Abstract

Additive manufacturing (AM) has been leveraged across various industries to potentially open design spaces allowing the design of parts to reduce the weight, cost, and integrated design. Over the past decade, AM has sped up fast enough to penetrate various industry offering potential solutions for multiple materials, such as metals, alloys, plastics, polymers, etc. However, challenges lie to best utilize the opened design spaces as current generation engineers are trained to design parts for the conventional manufacturing process. With this lack of design guidelines for the AM process, users are limiting themselves to best utilize the offering made by advanced manufacturing. For aerospace parts, the design freedom of additive manufacturing is attractive mainly for two purposes: for weight reduction through lighter, integrated design concepts as well as for functional optimization of parts aiming at an increase of performance, e.g., by optimizing flow paths. For both purposes, it is vital to understand the material-specific and manufacturing process design limits. In AM, combination of each material and manufacturing process defines the design space by influencing minimum thickness, angle, roughness, etc. This paper outlines a design guideline for the laser powder bed fusion (also DMLM, direct metal laser melting) AM process with Inconel 718 material. Inconel 718 is a superalloy with superior mechanical properties and corrosion resistance at elevated temperatures up to 700 °C and is, therefore, used in several applications including aerospace engine parts. Due to its weldability, the alloy has also been extensively investigated in laser powder bed fusion and other additive manufacturing processes. A comprehensive study is provided both analytically and experimentally suggesting how parts can be designed having critical design features, manufacturing direction/orientation to meet design requirements, design accuracy, and quality. Design features presented include walls, overhangs, bore holes, and teardrop shapes, with their minimal feature sizes and effects on accuracy and roughness of the build parts. For the light-weight design of parts, different concepts such as lattices and stiffener structures are discussed. For gas or liquid carrying flow channels, the geometrical form and size are highlighted. Based on an approach by Kranz et al., design guidelines for Inconel 718 are derived from the experiments and provided in the form of a catalog for easy application.

Highlights

  • Nickel-based superalloys are used today in a broad range of industrial and, especially, aerospace applications due to their high strength and corrosion resistance at higher temperatures.A variety of alloys exists, some of which are designed for use in cast, wrought, and powder metallurgical production routes.1One of these alloys is Inconel 718 (IN718), which is typically wrought or processed in powder bed fusion due to its weldability, Unsupported small wallsHorizontal overhangsWidth Height ThicknessUnsupported large walls10 15 0.1, 0.2, ... , 0.7/1.0/1.5Width Height Total length Overhang length aHorizontal bridges5 14 5+a 0.5, 1.0, ... , 3.0 Supported walls

  • Selected design features have been built by laser powder bed fusion (L-PBF) in IN718

  • General recommendations for the design of IN718 L-PBF parts can be derived that are mainly in line with similar investigations performed with different materials, such as Ti-6Al-4V

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Summary

INTRODUCTION

Nickel-based superalloys are used today in a broad range of industrial and, especially, aerospace applications due to their high strength and corrosion resistance at higher temperatures. Additive manufacturing is used in the aerospace industry typically to optimize parts regarding weight and functionality, using its high degree of design freedom.. To exploit the full potential and avoid production waste and costs, the designer needs to know the exact design limits of the technology for a given material as part of a holistic design for additive manufacturing (DfAM) approach. The work presented by Kranz et al. provides specific design limits for typical part features, such as walls, bar structures, bore holes, and the like, for laser powder bed fusion (L-PBF). This article builds on the mentioned design guidelines and identifies the corresponding design limits for design features build-out of IN718 and discusses its application to the DfAM of an aerospace engine frame

Design features and reference geometries
Materials
L-PBF process
Roughness measurement
RESULTS AND DISCUSSION
Overhang and bridge features
Horizontal bore holes
Unsupported bars
Application to light-weight design
SUMMARY AND OUTLOOK
Full Text
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