• Login
    View Item 
    •   DSpace Home
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   DSpace Home
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Learnings in the Qualification of ABD®-900AM for Turbine, Aerospace, and Energy Applications

    Thumbnail
    View/Open
    gtp-25-1371.pdf (2.390Mb)
    Date
    2026
    Author
    Shingledecker, John
    Bridges, Alex
    Harless, Nikki
    Grylls, Richard
    Hussain, Zara
    Pereira, Seba
    Srinivasan, Shankar
    Musto, Marco
    Kroenlein, Kenneth
    Saal, James
    Metadata
    Show full item record
    Abstract
    Abstract. 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.
    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4315010
    Collections
    • Journal of Engineering for Gas Turbines and Power

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV
     

     

    Browse

    All of DSpaceCommunities & CollectionsBy Issue DateAuthorsTitlesSubjectsThis CollectionBy Issue DateAuthorsTitlesSubjects

    My Account

    LoginRegister

    Statistics

    View Usage Statistics

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV