US2023127804A1PendingUtilityA1
Method for fabricating components using hybrid additive manufacturing and consolidation process
Est. expiryOct 31, 2038(~12.3 yrs left)· nominal 20-yr term from priority
B22F 10/66B22F 10/68B22F 10/28B22F 3/15B33Y 10/00B22F 10/62B22F 2003/247B33Y 30/00B22F 3/24B30B 11/002B22F 2201/10B33Y 70/00Y02P10/25B22F 2003/153
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Claims
Abstract
A method of fabricating a near net shape component includes forming a sacrificial shell from a pulverant material using an additive manufacturing process, the shell having an aperture. The method further includes filling the shell with a second pulverant material, subjecting the filled shell to a consolidation process, and removing the shell from the consolidated second pulverant material.
Claims
exact text as granted — not AI-modified1 . A system for fabricating a component, the system comprising:
a sacrificial shell formed from a first material and comprising an aperture; a second material contained within the hollow shell, the second material being a pulverant material; and means for consolidating the second material within the hollow shell.
2 . The system of claim 1 and further comprising: chemical or mechanical means for removing the hollow shell from the consolidated second material.
3 . The system of claim 2 , wherein chemical means for removing the hollow shell comprises a chemical etchant.
4 . The system of claim 2 , wherein mechanical means for removing the hollow shell comprises at least one of a cutting, milling, and grinding process.
5 . The system of claim 1 , wherein the means for consolidating the second material comprises an isostatic pressing process.
6 . The system of claim 1 , wherein the first material is different from the second material.
7 . The system of claim 1 , wherein the shell comprises a first region with a first shell thickness, and a second region with a second shell thickness different from the first shell thickness.
8 . The system of claim 1 , wherein the shell has an inner surface geometry complementary to a component geometry.
9 . The system of claim 1 and further comprising: a solid base portion attached to the sacrificial shell and formed from the first material.
10 . The system of claim 1 and further comprising: a solid component portion formed from the first material and integral to the sacrificial shell.Cited by (0)
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