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contributor authorShingledecker, John
contributor authorBridges, Alex
contributor authorHarless, Nikki
contributor authorGrylls, Richard
contributor authorHussain, Zara
contributor authorPereira, Seba
contributor authorSrinivasan, Shankar
contributor authorMusto, Marco
contributor authorKroenlein, Kenneth
contributor authorSaal, James
date accessioned2026-08-23T07:22:22Z
date available2026-08-23T07:22:22Z
date copyright2026/01/01
date issued2026
identifier issn0742-4795
identifier othergtp-25-1371.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4315010
description abstractAbstract. ABD®-900AM is a highly printable, gamma prime strengthened superalloy purposely designed for powder bed fusion (PBF) additive manufacturing (AM) with broad applicability to high-temperature gas turbine, aerospace, defense, and energy applications. To accelerate the adoption of the alloy, a collaborative team led by EPRI has initiated a first-of-a-kind project to demonstrate qualification of the alloy across multiple AM machines and sites with the goal of developing requisite SAE PBF feedstock and material specifications with supporting statistical material allowables for future inclusions in the metallic materials properties development and standardization (MMPDS) Handbook. In working through the existing SAE qualification framework, a number of challenges were addressed to adapt the specification requirements to the unique attributes of the alloy, future applications, and machine variables. The project started by defining alloy key characteristics (KCs) and key process variables (KPVs) for AM process evaluation. Prequalification work involved a KPV study on a single batch of powder across five machines considering the impact of layer thickness, heat-input, heat-treatment, sample location, and sample orientation. Sensitivity analysis was also performed to assess the impact of minor variations in laser power and solution-heat-treatment temperature. Statistical analysis evaluated these variables against tensile test results and large area microstructural analysis. Initial comparisons to elevated temperature tensile, and creep behavior at 800 °C are also presented and compared to prior work to describe ongoing activities to expand qualification activities to a minimum of 10 heats of powder and 20 manufacturing lots.
publisherThe American Society of Mechanical Engineers (ASME)
titleLearnings in the Qualification of ABD®-900AM for Turbine, Aerospace, and Energy Applications
typeJournal Paper
journal volume148
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4069582
journal fristpage5651
journal lastpage5675
page25
treeJournal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:001
contenttypeFulltext


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