Titanium alloy parts have the characteristics of low density and good corrosion resistance, so they have become ideal structural materials for aerospace engineering; however, there are many factors that affect its machinability at the same time; this is because of the metallurgical properties of 6al4v titanium plate and material properties, which can have serious effects on the cutting action and the material itself.
The clamping principle of titanium alloy parts is the key technology for Grade 2 Pure Titanium Plate manufacturers to process titanium alloys, as follows:
(1) The clamping force in the roughing stage should be large to prevent the parts from loosening during the machining with large cutting force; the clamping force in the finishing stage should be small to prevent the deformation of the clamping.
(2) The clamping force acts on the rigid place, and the force is applied at as many points as possible.
(3) Appropriate auxiliary devices should be added for thin-walled structural parts with poor rigidity to increase the rigidity of the entire processing system.
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