Microsoft Word - 2261 P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 370 Characterization and tensile fractography of nano ZrO2 reinforced Copper-Zinc alloy composites Prasad H. Nayak VTU RRC, Belgaum, Dept. of Mechanical Engineering, Oxford College of Engineering, Bangalore, Karnataka, India Prasadnayak990@gmail.com H. K. Srinivas Dept. of Mechanical Engineering, SJBIT, Bangalore, Karnataka, India Madeva Nagaral Aircraft Research and Design Centre, Hindustan Aeronautics Limited, Bangalore, Karnataka, India madev.nagaral@gmail.com, http://orcid.org/0000-0002-8248-7603 V. Auradi Dept. of Mechanical Engineering, SIT, Tumkur, Karnataka, India vsauradi@gmail.com ABSTRACT. Nano particulates fortified metal lattice composites are finding extensive variety of utilizations in car and sports hardware fabricating businesses. In the present investigation, an endeavor has been made to create copper-zinc-nano ZrO2 particulates strengthened composites by utilizing fluid liquefy technique. 4, 8 and 12 wt. % of nano ZrO2 particulates were added to the Cu-Zn base grid. Microstructural studies were finished by utilizing SEM and EDS examination. Mechanical behavior of Cu-Zn-4, 8, 12 wt. % of nano ZrO2 composites were assessed according to ASTM benchmarks. Checking electron micrographs uncovered the uniform dispersion of nano ZrO2 particulates in the copper zinc composite network. EDS examination affirmed the nearness of Zr and O components in nano ZrO2 strengthened composites. Further, it was noticed that hardness, UTS, yield quality of Cu- Zn composite expanded with the expansion of 4, 8 and 12 wt. % of nano ZrO2 particulates. Ductility of nano composites was decreased by adding zirconium oxide particulates. Fractography of tensile specimens were carried out by using SEM micrographs to understand the failure mechanisms. KEYWORDS. Cu-Zn Alloy; Nano ZrO2 Particulates; Liquid Melt Method; Mechanical Behavior; Fractography. Citation: Prasad, H., N., Srinivas, H, K., Nagaral, M., Auradi, V., Characterization and tensile fractography of nano ZrO2 reinforced copper zinc alloy composites, Frattura ed IntegritàStrutturale, 48 (2019) 370-376. Received: 17.11.2018 Accepted: 21.01.2019 Published: 01.04.2019 Copyright: © 2019 This is an open access article under the terms of the CC-BY 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited. http://www.gruppofrattura.it/VA/48/2261.mp4 P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 371 INTRODUCTION he common name being composition material or simply a composite is combination of two or many materials with non-identical physical and chemical behaviors, when intermixed produces entirely different product with distinct characteristic when compared with the individual material characteristic. The blending of the material is usually done at a macroscopic level. These materials are intermixed in such a ratio that its certain properties get enhanced. The ratios of two materials are optimized based on their applications. These composites are used not only for their improvised mechanical properties, but also for thermal, electrical and environmental applications [1, 2]. These materials are generally preferred for different applications like concretes, reinforced plastics such as fiber reinforced polymers, metal composites, ceramic composites. Ceramic matrix composites & metal matrix composites are generally used for bridges and structure such as boat house, panels of swimming pools, bodies of sports cars, bath tubs, and storage tanks & also advanced materials in spacecrafts & aircrafts building which are in high demand [3, 4]. The composites usually consist of fiber or particulate phase which is stronger & stiffer when compared with the matrix phase. The fiber or particulates commonly known as reinforcement phase have good mechanical, thermal & electrical properties when compared to the matrix phase [5]. Nano Metal Matrix Composites are gradually getting to be distinctly appealing materials for cutting edge aviation applications and yet their properties can be custom-made by the proper chose of reinforcement. Among three different composites, particulate strengthened MMCs as of late discovered unique intrigue on account of their quality and firmness at a normal room and raised temperatures. It is important to note that the properties of the nano metal matrix are unequivocally affected by secondary parameters of the reinforcement, for example, shape, size, introduction, circulation and volume [6]. Among any of other commonly used metals, copper is one characterized by the best thermal conductivity and resistance to corrosion which explains why it is commonly chosen in the first instance for metal material. On the other hand, having very low mechanical properties, it must be strengthened by ceramic particles, for example, which is one of the most reliable methods of reinforcement. Copper based metal lattice composites (CMCs) have discovered more prominent applications in the field of car, air ships and machine apparatus enterprises attributable to their low thickness and associative high wear opposition, quality, consumption obstruction, firmness and warm conductivity. Copper and its combination are to a great extent utilized as a material for heading [7, 8]. Since copper-based materials have a relativity high temperature and low wear obstruction, the copper network has been effectively fortified with nano zirconium oxide and graphite particles, proceeds or irregular strands, called metal matrix composite (MMCs). There is a globally developing attention in assembling clay particulate fortified metal grid materials which forms joined properties of its fortifications and display enhanced physical and tribo-mechanical properties. In the present investigation, copper-10%Zn amalgam-based composites were manufactured by stir process. Nano ZrO2 particulates were utilized as the support. The 4, 8 and 12 wt. level of earthenware production fortifications were taken to create the copper-ZrO2 composites. The composites were tried for mechanical properties like hardness, extreme rigidity, yield quality and rate stretching according to ASTM guidelines. Elements Content wt. % Cu 89.20 Zn 9.90 Others 0.90 Table1: The chemical composition of Cu-Zn alloy EXPERIMENTAL DETAILS he Copper-Zn-nano ZrO2 composites created in this investigation contains 4, 8 and 12 wt. % of artistic nano ZrO2 particulates. The density of copper-zinc compound is 8.737 g/cm3 and that of ZrO2 is 5.68 g/cm3. The density of composites diminishes with expansion of nano ZrO2 particulates. The concoction creation of copper- zinc combination is appeared in the Tab. 1. The fabrication of copper-zinc-ZrO2 composites was carried out by liquid metallurgy route via stir casting technique. The preparation of copper-zinc-nano ZrO2 composites was accomplished by two-stage stir casting technique. Pre-calculated T T P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 372 quantity of Cu-Zn alloy ingots were charged into the heating furnace to liquefy. Though the Cu-Zn alloy melts at 1080˚C, the melting furnace was superheated to a temperature of 1150˚C. Thermocouples were used to measure temperature. The melt metal in crucible was then degassed to remove unwanted byproducts using a chemical called hexa-chloro-ethane (C2Cl6) upto 3 mins. A steel impeller used was coated with a ceramic material known as zirconium which is used to agitate by rotating the molten metal such that the vortex is created. The process of stirring was carried out at a speed of 300 rpm & the impeller was immersed for about 60% height of molten metal from the top surface of melt within the crucible. Simultaneously during the process of stirring the pre-calculated amount of reinforcement was added into the vortex in two-stages, to ensure good wet-ability stirring was continued for upto 5 mins. The reinforcing materials ZrO2 was preheated upto 500˚C in oven to remove moisture content before adding it into molten metal vortex. Now, Cu-Zn alloy along with 4 wt. % ZrO2 particulates were poured into solid cast iron mould to get a composite after solidification. Similarly, Cu-Zn-8 and 12 wt. % of ZrO2 composites were fabricated for the further studies. The microstructural analysis completed by utilizing SEM instrument. Tests around 5 mm thickness across taken from the casting samples and were cleaned appropriately. A reagent named Keller's was utilized to etch the examples. Hardness of as cast copper-zinc-ZrO2 amalgam composites were coordinated to know the influence of nano scale ZrO2 particles in the system material ASTM E 10 standard [11]. The cleaned precedents were striven for their hardness, using Brinell hardness testing machine, which is having a ball indenter and applying a load of 250 kg and tolerate time of 30 seconds, three courses of action of readings were noted at better places of the sample and an average of all the value was used for figuring. The tensile properties of the prepared samples are established as per the ASTM E8 method upon tension test piece of gauge-diameter 9mm with gauge-length of 45mm. Metal & its alloys are to be designed to provide material properties tailored to applications. Universal testing machine (UTM) is used to conduct tensile test to find out the effect of nano ZrO2 particulates on tensile behavior of Cu-Zn alloy composites. RESULTS AND DISCUSSION Microstructural Analysis ig. 1(a) shows microstructure of as cast copper-10% zinc alloy, fig. 1b represents Cu-Zn-12 wt.% of nano ZrO2 composites. The SEM micrographs reveal almost uniform distribution of ZrO2 particulates throughout the matrix as observed in the fig. 1b. Uniformly distributed particulates increase the overall strength and other properties reducing the porosity of the MMC. Fig. 2 is the EDS spectrum of copper-zinc and 12 wt.% of nano ZrO2 reinforced composites. EDS spectrum revealed the presence of nano ZrO2 particles in the copper-zinc alloy matrix in the form of Zr and O elements along with Cu and Zn matrix elements. (a) (b) Figure 1: SEM micrographs of (a) as cast copper-zinc alloy (b) copper-12 wt. % ZrO2 composite F P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 373 Figure 2: EDS spectrum of copper-zinc-12 wt. % ZrO2 composite HARDNESS MEASUREMENTS ardness is a property of a material that demonstrates the capacity of the material to oppose nearby plastic disfigurement. Fig. 3 demonstrates the impact of the nano ZrO2 molecule substance on the hardness of the copper-zinc compound. The hardness esteems are decidedly related with the weight level of nano particles, since particles fortified the lattice. Moreover, the outcomes demonstrate that nano particles fortified MMCs harder than copper- zinc composite because of Hall-Petch and Orowan fortifying components and in addition the great interface between the fortification and framework. Copper-zinc and 12 wt. % nano ZrO2 composites demonstrate more hardness; the expansion in hardness of these composites can be ascribed to the scattering fortifying impact [13]. By including 12 wt. % nano ZrO2 particulates into the copper combination, the hardness of copper amalgam expanded to 85.4 BHN from 126.7 BHN. Figure 3: Showing the hardness of as cast copper-zinc alloy and nano ZrO2 composites TENSILE BEHAVIOR ig. 4 and 5 demonstrating the tensile properties of copper-zinc combination and copper-zinc-4, 8 and 12 wt. % nano ZrO2 composite. Fig. 4 demonstrating the ultimate strength (UTS) of copper-10% zinc compound and ZrO2 composites. Fig. 4 it is apparent that UTS of copper-zinc-ZrO2 composite is much more than the base lattice H F P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 374 combination. By including 3, 8 and 12 wt. % of nano ZrO2 nano particulates to the base amalgam UTS has expanded from 329.7 MPa to 435 MPa. From the fig. 4 it was discovered that yield quality of the copper-zinc base compound is 275.6 MPa and in copper-zinc-12 wt. % nano ZrO2 composite is 356.2 MPa. It demonstrated a change of 29 % in yield quality. The expansion in UTS and YS is essentially because of solid holding between fortification particles and copper-zinc grid, plays an imperative role on the load exchanging from network to support. This is a result of grain refinement and molecule fortifying [14, 15]. The upgrades of quality are influenced by the higher load bearing and confound fortifying caused by nano ZrO2 particles. In contrast with the base copper, the immense improvement in the quality saw in the composites is because of the nearness of the particles as obstructions that confine the movement of separations caught by ZrO2 particulates. This will prompt increment the strength of the nano composites during tests. Fig. 5 demonstrates the elongation of as cast copper-zinc amalgam and its composites. The rate prolongation was lessened in copper-zinc-ZrO2 composite when contrasted with the base combination. It very well may be seen from the diagram that the flexibility of the composites diminishes fundamentally with the 4, 8 and 12 wt. % nano ZrO2 fortified composites. This diminishing in rate prolongation in correlation with the base combinations is a most regularly happening burden in particulate fortified metal lattice composites. The lessened flexibility in copper-zinc-4, 8 and 12 wt. % composites can be ascribed to the nearness of ZrO2 particulates which may get broke and have sharp corners that make the composites inclined to confined break commencement and engendering. The embrittlement impact that happens because of the nearness of the hard-artistic particles causing expanded neighborhood stretch focus destinations may likewise be the reason [16]. Figure 4: Showing the ultimate tensile and yield strength of as cast copper alloy and copper-zinc-4, 8 and 12 wt. % nano ZrO2 composite. Figure 5: Showing the percentage elongation of as cast copper alloy and copper-zinc-4, 8 and 12 wt. % nano ZrO2 composite. FRACTOGRAPHY he study of fractured surface of alloys & its composites becomes necessary to find the cause of failure of the fabricated materials. There are two important things to be remembered during analysis of fractography, a ductile material when fails there is a formation of small dimple like structure in the broken areas whereas in case of brittle fractures there is transgranular (fracture through grains) or inter-granular (fracture through grain boundaries) failures which can be observed in SEM images taken from a failed material. The fractured surfaces of copper-zinc along with 12 wt. % of nano ZrO2 composite resulted from tension tests, are shown in fig. 6 (a-b). Fig. 6a represents the ductility fracture in copper-zinc alloy. SEM analysis of the fractured surfaces shows the dimpled fracture surface for the reinforced & unreinforced material. T P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 375 (a) (b) Figure 6: SEM tensile fractured surfaces of (a) Copper-Zinc alloy (b) Copper-Zinc-12 wt.% of nano ZrO2 composites CONCLUSIONS n this research, by using stir casting fabrication technique the nano ZrO2/Copper-Zinc nano composites have been fabricated by considering 4, 8 and 12 wt. % of reinforcement. The micro-structural analysis, major mechanical behaviors like hardness, ultimate and yield strength, percentage elongation, and fractography behavior of prepared samples are studied as per ASTM standards. The matrix is almost free from pores in as cast alloy and uniformly distributed of nano particles in the prepared composite, which is evident from SEM microphotographs. The EDS analysis confirms the presence of nano ZrO2 particles in the Cu-Zn alloy matrix. Compared to unreinforced material the mechanical properties of Cu-Zn-4, 8 and 12 wt. % nano ZrO2 composite are superior and enhanced. Due to strain localization, the fracture surface of the composite material consists of small voids. REFERENCES [1] Baradeshwaran, A., Elaya Perumal, A. (2014). Study on mechanical and wear properties of Al7075-Al2O3-Graphite hybrid composites, Composites Part:B, 56 , pp. 464-471. [2] Mohsen, (2011). On the role of processing parameters in producing Cu/SiC metal matrix composites via friction stir processing: Investigating microstructure, microhardness, wear andtensile behavior, Materials Characterization, 62, pp. 108-117. [3] Suhas, J, Quadros, D., Vaishak, N. L., (2016). Evaluation and characterization of tensile properties of short coated carbon fiber reinforced aluminium 7075 alloy metal matrix composites via liquid stir casting method, Material Science Research India, 13(2), pp. 66-73. [4] Naher, S., Brabazon, D., Looney, L. (2003). 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