The invention relates to surface differential
lubrication, in particular to a surface differential
lubrication method for an
aviation internal high-pressure forming three-way
pipe. The top of the three-way
branch pipe can be effectively prevented from being broken, and meanwhile wrinkles in a non-deformation area are effectively prevented. Comprising the following steps: S1, selecting a
metal tube blank with certain outer
diameter and wall thickness according to the specification of a finished product; s2, the surface quality and the
internal quality of the
pipe blank are checked; s3, the pipe blank is
cut to the length of 250 mm; s4, a material supplementing area, a deformation area and a non-deformation area are marked on the pipe blank through a marking pen; s5, the non-deformation area is subjected to
polishing treatment through raw
abrasive paper; s6, a
molybdenum disulfide
lubricant is sprayed to the deformation area to reduce
friction force; s7, the material supplementing area is not treated; s8, the pipe blank is placed in the dies, and the upper die and the lower die are closed to start the forming process; s9, advancing to a water injection position through a left pushing head and a right pushing head; s10, continuously advancing to a sealing position; s11, liquid is injected into the pipe through the push head; s12, applying counter-acting force to the formed three-way
branch pipe by using a reverse thrust head; and S13, forming is completed.