NASA SBIR 2018-I Solicitation

Proposal Summary

 18-1- Z3.01-5453
 Advanced Metallic Materials and Processes Innovation
 Internal/External Surface Finishing of Additively Manufactured IN-625 Components
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
REM Chemicals Inc. dba REM Surface Engineering
325 West Queen Street
Southington , CT 06489-1177
(860) 621-6755

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Agustin Diaz
2107 Longwood Dr. Brenham, TX 77833 - 5231
(979) 277-9703

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Nathan Michaud
325 W. Queen St Southington, CT 06489 - 1177
(860) 621-6755
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 6
Technical Abstract

The objective of this proposal is to develop a surface finishing technology for Inconel 625 Additive Manufactured (AM) workpieces.   The following methodologies will be evaluated and optimized: vibratory finishing, chemical milling and electropolishing.  Once optimized, the project will explore combinations of these aforementioned methodologies in order to identify a surface finishing process that can remove 0.02 inches (0.51 mm) of stock in the shortest practical time.  The deliverable will be a practical surface finishing procedure that is amenable to commercial industrial scale-up.

Inconel 625 is a nickel-based superalloy that is used in critical aerospace parts that require mechanical strength, resistance to thermal creep deformation, surface stability and resistance to corrosion or oxidation.  AM Inconel 625 parts are lighter, can be more complex and consist of fewer components than those made by conventional machining.  AM parts, however, suffer from very rough surfaces having initiation sites that lessen their mechanical strength and fatigue properties.  A process is urgently needed to reduce the surface roughness so as to eliminate stress raisers in order for the aerospace industries to take full advantage of AM Inconel 625.  Currently, there are no known processes to accomplish this proposal’s objectives.

Potential NASA Applications

This technology is applicable to all NASA additively manufactured IN-625 projects requiring improvement to surface finish or mechanical performance including fuel nozzles, missile bodies, rocket skin, nuclear reactor components, turbomachine components, stud supporters, thrust chambers, engine manifolds, and rocket engines.  IN-625 components produced by other methods will also benefit from the technology due to surface finish and mechanical performance improvements.

Potential Non-NASA Applications

The technology applies to other agencies (including the DoD) and the entire metal-based AM field; industries including aerospace industry, medical devices, automotive/ground vehicle transportation/heavy equipment, energy (nuclear/oil and gas), and industrial machinery are pursuing metal-based AM using alloys such as IN-625. Applications include fuel nozzles, nuclear reactor components, turbomachine components, stud supporters, thrust chambers, engine manifolds, and exhaust components.


Form Generated on 05/25/2018 11:57:02