US2023127804A1PendingUtilityA1

Method for fabricating components using hybrid additive manufacturing and consolidation process

76
Assignee: HAMILTON SUNDSTRAND CORPPriority: Oct 31, 2018Filed: Oct 13, 2022Published: Apr 27, 2023
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
76
PatentIndex Score
0
Cited by
0
References
0
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-modified
1 . 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)

No later patents cite this yet.

References (0)

No backward citations on record.