Titanium carbide, because of its high modulus, high hardness and high melting temperature, is an attractive compound for use as a reinforcing phase in metallic matrices. [1][2][3][4] Amongst the disadvantages are, however, poor mechanical and wear properties which can lead to premature failure of components in service. Alloying can improve these properties but the high elemental additions required significantly decrease the conductivity. [5] Self-propagating high-temperature synthesis (SHS), developed by Merzhanov and Borovinskaya [6] in the late 1960s, is a new kind of method to produce materials. It has been extensively employed for the production of ceramics, [7][8][9] ceramic matrix composites, [10] etc. It has many attractive advantages, such as high purity of products, low processing cost, and energy and time efficiency, no hightemperature furnace process, non-polluting traits, etc. Applying this method, An even dispersion of particulate TiC in an aluminum matrix can be obtained by the SHS reaction between titanium, aluminum and carbon. Thus, many researchers [11][12][13][14][15][16][17][18] have been exerted toward studying the SHS of TiC/Al composites in recent years, According to the literature, [11][12][13][14][15][16][17][18] it can be seen that the combustion-synthesized products of Ti-C-Al system are TiC and Al, during the reaction, there is Ti-Al alloy existing, but the kinds of Ti-Al alloy that they got are different. More detailed experimental observation and a description of the microstructural evolution are still lacking. Therefore, it is necessary to observe more carefully the microstructural evolution and to study further the mechanism of TiC-Al combustion synthesis.The purpose of the present study is to investigate the process of microstructural evolution during Laser igniting selfpropagating high-temperature synthesis of Al/TiC composite from Ti, Al, and C powder mixtures to get a better understanding of the mechanism of the combustion synthesis of Al/TiC composite by combustion front self-extinguished method. On the basis of these experimental results, a mechanism of the combustion synthesis was proposed, and a model corresponding to the mechanism was discussed.
ExperimentalCommercial powders of aluminum (98.0 % purity, 29 lm), titanium (99.5 % purity,15 lm ) and graphite (99.9 % purity, 38 lm) were used for experiments in an atomic ratio of C:Ti=1:1 with 40 wt. % Al. First, the powders were mixed by dry milling with steel balls for 2 h and the blends were pressed into compacted samples. The length of the compact COMMUNICATIONS ADVANCED ENGINEERING MATERIALS 2007, 9, No. 8 Fig. 1. Scheme of combustion synthesis by the LISHS.Fig. 2. XRD pattern of the different combustion zone. (a) Initial reactants zone; (b) Reacting zone; (c) Product zone.