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Influences of Introduced Yttrium Oxide Particles on Superalloy 718Additive manufacturing has proven useful for introducing oxide particles into superalloys, to provide oxide dispersion strengthening (ODS) at high temperatures. This study screened how such an approach can influence microstructure and failure modes for superalloy 718. The objective of this study was to compare tensile and creep failure modes for additively manufactured superalloy 718 having introduced oxide particles. Fine yttrium-oxide (yttria) particles were introduced into 718 powder using two different powder mixing methods. Additive manufacturing by laser powder bed fusion was then used to prepare specimen blanks for each case, oriented parallel and transverse to the building direction. These were subsequently given consistent stress relief, hot isostatic pressurization, and final heat treatments, then subjected to tensile and creep tests at varied temperatures. Additively manufactured 718 without ODS (“no-ODS”) had nearly equiaxed grains at 50 μm in width. Roll-mixed ODS material had a bimodal grain size distribution, with fine grains at 9 μm and coarse grains at 66 μm in average width. The fine grains were elongated about 5x in the building direction. Acoustic-mixed ODS materials had grains at 10 μm in width that were elongated about 10x in the build direction. Compared to no-ODS, roll-mixed and acoustic mixed ODS materials did not show improved tensile strengths at room temperature, 760 °C, and 1093 °C. The tensile failure strains parallel to the building direction of roll-mixed ODS material were lowest in these tests. Flattened clumps of yttria had formed transverse to the building direction in roll-mixed material, which were easily cracked. Creep rupture response at 760 °C in the building direction was highest for acoustic-mixed material test. Creep tests at 1093 °C showed varied results, with low rupture lives associated with enhanced cavitation at grain boundaries and surface oxidation. Transverse to the building direction, all three materials had low failure strains in tests at 760 °C. The elongated grain boundaries failed readily in all transverse specimens tested at 760 °C and 1093 °C.
Document ID
20260001480
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Timothy P Gabb
(Glenn Research Center Cleveland, United States)
Christopher A Kantzos
(Glenn Research Center Cleveland, United States)
Timothy M Smith
(Glenn Research Center Cleveland, United States)
Henry C Degroh III
(Glenn Research Center Cleveland, United States)
Aaron C Thompson
(HX5, LLC)
Date Acquired
February 17, 2026
Publication Date
July 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Metals and Metallic Materials
Report/Patent Number
E-20405
NASA/TM-20260001480
Funding Number(s)
WBS: 361807.02.03.02.06
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
oxide dispersion strengthening
additive manufacturing
supper alloys
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