Hot upset forging method
US-9427793-B2 · Aug 30, 2016 · US
US9296036B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9296036-B2 |
| Application number | US-201414327218-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 9, 2014 |
| Priority date | Jul 10, 2013 |
| Publication date | Mar 29, 2016 |
| Grant date | Mar 29, 2016 |
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Methods for producing forged products and other worked products are disclosed. In one embodiment, a method comprises using additive manufacturing to produce a metal shaped-preform and, after the using step, forging the metal shaped-preform into a final forged product. The final forged product may optionally be annealed.
Opening claim text (preview).
What is claimed is: 1. A method compromising: (a) using additive manufacturing to produce a metal shaped-preform, wherein the metal shaped-preform comprises a titanium alloy, wherein the additive manufacturing comprises: depositing layers of a first material on an upper side of a building substrate; and depositing layers of a second material on a opposing lower side of the building substrate; wherein at least one of the first material, the second material, and the building substrate comprises the titanium alloy; (b) after the using step (a), forging the metal shaped-preform, with the building substrate therein, into a final forged product having the building substrate therein. 2. The method of claim 1 , wherein the forging step comprises a single die forging step, wherein the single die forging step is using a single blocker die to die forge the metal-shaped preform into the final forged product. 3. The method of claim 1 , wherein at least one of the first material, the second material, or the building substrate of the metal shaped-preform comprises titanium aluminide. 4. The method of claim 1 , wherein the forging step comprises: heating the metal shaped-preform to a stock temperature; and contacting the metal shaped-preform with a forging die, wherein, when the contacting step is initiated, the forging die is a temperature that is at least 10° F. lower than the stock temperature. 5. The method of claim 1 , wherein the final forged product is a blade for a jet engine. 6. The method of claim 1 , wherein the titanium alloy includes at least 50 wt. % Ti and at least one titanium aluminide phase, wherein the at least one titanium aluminide phase is selected from the group consisting of Ti 3 Al, TiAl and combinations thereof. 7. The method of claim 6 , wherein the titanium alloy includes 5-30 wt. % aluminum, and the titanium alloy comprises at least some Ti 3 Al. 8. The method of claim 1 , wherein the titanium alloy is a Ti-6Al-4V alloy. 9. The method of claim 4 , wherein the contacting step comprises applying sufficient force to the metal shaped-preform via the forging die to realize a true strain of from 0.05 to 1.10 in the metal shaped-preform. 10. The method of claim 1 comprising, after the forging step (b), annealing the final forged product. 11. The method of claim 10 , wherein at least one of the first material, the second material, or the building substrate of the metal shaped-preform comprises a Ti-6Al-4V alloy, and wherein the annealing step comprises heating the final forged product to a temperature of from 640° C. to 816° C. 12. The method of claim 11 , wherein the annealing step comprises heating the final forged product to a temperature of from 670° C. to 750° C. 13. The method of claim 1 , comprising: prior to the using step, designing the shape of the building substrate such that, after the forging step, the building substrate is located in a predetermined area of low strain of the final forged product.
by mechanical means · CPC title
by thermal means (control of energy beam parameters for post heating B22F10/364) · CPC title
Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title
Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations {(B21J5/063 takes precedence)} · CPC title
turbine or like blades from one piece · CPC title
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