The invention relates to the technical field of improvement of the strength of aircraft or high-speed locomotive structural
fastener connecting holes and specifically relates to a method for intensifying the strength of an aircraft or high-speed locomotive structural
fastener connecting hole in an extruding mode, in particular to a
machining method of a split sleeve. The method comprises the following steps that raw materials are selected according to specification requirements of the required stainless steel split sleeve, wherein the raw materials are hard stainless
steel plates which are subjected to no heat treatment when leave a factory; and the raw materials are subjected to annealing heat treatment and then subjected to rolling depression and leveled on a roller press according to needs, the thickness is adjusted, and after calculation and blank
layout are completed, the raw materials are
cut into bar-shaped to-be-machined raw materials. According to the
machining method of the split sleeve, heat treatment is adopted for the excessively thicker stainless
steel plates subjected to no heat treatment, firstly the thickness is adjusted, then
punching blanking and bending and
rounding linkage forming reinforcing are performed, and the problem that high-strength stainless steel sheets are difficult to form is solved in the mode that the thickness of the stainless
steel plates subjected to heat treatment is adjusted firstly, and then
punching blanking and bending and
rounding linkage forming reinforcing are performed.