The invention discloses a
metal part production and forming process for the
aviation field, relates to the technical field of
metal part production and manufacturing, and aims to solve the problems that in the heating stage of a
casting, if equipment breaks down, no
emergency treatment measures exist, and the
alloy plasticity of the
casting is easily affected in the existing
metal part production and forming process for the
aviation field. The process comprises the following steps of, 1, preparing a
titanium ingot, reducing
titanium ore into pure
titanium tetroxide through chlorination and
distillation, refining the pure titanium tetroxide into a
sponge titanium
raw material by virtue of vacuum separation, removing impurities, and obtaining the titanium
ingot through
electrode welding; 2, carrying out end face pretreatment, specifically, cleaning one end face of the titanium
ingot, spraying an anti-oxidation
coating after cleaning is completed, and marking an ingot number; and 3, carrying out pretreatment on the titanium ingot, placing the face, with the ingot number, of the titanium ingot on an adsorption base of a cleaning and spraying all-in-one
machine, and fixing the titanium ingot to the adsorption base through
suction force generated by a vacuum generator.