The invention discloses a single-process
machining method of a multilayer
metal composite material. The single-process
machining method is characterized in that two or more
solid metals or alloys are taken as raw materials, and circular arc workpieces of the different metals or the different alloys are placed closely and are spliced into a complete tube-shaped sample; the internal wall and the external wall of the tube-shaped sample are completely restrained by an internal restriction body and an external restriction body, pressure is applied to the annular end faces or the cylindrical surface of the tube-shaped sample, and the internal restriction body and the external restriction body rotate oppositely around a center axis shared by the internal restriction body, the external restriction body and the circular arc workpieces; the circular arc workpieces undergo tangential
shearing deformation under a high
hydrostatic pressure condition, constant growth of the contact surfaces of the different metals is realized, and interface multiplication is formed; and with the continuous increasing of a rotation angle, initial interfaces penetrating through the interior and the exterior of the tube-shaped sample, which are initially formed through
close contact of the circular arc workpieces of the different metals gradually develop into spiral interfaces of which starting points and terminal points are formed at the internal wall and the external wall of the complete tube-shaped sample, and the spiral interfaces are wound by several circles in the tube wall, thereby forming a multilayer
metal composite material structure. With the adoption of the single-process
machining method, the disadvantages that the traditional
metal layer
composite material machining method is complicated, and low in efficiency, interfaces are prone to be polluted by the environment and the
interface bonding quality is poor are overcome, and the multilayer metal composite material having required components, the required number of
layers, the required
layer thickness and the like can be prepared by a
single process.