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Materials Research

Print version ISSN 1516-1439

Mat. Res. vol.15 no.6 São Carlos Nov./Dec. 2012 Epub Sep 04, 2012 

Effect of ball to powder weight ratio on the mechanochemical synthesis of MoSi2-TiC nanocomposite powder



Mohamad ZakeriI,*; Mohammad RamezaniII; Ali NazariIII

ICeramic Department, Materials and Energy Research Center, P.O. Box 31787/316, Karaj, Iran
IIYoung Researchers Club, Saveh Branch, Islamic Azad University, Saveh, Iran
IIIDepartment of Materials, Saveh Branch, Islamic Azad University, Saveh, Iran




MoSi2-TiC nanocomposite powders were successfully synthesized with different ball to powder weight ratios (BPR) by ball milling of Mo, Si, Ti and graphite elemental powders. Formation of this composite was studied by X-ray diffraction (XRD). Morphology and microstructure of the milled powders were monitored by scanning and transmission electron microscopy (SEM and TEM), respectively. There was incomplete formation in BPR 5:1 after 30 hours of milling, however, the formation of this composite was completed after 10 hours in BPRs 15:1 and 20:1. Higher BPRs with longer milling time led to partially transformation of β to α MoSi2. Based on Rietveld refinement analysis, and subsequent verification by TEM image, nanostructure powders with the mean grain size less than 25 nm were obtained in all BPRs. Very fine submicron powders in agglomerated ones for BPRs 10:1 and 15:1were obtained at the end of milling.

Keywords: MoSi2-TiC, ball milling, nanostructure



1. Introduction

With the rapid development of aerospace technology, it is urgent to study the new material used in high temperature structural components. MoSi2 intermetallic compound has become an attractive candidate for structural application at temperatures up to 1600 ºC because of its interesting combination of thermo-physical and mechanical properties1,2 such as high strength, ductility and oxidation resistance. Because of its relatively high conductivity, MoSi2 and MoSi2-based materials can be electro-discharge machined. However, it exhibits ceramic-like brittleness at room and metal-like plasticity at elevated temperatures.

The major problem impeding the use of MoSi2 as a high temperature structural material is its brittleness at low temperatures and low strength and creep resistance at temperatures above 1200 ºC. An effective method to solve both of these problems is the addition of brittle or ductile reinforcements as second phase in MoSi2 matrix. MoSi2 is thermodynamically stable with a wide variety of potential ceramic reinforcements for composites, including SiC, Si3N4, ZrO2, Al2O3, TiB2, TiC etc. Its stability extends essentially to the full range of important structural ceramic materials3-10. TiC is another probable reinforcement for MoSi2 with potential advantages: (1) it has a brittle-to-ductile transition above 600 ºC, (2) the thermal expansion coefficient of TiC is virtually same as that of MoSi2, and (3) thermodynamic calculations indicate that TiC and MoSi2 should not react at the temperatures used for densification of MoSi2[11]. Preparation in nanostructure condition is another approach to improve mechanical properties12.

MoSi2-TiC composite can be produced easily by direct mixing of MoSi2 and TiC powders. But the resulting heterogeneous microstructure and high cost of the starting materials are two important drawbacks of this method13-17. Alternatively, MoSi2-TiC nanocomposite powder can be synthesized in situ through high energy reactive milling of a mixture of Mo, Si, Ti and graphite powders. The formation of compounds via solid-state reaction that occurs during ball milling, called mechanical alloying (MA), is a promising way of producing such composites. During MA, both matrix and reinforcement are formed through in situ process, which will promote suitable bonding between matrix and reinforcement. Moreover, a homogeneous distribution of fine reinforcing particles can be obtained by the MA process18-20. There is no report on the synthesis of this composite except of our previous work. In that work MoSi2-30 wt. (%) TiC nanocomposite powder was successfully synthesized by ball milling and following heat treatment. Results showed that the synthesis of this composite begins after 10 hours of milling and progresses gradually up to 30 hours of milling. MoSi2-TiC composite was completely synthesized after annealing of 30 hours milled powder at 900 ºC[21]. Effect of BPR on the mechanochemical synthesis was investigated in the other systems. For example FeAl-Al2O3 composite was formed after 120, 270 and 360 minutes of milling at the BPRs of 5:1, 10:1 and 15:1 respectively. It means that in the higher BPR, the shorter milling time is required for the synthesis22.

The aim of this work is in situ synthesis of MoSi2-TiC nanocomposite powder by mechanical milling of the corresponding elemental powders with different BPRs. Formation of this composite has been studied by thermodynamic discussions and its microstructure has been investigated by Reitveld refinement analysis.


2. Experimental Procedures

MA experiments were performed in a planetary ball mill at approximately room temperature and cup of speed 750 rounds per minute (RPM). The four cup planetary ball mill of Retch Company was used for MA experiments. Pure Merck Mo (99.7 wt. (%), 50 µm), Si (99.8 wt. (%), 25 µm), Ti (99.0 wt. (%), 30 µm) and graphite (99.3 wt. (%), 10 µm) were mixed to give the desired MoSi2-30 wt. (%) TiC composition. Four BPRs of 5:1, 10:1, 15:1 and 20:1 were used. A distribution of 20, 15 and 10 mm stainless steel balls was used in MA experiments. In order to prevent excess agglomeration 1 wt. (%) Stearic acid was added. The powders and balls were charged into a stainless steel cup (250 mL) in an Ar atmosphere. Samples were removed for analysis in a glove box under an Ar atmosphere by interrupting milling at various intervals.

XRD profiles were recorded on a Siemens diffractometer (30 kV and 25 mA) with Cu Kα1 radiation (l.5404 Aº). The Recorded XRD patterns were used for calculation of crystallite size and strain. Mean grain size and microstrain were calculated on the basis of Rietveld refinement method by using of X'Pert high score plus software (developed by PANalytical BV Company, Almelo, the Netherlands, and version 2.2b). In this method, peak profile fitting, size broadening and strain broadening were calculated based on the following equations23.

where Gik is Pseudo-Voigt function, C0 = 2, C1 = 4 ln 2, Hk is full width at half maximum of the Kth brag reflection, Γ is shape parameter, Xik = (2θi - 2θk)/Hk. Di, ηi, λ, U and W are grain size function, strain function, wavelength, strain parameter and size parameter of peak profile, respectively. In the size and strain functions, i and std are referred to analyzed and standard samples, correspondingly. In this project, a pure MoSi2 that annealed at 1500 ºC for 10 hours was used as standard material for deconvolution of instrumental broadening.

Structural observations of milled powders were carried out with a Philips EM208 TEM operating at 200 kV. The powders were ultrasonically dispersed in methanol. One drop of this suspension was placed on a copper grid for TEM observation. The morphology and particle size of samples were examined by using a Philips (XL30) SEM operating at 30 kV. Iron contamination of milled powders was measured by inductivity coupled plasma (ICP) method.


3. Results and Discussions

3.1. Synthesis

Effect of BPR was studied on the formation of MoSi2-TiC composite powders. As received powders including the mixture of Mo, Si, Ti and graphite elemental powders were blended to give the desired MoSi2-30 wt. (%) TiC. Figure 1 shows the XRD patterns of 10 hours milled powders with different BPRs. There is no reaction in BPR 5:1 and the as-received materials reflections can be seen after 10 hours of milling. Graphite reflections were disappeared as a result of large mass absorption coefficient of Mo and Ti in comparison with graphite (Table 1). In fact, the absorption of graphite reflections by Mo and Ti was promoted by the intimate mixing and size decreasing in the early stage of milling24.



With increasing milling energy at BPR 10:1, a partially reaction was performed between the starting materials. However, the strong Mo peak can still be seen in the pattern of this sample. Higher milling energy in BPR 15:1, led to the full reaction and formation of β-MoSi2 and TiC. β-MoSi2 is high temperature polymorph (HTP) and is unstable during room temperature. In fact, high exothermic reactions take place and increase the temperature of the powder particles. This condition favors the formation of the high temperature phase (β-MoSi2 is stable in the temperatures above 1900 ºC)1. Formation of HTP of MoSi2 can be explained as follow; it is now well recognized that the structure and constitution of advanced materials can be better controlled by processing them under non-equilibrium (or far-from-equilibrium) conditions. Amongst many processes, which are in commercial use, MA has been receiving serious attention from researchers. The central underlying technique is to synthesize materials in a non-equilibrium state by energizing and quenching. The energization involves bringing the material into a highly non-equilibrium (meta-stable) state by some external dynamical forcing, such as mechanical energy25. On the basis of above discussion, non-equilibrium condition of milling leads to the formation of HTP of MoSi2 that is unstable at room temperature. The synthesized β-MoSi2 was partially transformed to α-MoSi2 at higher BPR (20:1).

As discussed in Figure 1, formation of MoSi2-TiC composite was completed after 10 hours milling in BPRs 15:1 and 20:1. Two samples with shorter milling times (3.5 and 7 hours) was studied for the determining the exact formation time of this composite. Figure 2a shows there is no reaction in BPR 15:1 after 3.5 hours of milling. On the other hand, in BPR 20:1, some minor MoSi2 was formed at this stage of milling. Increasing milling time to 7 hours in BPR 15, led to the formation of MoSi2 in minor amount (Figure 2b). In the BPR 20:1, at this stage of milling, the intensity of Mo peak was significantly decreased due to the formation of β-MoSi2.

The BPRs 5:1 and 10:1 were compared at longer milling times (20 and 30 hours) due to their incomplete formation of MoSi2-TiC composite. Figure 3a shows some minor amount of starting materials was reacted to form MoSi2 after 20 hours of milling in BPR 5:1. However, in BPR 10:1, the formation of this composite was completed at this stage of milling. Increasing milling time to 30 hours in BPR 5:1, resulted in the considerable formation of MoSi2 and TiC with the remaining of considerable amount of starting materials such as Mo. Longer milling time (30 hours) in BPR 10:1, had no considerable effect except partially transformation of β-MoSi2 to α-MoSi2.

The beginning and completing time for the formation of MoSi2-TiC composite with the end product for all BPRs were summarized in Table 2. With increasing BPR, the beginning time was significantly decreased. Higher BPR led to the higher milling energy. It means that the activation energy for the formation of MoSi2-TiC composite is provided at the shorter milling time. . Higher milling energy also affect the completing time for the formation of this composite. Table 2 shows that the formation of this composite was not completed after 30 hours in BPR 5:1. However, in BPRs 15:1 and 20, this composite was formed after only 10 hours. It means that at higher BPRs, the higher energy per time is introduced to the milled powders. In the other words, the kinetic of MoSi2-TiC formation increases at higher BPRs. The long milling period for the formation of this composite at all BPRs indicates that it was performed in gradual mechanism. The longer milling time (10:1, 30 hours) or higher BPR (20:1, 10 hours) led to the partially transformation of β-MoSi2 to α-MoSi2. It may be due to the activation of recovery mechanism or from the mechanical energy heating. Higher BPR with longer milling time led to the heating of milled powders from mechanical energy. Introducing of this energy to the milled powder promotes the transformation of meta-stable β-MoSi2 to stable α-MoSi2.

3.2. Morphology and Microstructure

Figure 4 shows the morphology and particles size of 30 hours milled powders for all BPRs. In BPR 5:1, very small submicron particles with spherical morphology were obtained after 30 hours of milling (Figure 4a). A few small agglomerated particles can be seen in this sample. Higher BPR (10:1) led to the excessive agglomeration because of higher milling energy. Cold welding and particles fracturing are in competition during milling process. For preventing excess agglomeration, Stearic acid was used as process control agent (PCA). In the lower BPR (5:1), the used PCA acts as surfactant and decreases the cold welding and agglomeration process. At higher BPR (10:1), the added PCA is decomposed due to the formation of MoSi2-TiC composite and its heat releasing. Therefore, there is no inhibitor for cold welding. All of primary particles were agglomerated at this BPR (Figure 4b). With increasing milling energy at higher BPR (15:1), cold working resulted in work hardening and fracturing of milled powders. Figure 4c shows that the amount and size of agglomerates were significantly decreased. These phenomena continue at higher BPR (20:1), so few agglomerates can be seen in this sample (Figure 4d).

Compositions of the milled powders were analyzed by energy dispersive spectroscopy (EDS) that was performed on the marked particles in Figure 4. The results of these analyses were presented in Figure 5. In all BPRs, there are Mo, Si and Ti peaks that confirm the composition of MoSi2 and TiC. As expected, carbon cannot be detected by this method. There is another peak that attributed to Fe in all BPRs. This peak intensity, increases at higher BPRs. Fore confirming the existence of Fe peak, the Fe amount of 30 hours milled powders was measured by ICP method. The results of this measurement were presented in top right corner of each BPR in Figure 5. As seen, the Fe content increases from the minimum value of 0.23 wt. (%) in BPR 5:1 to 8 wt. (%) in BPR 20:1. These results indicate that the higher milling energy led to the higher wearing rate of steel cup and balls. In lower BPRs, this Fe impurity can be neglected due to its minor amount while in higher BPR; it can be removed by conventional leaching methods.

The mean grain size and microstrain of the milled powders were calculated on the basis of Reitveld refinement method (Figure 6). Longer milling time as well as higher BPRs led to the smaller mean grain size (Figure 6a). On the other hands, the milled powders with larger micro strain were obtained at higher BPRs and longer milling times (Figure 6b). As seen in both parameters, a steady state condition was obtained at longer milling time. It means that there is equilibrium between the grain size lessening and recovery mechanisms at longer milling times. In all BPRs and milling times, a nanostructure powders was obtained. The minimum mean grain size acquired for 30 hours-milled powder with 20:1 BPR. The bright field TEM image of 30 hours-milled sample with BPR of 10:1 was shown in Figure 7 due to the complete formation of MoSi2-TiC with the lower Fe impurity. A mean grain size of 12 nm was obtained for this sample by Rietveld method. Figure 7 shows that it is approximately in consistent with the Rietveld result.



4. Conclusions

In this research, the effect of the BPR was studied on the formation of MoSi2-TiC composite powder. Beginning and completing time for the formation of this composite were decreased with increasing BPR. High temperature polymorph of MoSi2 (β) was obtained at higher BPR or longer milling time. The minimum and maximum Fe impurity of 0.23 and 8 wt. (%) were introduced to the 30 hours milled powders with the BPRs of 5:1 and 20:1, respectively. Nanostructure powders with the mean grain size less than 25 nm were obtained in all BPRs that confirmed by TEM image.



1. Schlichting J. Molybdenum disilicide as a component of modern high temperature composites. High Temp-High Pressures. 1978;10(3):241-269.         [ Links ]

2. Meschter PJ and Schwartz DS. Silicide-matrix materials for high temperature applications. JOM. 1989;10(1):52-59.        [ Links ]

3. Jeng YL and Lavernia EJ. Processing of molybdenum disilicide. Journal of Materials Science. 1994;29(1):2557-2571.        [ Links ]

4. Ward CM. Intermetallic-matrix composites. Intermetallics. 1994;4(2):217.         [ Links ]

5. Yang JM, Kai W and Jeng SM. Development of TiC particle-reinforced MoSi2 composite. Scripta Metallurgica. 1989;23(11):1953.        [ Links ]

6. Petrovic JJ. Toughening strategies for MoSi2-based high temperature structural silicides. Intermetallics. 2000;8(11):1175-1182.        [ Links ]

7. Soboyejo W, Brooks D, Chen LC and Lederich R. Transformation toughening and fracture behavior of molybdenum disilicide composites reinforced with partially stabilized zirconia. Journal of the American Ceramic Society. 1995;78(1):1481.        [ Links ]

8. Zakeri M, Yazdani-Rad R, Enayati MH and Rahimipoor MR. Synthesis of MoSi2-Al2O3 nanocomposite by mechanical alloying. Materials Science and Engineering: A. 2006;430(2):185-188.        [ Links ]

9. Yazdani-rad R, Mirvakili SA and Zakeri M. Synthesis of (Mo1-xCrx)Si2 nanostructured powders via mechanical alloying and following heat treatment. Journal of Alloys and Compounds. 2010;489(1):379-383.        [ Links ]

10. Zakeri M and Ahmadi M. Effect of starting composition on the formation of MoSi2-SiC nanocomposite powder via ball milling. Bulletin of Materials Science, 2011. In press.         [ Links ]

11. Vasudevan A and Petrovic JJ. A comparative overview of molybdenum disilicide composites. Materials Science and Engineering: A. 1995:155(1):1.         [ Links ]

12. Takacs L. Combustion Phenomena Induced by Ball Milling. Materials Science Forum, 1998;269-272(1):513-523.        [ Links ]

13. Sun L and Pan J. Fabrication and characterization of TiC-particle-reinforced MoSi2 composites. Journal of the European Ceramic Society. 2002;22(2):791-796.        [ Links ]

14. Sun L and Pan J. TiC whisker-reinforced MoSi2 matrix composites. Materials Letters. 2001;51(1):270-274.        [ Links ]

15. Yuping Z, Xu C and Watanabe T. The effects of carbon addition on the mechanical properties of MoSi2-TiC composites. Ceramics International. 2002;28(1):387-392.        [ Links ]

16. Menga J, Lua J, Wang J and Yang S. Preparation and properties of MoSi2 composites reinforced by TiC, TiCN, and TiB2. Materials Science and Engineering: A. 2005;396(1):277-284.         [ Links ]

17. Sun L, Pan J and Lin C. Wear behavior of TiC-MoSi2 composites. Materials Letters. 2003;57(1):1239-1243.        [ Links ]

18. Koch CC. Structural nanocrystalline materials. Journal of Materials Science. 2007;42(1):1403-14.        [ Links ]

19. Koch CC. Intermetallic matrix composites prepared by mechanical alloying. Materials Science and Engineering: A. 1998;244(1):39-48.        [ Links ]

20. El-Eskandarany MS. Mechanical alloying for fabrication of advanced engineering materials. New York: Noyes Publication;2001.        [ Links ]

21. Zakeri M and Ramezani M. Synthesis of MoSi2-TiC nanocomposite powder via mechanical alloying and subsequent annealing. Ceramics International. 2012;38(1):1353-1357.        [ Links ]

22. Zakeri M, Rahimipour M and Pourhosseini J. In situ formation of FeAl-Al2O3 nanocomposite at different conditions of milling and subsequent annealing. Powder Metallurgy. 2011;54(3):292-298.        [ Links ]

23. Rietveld HM. A profile refinement method for nuclear and magnetic structures. Journal of Applied Crystallography. 1969;2(1):65-71.        [ Links ]

24. Cullity BD. Elements of X-Ray Diffraction. 2nd ed. Addison-Wesley Publishing; 1977.         [ Links ]

25. Suryanarayana C. Non-equilibrium Processing of Materials. Oxford: Pergamon Press; 1999.         [ Links ]



Received: December 10, 2011
Revised: May 29, 2012



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