Comparison of Electron Beam and Laser Beam Powder Bed Fusion Additive Manufacturing Process for High Temperature Turbine Component Materials, Phase II. CRADA Final Report
The evolving additive manufacturing (AM) technology is now at the point where some metallic turbine components are being fabricated for both development and production purposes. The goal of this phase II project is to continue the evaluation of AM Nickel Alloy X fabricated by electron beam (EB) or laser beam (LB) powder bed fusion (PBF) process for gas turbine applications. Microstructure, mechanical and oxidation properties characterization was conducted on test specimens produced with powders of different chemistries within the typical material specification range. Powders with high Silicon (Si) content for the LB-PBF and low Si content for the EB-PBF displayed significant cracking levels in the AM Nickel Alloy X material. Accordingly, optimum fatigue performance would require careful control of powder chemistry, optimization of the fabrication parameters for a given powder and use of hot isostatic pressing (HIP) post treatment. Oxidation testing conducted at 1472°F (800ºC) in air showed that the roughness of the EB-PBF specimens led to an increase in specimen mass change, but overall the AM specimens exhibited oxidation behavior at 1472°F (800ºC) that is appropriate for applications in gas turbine engines. Assessment of the geometric capability of the LB-PBF and EBPBF systems using artifacts representative of turbine component geometries revealed that the LB-PBF process is well-suited for the fabrication of intricate geometries needed for turbine engine fuel injector components, but further process development is required to improve the EB-PBF system feature resolution.