The invention relates to a space envelope forming manufacturing method of a thin-wall high-rib heat dissipation component. The method comprises the following steps that S1, a
forging is designed, specifically, a
forging parting surface of the thin-wall high-rib heat dissipation component is a plane where a bottom plate is located, and an oblique flash edge is arranged at the top of the side face of a bottom plate of the
forging; S2, a blank is designed, specifically, the blank is a slab, and the shape of the cross section
contour line of the slab is the same as the shape of the cross section
contour line of the bottom plate; S3, space envelope forming is carried out; S4, envelope finishing is carried out; S5, the forging is ejected; and S6, trimming is carried out, specifically, high ribsof the forging obtained in the S5 are inserted into hole type cavities of a lower die of a trimming die, an upper die of the trimming die makes contact with the bottom plate of the forging, the forging and the lower die of the trimming die are pushed to move downwards at the same time, and the flash edge of the forging is
cut off under the shearing action of the upper die and a fixing die of the trimming die; and S7, the end surfaces of the high ribs are orderly
cut. According to the space envelope forming manufacturing method of the thin-wall high-rib heat dissipation component, not only canthe integral forming of the thin-wall high-rib heat dissipation component be realized, but also the material
utilization rate can be improved, the forming limit of the
thin wall and the high ribs canbe improved, and the loaded state of a die can be improved.