The invention belongs to the technical field of precision plastic forming, and particularly relates to a variable-thickness lightweight elastic wing
skin forming method adopting an integral superplastic
diffusion connection method. According to the variable-thickness lightweight elastic wing
skin forming method, outer plates and inner plates of two-layer
skin are subjected to
diffusion connectionand superplastic forming, a
process compensation surface formed in the process of forming reinforcing ribs is subjected to
wire cutting to remove process allowance, then forming and manufacturing withdifferent thicknesses are realized in different regions of the skin, and a bending angle of a windward surface is subjected to cold bending. The variable-thickness lightweight elastic wing skin forming method is realized through a novel and reasonable design of the
variable thickness reinforced structural skin, the combining
diffusion connection, the superplastic forming, the
wire cutting and thecold bending. According to the variable-thickness lightweight elastic wing skin prepared from the forming method, the structural strength of the skin can be effectively improved while weight reduction of traditional thickness skin is realized, the width of a skeleton rib can be greatly reduced, the weight of a traditional skeleton is greatly reduced, the requirements of future
missile models on lightweight bearing structures can be met, the qualification rate and production efficiency of products are improved, and
mass production can be realized.