1 Introduction

Structural nanocrystalline (NC) and ultrafine-grained (UFG) metals possess remarkably high strength, but generally suffer from low ductility and toughness.[1,2] The deterioration of ductility and toughness presently limits the use of UFG metals in manufacturing bulk mechanical parts. This is a major barrier to the widespread use of these materials.

In an effort to enhance the ductility and toughness of bulk UFG metals, incorporating coarser grains (CGs) in a UFG matrix has been suggested as a means of overcoming the observed brittle behavior.[36] The motivation was based on the hypothesis that if a small proportion of CG material was added to the UFG matrix, the ductility could be increased with only a small decrement in strength analogous to ductile-phase toughening. Thus, as a simplest case, a bimodal grain size distribution, encompassing both NC and UFG regimes, has been pursued in an attempt to exploit the advantages of both increased strength resulting from grain refinement and retention of substantial ductility resulting from incorporation of ductile CG.

In one recent study, high tensile ductility was achieved in annealed NC Cu with a bimodal grain size in the NC regime.[5] In an earlier study of UFG alloys, Tellkamp et al. reported tensile elongation of over 8 pct in a cryomilled bulk Al alloy without significant loss of strength.[4] The authors suggested that the presence of CG material in the NC or UFG matrix might be responsible for the enhanced ductility. Building on this early work on cryomilled Al alloys, Witkin et al. demonstrated a more feasible method to achieve a bulk bimodal microstructure from cryomilled powder by design.[7] The deliberate blending of unmilled CG powders and cryomilled NC/UFG powders resulted in a bimodal grain structure comprised of a hard UFG matrix with ductile CG inclusions. This powder metallurgical process route to manufacture bimodal structures allows the convenient combination of constituents of different strength and ductility without the compositional differences normally associated with composite materials. Thus, a bimodal Al-7.5Mg consisting of UFG and CG constituents yields balanced mechanical properties that include enhanced yield and ultimate strength and acceptable or superior ductility and toughness compared to conventional grain-sized alloys and UFG metals only.[8]

However, the underlying deformation and fracture mechanisms associated with bulk bimodal metals, which can render them attractive for further design, have not been fully elucidated because of a lack of unambiguous evidence and direct observations in various scale ranges.[6,912] The major difficulty in direct cross-sectional observation of tensile fractures of UFG Al alloys stems from the sample preparation of near-fracture surfaces, which can preserve embedded voids and cracks, for scanning electron microscopy (SEM) and transmission electron microscopy (TEM).[6] In the present study, the surface treatment for SEM and thin foil preparation for cross-sectional TEM are facilitated by focused ion beam (FIB), which preserves embedded voids and cracks for systematic scrutiny. Cross sections of tensile fractures were examined to determine the deformation and failure mechanisms of cryomilled bulk bimodal Al-Mg alloy.

2 Experimental Procedures

The bimodal Al-7.5Mg alloys were produced by mechanical blending of cryomilled UFG powders with 30 vol pct unmilled CG powder in an inert atmosphere to achieve a uniform distribution of unmilled powders. Experimental details on the cryomilling experiments can be found elsewhere.[7,9] For comparison, UFG samples were prepared from 100 vol pct cryomilled powders. The powders used for cryomilling and for unmilled additions were from the same spray-atomized batch. The powder blends were canned and then consolidated by cold isostatic pressing at a pressure of ~400 MPa. The consolidated compacts were vacuum degassed at 673 K. To remove any remaining porosity and improve mechanical properties, the consolidated billets were extruded at 823 K to a round bar 19.05 mm in diameter.

Cylindrical tensile specimens with a gage length of 13.5 mm and a gage diameter of 3 mm were tested on a universal testing machine (Instron 8801, Canton, MA). Uniaxial tensile tests were performed parallel to the extrusion direction at a constant crosshead velocity of 0.012 mm/s until failure, with direct measurement of the displacement of the tensile gage section by a dual-camera video extensometer.

The cross sections of tensile fracture ends were molded and mechanically polished and chemically etched for optical microscopy (OM) observation. The FEI dual beam (FIB) milling on mechanically polished surfaces was used to remove surface oxide and ensure smooth surfaces for SEM observation.

The TEM specimens near tensile fracture surfaces were molded to preserve the fracture surface and cracks and then sectioned with a diamond saw. The thin and small specimens were mechanically polished to a thickness of 2 to 5 μm and bonded to a half-cut TEM slotted grid for FIB milling. Areas of interest beneath fracture surfaces were thinned by FIB milling to prepare electron transparent sections for TEM observation. The TEMs (JEOLFootnote 1 200CX and field emission PHILIPSFootnote 2 CM200) were operated at 200 kV for bright- and dark-field imaging.

3 Results and Discussion

The typical bimodal microstructure of as-extruded cryomilled Al-Mg alloy is shown in Figure 1, which shows OM images and TEM dark-field images along the extrusion and transverse directions. When chemically etched surfaces are viewed normal to the extrusion direction, UFG and CG regions exhibit dark and bright contrast, respectively. The CG regions extend along the extrusion direction and form discrete narrow bands surrounded by the continuous UFG matrix. The individual grains in both CG and UFG regions are evident in the TEM dark-field images. The mean grain sizes of the UFG and CG regions were estimated to be ~100 to 300 nm and 1 μm, respectively. Microhardness measurements performed on the two discrete regions indicated that the UFG region was approximately 2 times harder than the CG regions.[8]

Fig. 1
figure 1

Typical bimodal microstructures of as-extruded Al-Mg alloys with CG30 percent content. Optical micrographs along the (a) extrusion and (b) transverse directions. The bright contrast indicates CG regions. The dark-field TEM images are shown in the (c) extrusion and (d) transverse directions. The CG and ultrafine grain are evident

Figure 2 shows an idealized experimental tensile stress-strain curve for the as-extruded bimodal alloy (30 pct CG), the all-UFG alloy (0 pct CG), and a conventional Al-Mg alloy (100 pct CG).[8] The all-UFG sample showed a high yield strength followed by a brief period of work hardening, but the specimen failed abruptly without necking, as shown in the inset fracture end cross section. It exhibits fully flat (plain strain) fracture and involves a brittle transgranular shear type separation. No delamination cracks perpendicular to the fracture plane are observed. The bimodal Al-Mg alloy with 30 pct CG demonstrated a slightly lower strength and greater ductility, as manifested by the flow-stress plateau after the ultimate tensile strength. Necking occurs in the bimodal 30 pct CG, as shown in the inset of the figure, which indicates more ductile behavior compared to the UFG sample. The fracture surface cross section shows mixed fracture mode: large shear lips with flat central region. Note that the central region of the fracture end of the bimodal sample (30 pct CG) is much flatter than that of the UFG sample, which is jagged. The all-CG specimens exhibited about one-third the ultimate strength of the bimodal samples, but more extensive work hardening and much higher strains than either the UFG or bimodal alloys. The difference between all ultrafine grains, 30 pct CG, and all CGs in the Young’s modulus calculated from the elastic portion of true stress-strain curves is marginal, as expected.

Fig. 2
figure 2

Schematic of uniaxial tensile stress-strain behaviors of bimodal UFG Al alloys compared with all UFG and CG metals. Cross-sectional micrographs of tensile-fractured specimens of CG0 and CG30 percent content. The CG region appears brighter by chemically etched fractures in zoomed-in images. Arrows indicate the extrusion and tensile directions

The strength and ductility values for bimodal alloys were intermediate between those of the UFG and the all-CG materials, representing a balance of both strength and ductility. This suggests that bimodal alloys have unusual deformation and fracture mechanisms arising from the fine-scale combination of hard and soft phases. The deformation and fracture mechanisms warrant further investigation, which is pursued through examination of tensile fractures.

Voids near tensile fractures of bimodal specimens tended to initiate both in UFG regions and in the interfaces between UFG and CG regions. Constrained ductile CG regions within the UFG matrix undergo yielding prior to UFG regions during tensile loading. However, after yielding, CG regions plastically deformed without fracture while the UFG matrix carried most of the tensile load elastically.[10] In contrast, UFG regions plastically deformed very briefly after yielding at a higher stress, because dislocation multiplication over short distances was effectively limited under sufficiently high applied stresses. In terms of load transfer, UFG regions sustained most of the applied stress and only a small part of the load was transferred to the softer CG regions. This phenomenon is analogous to load transfer in fiber-reinforced composites, although in the present case, the stronger phase is continuous. This causes a slight decrease in yield strength of the bimodal specimen. Subsequent to yielding of the UFG matrix, stress concentrations in the UFG regions may be relaxed by void generation and growth and by transferring local loads to the softer CG regions. In addition, stress mismatch between CG and ultrafine grains also increases with the increase of quasi-static load[10,11] and leads to initiation of voids at the UFG-CG interface, as illustrated in the schematic of Figure 3(a). Voids are observed both in the UFG matrix and at the UFG-CG interfaces near fracture surfaces, as shown in Figure 3(b). Fine voids did not appear in the SEM. However, TEM observations (Figure 3(c)) revealed small voids about 50 to 300 nm, similar to the grain size of UFG regions. The cross-sectional TEM sample in Figure 3(d), which was prepared by FIB, shows the preserved voids located in the CG and UFG interfaces.

Fig. 3
figure 3

Void initiation in (a) schematic, (b) SEM, and (c) and (d) TEM images. The TEM samples were prepared by FIB

Cracks were also evident in the UFG matrix between CG bands, and several cracks were apparently arrested by the ductile CG bands. Crack propagation in UFG regions tended to stop at CG regions, and interface voids appeared to coalesce by transgranular-shear type separation and remain in the UFG regions. Ductile CG regions may sustain additional plastic deformation beyond yielding of the UFG matrix, which is the majority constituent by volume. Thus, ductile CG bands effectively blunt propagating crack tips. Figures 4(a) and (b) show a schematic of the crack blunting together with an SEM image of a similarly blunted crack in a UFG region between two CG bands. A similar configuration is shown in the TEM image of Figure 4(c), which reveals blunted cracks in UFG regions, as well as voids. These observations indicate that despite the thin and relatively small volume fraction of CG bands, they effectively inhibit and delay tensile fracture in bimodal specimens. Additional crack configurations are illustrated in Figures 4(d) through (f). Figure 4(d) shows a schematic of a crack that grew into a CG region, branched, and then stopped. A similar crack configuration was observed in the SEM, as shown in Figure 4(e), while an unbranched crack was observed in halt in a CG region, as shown in Figure 4(f).

Fig. 4
figure 4

(a) through (c) Schematic, SEM, and TEM micrographs of crack blunting of UFG at the CG region. (d) through (f) Deflecting and branching of a longitudinal crack in CG. Schematic, SEM, and optical micrographs

Figure 5 illustrates by a schematic drawing a process by which CG bands can bridge cracks and inhibit abrupt fracture. Cracks tend to initiate within UFG regions, while CG regions tend to constrain their growth (Figure 5(a)). This is effectively a ductile-phase toughening mechanism, and such bimodal microstructures can be designed as optimized for structural applications.[1315] Note also that interface delamination between CG and UFG regions perpendicular to the fracture plane is evident in Figures 5(c) and (d). These are regions of severe plastic deformation near tensile fractures, and such delaminations may contribute to the enhanced ductility in bimodal specimen.

Fig. 5
figure 5

(a) and (b) Schematic and SEM images of crack bridging and branching of CG. (c) and (d) Interface delaminating and extensive plastic deformation of CG

In view of observations collected, we propose a descriptive model for tensile deformation and fracture of bimodal UFG metals, as shown in Figure 6. The tensile deformation and fracture stage are described by the four steps in the schematic. First, the CG regions are elongated along the extrusion direction in the as-extruded specimen (Figure 6(a)), and uniaxial tension is applied to the specimen along the extrusion direction. When the stress reaches the yield point of the CG material, plastic deformation occurs within these regions. Second, as the stress increases and reaches the yield point of UFG material, voids initiate within UFG regions and at UFG-CG interfaces, and the CG bands undergo elongation, as shown in Figure 6(b). Third, as the tensile strain increases, cracks grow from the voids and extend transverse to the load axis. However, the cracks tend to be localized in UFG regions between CG regions, as shown in Figure 6(c). Cracks are effectively impeded by the CG stringers, which blunt and bridge the cracks, causing, in some cases, deflection and branching in CG regions and at UFG-CG interfaces. Finally, fracture ensues when cracks link and the CG regions can no longer sustain the load, as shown in Figure 6(d).

Fig. 6
figure 6

Schematic of tensile deformation and fracture mechanism of bimodal UFG Al-Mg alloys under uniaxial tension along the extrusion direction: (a) as extruded, (b) void nucleation and growth, (c) crack growth, and (d) fracture

4 Conclusions

Direct observations in various scale ranges revealed void nucleation and crack behavior in tensile fracture of bimodal Al-Mg alloys. The bimodal grain structures exhibited unusual deformation and fracture mechanisms similar to ductile-phase toughening of brittle materials. Voids initiated and grew in the UFG matrix and at CG-UFG interfaces. The CG bands tended to deform locally at stress concentrations, arresting cracks by local blunting, resisting crack growth by bridging of crack wakes, and impeding crack propagation by deflecting and branching of crack tips and by delamination during plastic deformation.

The present work provides insights for the design of UFG metals resistant to deformation and fracture. Using these observations, single-phase materials with local variations in grain size can be designed to achieve unique combinations of strength, ductility, and toughness. Using this design approach, the deformation mechanisms can be altered by manipulating (a) the morphology and dispersion of the CG phase and (b) the interface properties and by selecting the intrinsic mechanical properties of phases. Single-phase, composite-like materials, because of the perfect CTE match of the constituent phases, may be well suited to high-temperature applications and processing routes. Further work is warranted to optimize bimodal microstructures for mechanical performance and to extend the approach to different multiscale alloys.[16] Dynamic straining experiments employing in-situ observation techniques should provide further insights into deformation and fracture mechanisms of bimodal materials.