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Evaluation of Superalloy 718 Additively Manufactured Lattice BlocksLattice block structures made up of high temperature superalloys could offer advantages in density, efficiency, and tailored properties. Three candidate lattice designs were screened through additive manufacturing of superalloy 718. Laser powder bed fusion was applied with 718 powder to produce lattice blocks for three-dimensional octahedral unit cell designs of three heights. As-designed versus additively manufactured 718 lattices were compared, including structural dimensions, densities, defects, grain structures, crystallographic texture, and surface residual stresses. Manufactured lattice I diverged the most from its design, with both corner and center nodes merged into continuous columns. Manufactured lattice III came closest to its design, though the actual nodes and struts were still larger in cross section than in the design. Only modest grain coarsening and negligible chemical segregation were observed for all three designs, suggesting uniform thermo-physical and mechanical properties are possible. Significant tensile residual stresses were present at the surface of the manufactured blocks, with highest stresses in the building direction. Current findings indicate this concept could produce useful superalloy structures for high-temperature-capable static components requiring tailored density, and thermo-physical/mechanical properties.
Document ID
20260001478
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Timothy P Gabb
(Glenn Research Center Cleveland, United States)
Aaron C Thompson
(HX5, LLC)
Christopher A Kantzos
(Glenn Research Center Cleveland, United States)
Timothy M Smith
(Glenn Research Center Cleveland, United States)
Richard B Rogers
(Glenn Research Center Cleveland, United States)
Richard W Rauser
(NovaTek Engineering Toledo, United States)
Richard E Martin
(HX5, LLC)
Date Acquired
February 17, 2026
Publication Date
March 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Metals and Metallic Materials
Report/Patent Number
E20392
NASA/TM-20260001478
Funding Number(s)
WBS: 361807.02.03.02.06
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
super alloys
additive manufacturing
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