffusion Coefficient in External Oxide
The oxygen tracer diffusion coefficient D Ã O in the external oxide was evaluated for all oxidation conditions using the 16 O À and 18 O À FIB-SIMS maps. An analysis used the isotopic fraction v of the oxygen isotopes distribution, as this mitigates the spurious variations in signal intensity due to sample topography, localized charging, and instrumen-tal factors. Neglecting the contribution from 17 O À , the isotopic fraction was calculated as: where 16 O À and 18 O À are the 16 O À and 18 O À intensities obtained from the FIB-SIMS maps. The application of Eq. 2 on a pointwise basis produced isotopic fraction (IF) maps, which indicated regions of 18 O enrichment. Because the maps are also m 9 n elemental arrays containing the spatial distribution and the intensities of the 16 O À and 18 O À species, it was possible to compute isotopic enrichment depth profiles (IEDPs). IEDPs were computed using an integrated line scan (ILS) method in MATLAB. This method computes the average of the integrated secondary ion intensity for a line scan width of N pixels at each depth increment x, to give a column vector C(x). Mathematically, this may be represented as: Finally, D O * was estimated by fitting the profiles (using a nonlinear least-squares method) according  to Fick's second law of diffusion for a semi-infinite media with a constant source: 26 where C 0 x ð Þ is the isotopic fraction normalized to the tracer natural isotopic abundance C bg (0.24%), and the tracer gas phase concentration C g (97.0%), x is the distance from the surface, and t 18 is the 18 O 2 exposure time. Figure 8 shows this method applied to the polished alloy oxidized under classical conditions (i.e., Figure 1a and b), giving both the IF map and the fitted isotopic enrichment profile for the external oxide. Table III lists the tracer diffusion coefficients calculated for classical and bending load specimens in both the polished and shot-peened conditions.
The values should be treated as effective diffusion coefficients as they account for both the bulk and grain boundary diffusivities. As shown, the shotpeened specimens consistently show higher diffusivities than the polished specimens. The bending loads appear to have only a small influence on the diffusivities, which increase by less than an order of magnitude for all examples. Importantly, the coefficients here agree with the apparent oxygen diffusion coefficients measured for Cr 2 O 3 scales grown on Ni-30Cr alloys at the same temperature. 17

Oxidation Damage
Depth measurements of the external scale, internal oxide, and c'-depleted/recrystallized region clearly highlighted the stress-related effects during oxidation under compressive and tensile loading. These stress effects do not portray straightforward relationships, and therefore, Table III interprets the load effects in terms of depth enhancement ratios R, the absolute depth increase D, and relative  The subscripts comp. and ten.-applied to R and D-indicate values for compression or tension, respectively. For the relative depth increase (R), the values in parenthesis are the absolute increase (i.e., D ten or D comp ) internal oxide area increase R IOA for both polished and shot-peened specimens. The polished specimens are most affected by the application of either compressive or tensile loads. This applies to all the parameters measured with the GPD/RX exhibiting both the greatest relative ($50% in compression) and absolute depth increases. Compressive loads have the greatest influence on the oxidation damage with relative increases of $50% for all damage parameters with the exception of the IO area where a 76% increase occurs. In contrast, the shot-peened specimens appear to be less influenced by the applied loads. Nearly all of the damage parameters demonstrate an increase less than 10%. Under compression, the internal oxide depth increases only slightly; however, the internal oxide area increases by 34%. Note that this specimen also revealed significant changes in the internal oxide morphology.

DISCUSSION
Induced internal stresses from shot-peening under classic oxidation conditions and external loading of polished samples modify the nature of the external and internal oxides and/or accelerates the oxidation kinetics. The difference in oxide morphologies comes as a surprise given that most of the current literature only reports expedited kinetics. [27][28][29][30][31][32] The isotopic tracer experiments indicated that shot-peening and applied stresses have very little influence on the inward oxygen diffusion, thus eliminating enhancement due to a greater contribution from inward anionic growth. This suggests that the shot-peening and mechanical loads applied to polished samples act to influence the diffusivity of the oxidized solute species (i.e., chromium and titanium) in the parent and recrystallized alloy, [33][34][35] and this is proposed to result from defects induced from creep deformation. This could explain the increased internal oxidation kinetics realized in the polished specimens under load. This appears to contradict much of the literature available (see for example, Refs. 27,36,37 ), which infers the greater penetration depths from stress-assisted grain boundary diffusion. The premise of this argument states that the hydrostatic stress increases the oxygen diffusivity. For example, modeling conducted by Karabela et al. 27,28 described accelerated internal oxidation kinetics by first computing the hydrostatic stress gradient through crystal plasticity modeling and then the oxygen diffusion. The authors successfully rationalized the amplified oxygen penetration depths through this method; however, this analysis did not account for flux of the metallic species and the oxidation processes themselves, which inherently modify the media in which the oxygen diffuses through. Furthermore, the approach itself implies that a compressive stress gradient should have a reverse effect and decrease the inward oxygen flux. Clearly, this is not consistent with the current study as compressive stresses generated increased internal oxidation penetration depths. The increased penetration depths presumably result from enhanced aluminum diffusion in the alloy, like the chromium and titanium to form the surface oxides. In support of this, both compression and tension sides demonstrate relatively higher c'-dissolution/recrystallization depths under load, indicative of an increased aluminum flux toward the internal oxidation front. To maintain internal oxide growth, the oxygen flux would have to equal that of the solute at the precipitation front to maintain the mass balance. SIMS mapping demonstrated a buildup of 18 O at an already established 16 O internal oxide front due to rapid surface diffusion along the internal oxide/alloy interface. Then, it is reasonable to assume that the internal oxidation front is already saturated with oxygen, so the oxygen potential is high enough for continued oxide precipitation. Hence, although the stress may influence the oxygen diffusion, the stresses could have a negligible effect with an already rapid surface diffusion taking place.
In the shot-peened specimens, a very different response occurs under external loads, which reflects the number of competing microstructural processes. The applied stresses did not increase the oxidation kinetics in the polished alloy above those of the shotpeened alloy. Even with defect annihilation in the shot-peened structure, it appears that the overall number defects reaches equilibrium. As such, the shot-peened alloy realizes no further enhancement of the oxidation kinetics at 800°C, but significant morphological changes to the oxide microstructure occur.