Learnings in the Qualification of ABD®-900AM for Turbine, Aerospace, and Energy ApplicationsSource: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:001::page 5651Author:Shingledecker, John
,
Bridges, Alex
,
Harless, Nikki
,
Grylls, Richard
,
Hussain, Zara
,
Pereira, Seba
,
Srinivasan, Shankar
,
Musto, Marco
,
Kroenlein, Kenneth
,
Saal, James
DOI: 10.1115/1.4069582Publisher: The American Society of Mechanical Engineers (ASME)
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.
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| contributor author | Shingledecker, John | |
| contributor author | Bridges, Alex | |
| contributor author | Harless, Nikki | |
| contributor author | Grylls, Richard | |
| contributor author | Hussain, Zara | |
| contributor author | Pereira, Seba | |
| contributor author | Srinivasan, Shankar | |
| contributor author | Musto, Marco | |
| contributor author | Kroenlein, Kenneth | |
| contributor author | Saal, James | |
| date accessioned | 2026-08-23T07:22:22Z | |
| date available | 2026-08-23T07:22:22Z | |
| date copyright | 2026/01/01 | |
| date issued | 2026 | |
| identifier issn | 0742-4795 | |
| identifier other | gtp-25-1371.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4315010 | |
| description 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. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Learnings in the Qualification of ABD®-900AM for Turbine, Aerospace, and Energy Applications | |
| type | Journal Paper | |
| journal volume | 148 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4069582 | |
| journal fristpage | 5651 | |
| journal lastpage | 5675 | |
| page | 25 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:001 | |
| contenttype | Fulltext |