Abstract

This paper reviews state of the art laser powder bed fusion (L-PBF) manufacturing of γ′ nickel-based superalloys. L-PBF resembles welding; therefore, weld-cracking mechanisms, such as solidification, liquation, strain age, and ductility-dip cracking, may occur during L-PBF manufacturing. Spherical pores and lack-of-fusion voids are other defects that may occur in γ′-strengthened nickel-based superalloys manufactured with L-PBF. There is a correlation between defect formation and the process parameters used in the L-PBF process. Prerequisites for solidification cracking include nonequilibrium solidification due to segregating elements, the presence of liquid film between cells, a wide critical temperature range, and the presence of thermal or residual stress. These prerequisites are present in L-PBF processes. The phases found in L-PBF-manufactured γ′-strengthened superalloys closely resemble those of the equivalent cast materials, where γ, γ′, and γ/γ′ eutectic and carbides are typically present in the microstructure. Additionally, the sizes of the γ′ particles are small in as-built L-PBF materials because of the high cooling rate. Furthermore, the creep performance of L-PBF-manufactured materials is inferior to that of cast material because of the presence of defects and the small grain size in the L-PBF materials; however, some vertically built L-PBF materials have demonstrated creep properties that are close to those of cast materials.

Highlights

  • The quest for higher efficiency jet engines and land-based gas turbines has necessitated the use of materials that can withstand the mechanical stress of operating at extremely high temperatures [1].Nickel-based superalloys are suitable for turbine blade applications where they confer resistance to creep, fatigue, and oxidation and protect against corrosion [1]

  • This is illustrated by the temperature profiles of single tracks that are melted on a substrate and a powder bed displayed in Figure 2 [17]

  • Demonstrated that the critical temperature range (CTR) from a Scheil-Guliver calculation spanned 350 ◦ C, whereas the CTR from an equilibrium calculation spanned 100 ◦ C. These results demonstrate that the factors necessary for solidification cracks are not limited to the presence of liquid films or a large solidification temperature range, but thermal or residual stress must pull apart the liquid film

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Summary

Introduction

The quest for higher efficiency jet engines and land-based gas turbines has necessitated the use of materials that can withstand the mechanical stress of operating at extremely high temperatures [1]. Laser powder bed fusion (L-PBF) is of interest for the manufacture of turbine blades using γ0 -strengthened nickel-based superalloys. 1, yielded few publications on powder bed fusion (PBF; using laser and electron beam energy sources) of superalloys. 36 publications where L-PBF was used to manufacture γ’ nickel-based superalloys were found. These superalloys were reviewed in the present manufacture γ0 nickel-based superalloys were found. Most publications on PBFbyof superalloys involve Alloy 718, as seen in the bottom of Figure 1. Strengthened by γ” (Alloy 718 is not reviewed in this paper) and is relatively easy to process [6].

Overview
Heat Source and Material Interaction in the L-PBF Process
Overview of Cracking and Porosity
Influence of Laser Scanning Strategy on Cracking
Influence of Stress on Cracking
Influence of Solidification on Cracking
Solutions to Cracking
Grain Structure
Phases in L-PBF Microstructure
11. As-built
Role of Other Microconstituents x FOR
Mechanical Properties and Performance
Findings
Summary
Full Text
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