The paper examines the results of machining tests carried out on two alloys commonly used in the aircraft industry, specifically, alphabeta type titanium alloy Ti6A14V and nickel-based superalloy of type 718. In view of their excellent mechanical properties and their resistance to a wide range of temperatures, these alloys are widely used in the manufacture of turbo-engine parts. They are extremely difficult to machine, however, for various reasons. The present aim is to consider how their drilling, turning, and milling could be made more productive.
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López de Lacalle, L., Pérez-Bilbatua, J., Sánchez, J. et al. Using High Pressure Coolant in the Drilling and Turning of Low Machinability Alloys. Int J Adv Manuf Technol 16, 85–91 (2000). https://doi.org/10.1007/s001700050012
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DOI: https://doi.org/10.1007/s001700050012