This invention discloses a
laser-shock-assisted
creep aging forming method for thin-walled components with complex curvature. The method includes: simulating and obtaining difficult-to-form regions; performing
laser shock on the difficult-to-form regions of a large-size aluminum
alloy thin-walled component sheet; wrapping and fixing a breathable felt around the impacted component; placing the component in a sealed space formed between a vacuum bag and the mold surface; evacuating the sealed space; and then sending the mold into an
autoclave for
creep aging. After completion, the component springs back, yielding the
target surface. This method uses a
laser to
impact localized areas of a large-size aluminum
alloy thin-walled component, introducing dislocations while achieving pre-forming. This provides a good surface foundation for subsequent high-precision
creep aging forming of the component, and is suitable for forming parts with complex curvature.