Compounds made of titanium diboride (TiB₂) particles and aluminum substrate (TiB₂/Al7175 metal matrix composites (MMCs)) produced in-situ have certain remarkable features that enable these highly potential materials to be excellent performance aviation blades. Machinability remains an issue attributable to the effect of TiB₂ particulate, limiting the applicability of TiB₂/Al7175 MMCs. For suit manufacturing demands, the effect of TiB₂ particulate upon its processing parameters for TiB₂/Al7175 MMCs was successfully examined. This investigation also looked into the best processing parameters for these types of MMCs. There are various factors to consider. The surface’s roughness and the amount of material removed (Material removal rate, MRR) were determined for the end process variables of the procedure after determining their optimum cutting velocity, feed rate, and depth of cut. The findings demonstrate a significant departure from TiB₂ nanoparticles strengthened MMCs and give another valuable roadmap for further optimizing the machining of this material.

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