The invention discloses a surface strengthening treatment method for an inner hole of a main connecting rod of a
piston type aero-engine. The surface strengthening treatment method comprises the following steps that S100, the main connecting rod is subjected to oil removal treatment; s200, performing
waxing treatment on the non-plated surface on the main connecting rod to form an insulating
protection layer; s300, weak
corrosion activation treatment is conducted on an inner hole of the main connecting rod; s400, a tool clamp is used for installing and hanging the main connecting rod, then a lead and
tin plating solution is poured into an inner hole of the main connecting rod for out-groove
electroplating treatment, and the lead and
tin plating solution comprises 110 g / L to 275 g / L of lead fluoroborate, 30 g / L to 65 g / L of stannous fluoroborate, 1 g / L to 2 g / L of
hydroquinone and 1.5 g / L to 2.0 g / L of oxhide
gelatin; and S500, the main connecting rod is detached from the tool clamp and then subjected to
wax removal and cleaning treatment, and then whether the lead-
tin layer is qualified or not is checked. According to the surface strengthening treatment method for the inner hole of the main connecting rod of the
piston type aero-engine, the uniformity of a plating layer can be improved, the tin content in a lead-tin layer is increased, and the wear-resisting and lubricating capacity is enhanced.