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Feasibility Study to Dissolve Additively Manufactured Inconel 718 Support StructuresAdditive manufacture (AM) component design face constrains due to support structure removal. Interior passages or delicate geometries require supports yet cannot be removed without compromising the design or complicating post-processing. A process was developed to dissolve metal AM supports where a sensitizing agent is applied post-build. During stress relief the sensitizing agent diffuses into the surface and alters the chemical composition of the top 100 to 200 μm. During an electrochemical dissolution process the sensitized region is susceptible to corrosion/dissolution and the etching reaction self-terminates once the sensitized region is dissolved. Support thickness varies from 80 to 200 μm, resulting in total dissolution or sufficiently weakened to facilitate removal. The objective of this project was to demonstrate a support structure dissolution process for IN718 components built using AM and to characterize the impact on mechanical properties, microstructure, and surface finish.
Document ID
20205003682
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Omar R Mireles
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
William Tilson
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Sara Rengifo
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Christopher Lefky
(Colorado School of Mines Golden, Colorado, United States)
Owen Hildreth
(Colorado School of Mines Golden, Colorado, United States)
Date Acquired
June 18, 2020
Subject Category
Composite Materials
Meeting Information
Meeting: 2020 AIAA Propulsion and Energy Forum
Location: Virtual
Country: US
Start Date: August 24, 2020
End Date: August 26, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80MSFC18N0001
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
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