Metal powder, method of producing additively-manufactured article, and additively-manufactured article
US-2016332227-A1 · Nov 17, 2016 · US
US11292057B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11292057-B2 |
| Application number | US-202016863199-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 30, 2020 |
| Priority date | Dec 26, 2019 |
| Publication date | Apr 5, 2022 |
| Grant date | Apr 5, 2022 |
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The present invention discloses a method for manufacturing a thin-walled metal component by three-dimensional (3D) printing and hot gas bulging. The present invention uses 3D printing to obtain a complex thin-walled preform, which reduces a deformation during subsequent hot gas bulging. The present invention avoids local bulging thinning and cracking, undercuts at the parting during die closing, and wrinkles due to the uneven distribution of cross-sectional materials, etc. The present invention obtains a high accuracy in the form and dimension through hot gas bulging. After a desired shape is obtained by hot gas bulging, a die is closed to keep the component under high temperature and high pressure for a period of time, so that a grain and a phase of the material are transformed to form a desired microstructure.
Opening claim text (preview).
What is claimed is: 1. A method for manufacturing a thin-walled metal component by three-dimensional (3D) printing and hot gas bulging, comprising the following steps: step 1, determining a shape of a large-sized thin-walled preform: determining a shape of the preform according to a characteristic of the thin-walled component with a large size; step 2, printing the preform: preparing the thin-walled preform by 3D printing; step 3, heating a die: heating the die for the hot gas bulging, to a first set temperature; the die is heated by a high-frequency induction heating device; when the preform is an aluminum alloy, the die is heated to 350-450° C.; when the preform is a high-temperature alloy, the die is heated to 850-950° C.; when the preform is a titanium alloy, the die is heated to 650-850° C.; when the metal plate is prepared, a titanium alloy sheet is heated to about 600° C.; step 4, placing the preform and closing the die: placing the pretreated preform into the die, and closing the die; step 5, filling a gas for bulging: filling a high-pressure gas into the preform or onto a surface of the preform to bulge the preform into a desired component; step 6, holding the temperature and pressure: keeping the die closed, and allowing the desired component to stand under high temperature and high pressure for a period of time; step 7, exhausting and cooling down: exhausting the gas inside or on the surface of the desired component after holding, to a set pressure, and cooling the die to a second set temperature; and step 8, opening the die and taking the thin-walled component out: opening the die, and taking the thin-walled component out. 2. The method for manufacturing a thin-walled metal component by 3D printing and hot gas bulging according to claim 1 , wherein after step 2 is completed, an end or surface of the obtained thin-walled preform is pretreated by cutting or grinding. 3. The method for manufacturing a thin-walled metal component by 3D printing and hot gas bulging according to claim 2 , wherein after step 8 is completed, an end or surface of the thin-walled component is treated. 4. The method for manufacturing a thin-walled metal component by 3D printing and hot gas bulging according to claim 1 , wherein in step 2, the thin-walled preform is prepared from a titanium alloy, a high-temperature alloy, an aluminum alloy or a titanium alloy powder by 3D printing. 5. The method for manufacturing a thin-walled metal component by 3D printing and hot gas bulging according to claim 4 , wherein in step 2, the 3D printing is selective laser melting (SLM); a laser, an ion beam or an electric arc is used as a heat source, and a powder or wire of a high-temperature alloy, an aluminum alloy or a titanium alloy is used as a raw material. 6. The method for manufacturing a thin-walled metal component by 3D printing and hot gas bulging according to claim 1 , wherein in step 5, a 3-6.5 MPa nitrogen gas is introduced into the preform or onto a surface of the preform for hot gas bulging, and the preform is bulged against a die cavity in 10-50 s to obtain a desired contour. 7. The method for manufacturing a thin-walled metal component by 3D printing and hot gas bulging according to claim 1 , wherein in step 6, the desired component is left in the die and the die is kept closed; the die is heated to 520-770° C., and the gas pressure rises to 10-20 MPa; the temperature and the pressure are held for 1 h.
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