The Mechanical Properties of the System and Training Zr59Nb5Cu18Ni8AL10 Bulk Metallic Glasses ()
1. Introduction
Amorphous alloys, also known as metallic glasses, have attracted increasingly intense scientific and technological attention since amorphous metal was first discovered [1]. Due to the lack of defects such as grain boundaries and dislocations, amorphous alloys exhibit extraordinary properties including superior mechanical properties and lower thermal conductivity as well as extreme wear and corrosion resistance. Amorphous alloys are therefore considered to be promising structural as well as functional materials for practical applications. However, the critical cooling rate typically required is above 106 K/s, for retaining the metastable amorphous phase during cooling process. Consequently, the size of the amorphous alloys obtained was limited to thin ribbons, tiny wires and small powders. This strongly restricts the further applications of the amorphization technique.
Since the late 1980s, investigations of multi-component liquid alloys with very deep eutectics have led to the development of metallic glasses with high glass-forming ability (GFA). The development of these metal alloys enables the fabrication of glassy samples with a thickness greater than 1 mm, which is known as bulk metallic glasses (BMGs). This development makes the application of BMGs a step closer to reality. Recently, many kinds of BMGs have been discovered and investigated in various alloy systems such as Fe- [2], Zr- [3,4], Ni- [5,6], Mg- [7], Pd- [8], Ti- [9-11], Cu- [12] based systems. The cooling rate for these BMGs varies in the range of 10−1 to 103 K/s. With a range of differences between the quenching rates of the bulk and ribbon metal glasses, a window of opportunity becomes available for the investigation of glasses with the same composition but produced in various structural states.
The aim of the present work is to study the glass formation behaviour of the Zr59Nb5Cu18Ni8Al10 prepared by the melt-spinning process, in the ribbon shape, and then injected into a copper mould to prepare alloy rods of about 2 mm in diameter. The mechanical properties of the composite have been examined through compression tests and indentation fracture of amorphous alloy is presented.
2. Experimental
An ingot of the Zr59Nb5Cu18Ni8Al10 alloy (composition is given in nominal atomic percentages) was prepared by arc-melting mixtures of Zr 99.99 mass % purity, Ti 99.8 mass % purity, Cu 99.9 mass % purity, Ni 99.9 mass % purity and Al 99.9 mass % purity in an argon atmosphere purified using Nb-gettering. In order to obtain a master alloy, followed by induction melting the master alloy and injection casting into a water-cooled copper mold to form 50 mm long cylinders with diameters of 2 mm. For comparison, thin ribbons of 5 mm width and about 30 µm thickness was prepared using a single-roller, melt spinning technique under a vacuum atmosphere.
All the ribbons and cylinders were investigated by differential scanning calorimetry (DSC) using a constant heating rate of 10˚C/s. The structure of the samples was examined by X-ray diffraction (XRD) with Cu Kα (λ = 1.54056 Å) radiation. Scanning electron microscopy ((JEOL JSM6400F) was employed for the analysis of the fracture features. The compression properties were tested by using an Instron testing machine at a strain rate of 5 × 10−4 s−1 at room temperature.
3. Results and Discussion
Figure 1 shows the constant-rate heating (10˚C/mn) DSC curves of Zr59Nb5Cu18Ni8Al10 analysis was carried out for melt-spun ribbons and as-cast cylinders. In the temperature range investigated, all the curves are characterized by two exothermic peaks, revealing a multi-step crystallization path that does not depend on the way of preparation. The analysis of the thermal stability data, summarized in Table 1, reveals striking similarities between the as-cast cylinders and the melt-spun ribbon.
The DSC curves indicate a small difference in glass transition temperature (Tg), crystallization temperature (Tx), super cooled liquid region (∆Tx = Tx − Tg) between the ribbon and rod samples, for the as cast 2 mm-diameter.
Figure 1. DSC curves of Zr59Nb5Cu18Ni8Al10 alloy ribbon and rods with diameters of 2 mm.
Table 1. Temperature of the glass transition (Tg), onset crystallization peak of the first (Tx1) and the second (Tx2), extension of the supercooled liquid region (∆Tx = Tx1 − Tg) for the melt-spun ribbons and as-cast rod 2 mm respectively.
Cylinder shows that alloy presents two over-lapping exothermic peak around 367 - 601 (˚C). The glass transition temperature, Tg, is 333 (˚C). The melt-spun ribbon for the same alloy presents two exothermic peaks corresponding to two distinct stages of phase transformations Tx1 and Tx2 369, 602 (˚C), respectively and an obvious Tg is 335 (˚C).
Figure 2 shows XRD pattern of the cast Zr59Nb5 Cu18Ni8 Al10 rod with a diameter of 2 mm, together with the XRD pattern of the melt-spun glassy alloy ribbon. Only a broad peak is seen around a diffraction angle of 40˚ for the bulk sample and ribbon, indicating the formation of a glassy phase.
The SEM observation on the fracture surface of broken samples provides insight into the fracture mechanism of the in situ composite. Figure 3 shows the secondary electron images taken for the fractured surface. River patterns predominate in the fracture surface (Figure 3(a)).
The fracture path is basically intergranular (Figure 3(b)), which implies that the remaining glassy phase in between the amorphous grains plays a role in the deformation process. Milman et al. [13] have proposed a parameter defining a plasticity factor for qualifying the brittleness of a material.
Figure 4 shows the compressive stress-strain curve at a strain rate of 5 × 10−4 s−1.The fracture of the samples occurs at a fracture stress σf of 2044 MPa and elastic a deformation up to a strain of about range [1.18%, 1.28%]. Young’s modulus is determined as 165 GPa forthe2 mm diameter sample.