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The Building Blocks of Directed Energy Deposition Design

INTAMSYS industrial 3d printing

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My kids love creating structures with Legos, Duplos, and boxes. Some days they build big houses with simple walls and others detailed spaceships with intricate features. Their block choice dictates the structure they build, or they pick the blocks based on the resolution they desire. Directed Energy Deposition (DED), a family of Additive Manufacturing (AM) processes, is quite similar in that a designer has a set of geometric “building blocks” she can combine to make a structure. The feature resolution is based on the size of the melt puddle and part volume on the size of the motion platform, but I am getting ahead of myself.

First, let us break down this AM process, as we do in TBGA Training, by asking (3) questions:

How is a Layer formed?

The layer is created with the energy coming together at a focused point to create a melt puddle which is propagated to form a bead.

Common motion platforms include robots and gantries; additional degrees of freedom are often added with turn or flip/tilt motion for the part fixture and substrate.

How is Energy applied?

Thermal or kinetic energy is used to convert particles or filament (wire) into a solid layer.

Today we are contemplating Fusion (thermal) DED, where the material is melted. Any compatible heat source and material combination can be used including laser, electron beam, plasma, and arc. Other processes use friction, ultrasonic, or kinetic energy.

How is the Material applied?

Wire via a feeder or powder particles fed with a carrier gas.

Some process and material combinations require specialty incoming material chemistries, but many can use standard “off the shelf” weld wire and coarser cuts of powder, which can be less expensive.

In a nutshell, DED is all about propagating a molten pool of metal to form a series of beads that solidify to form geometries. The bead needs a surface to attach to, so the process begins with a substrate, or base, to start deposition. Deposition is often followed by a heat treatment, partial or full machining (or other surface smoothing step), and non-destructive evaluation. DED is also often combined with other welding or cladding processes to create a final part. Two common process set ups are shown in Figure 1. The part shown in the figure is a partially machined titanium demonstrator manufactured by GKN Aerospace using Laser Wire DED showing geometry “building blocks” of straight walls, curved walls, and multiple intersections. Another characteristic of DED processes is a wide range of possible part sizes ranging from a few cubic centimeters to many cubic meters.

Figure 1: Two deposition setups showing (top) cylindrical substrate with a secondary turning axis and (bottom) flat plate substrate. Gray denotes substrate, green deposition head, and blue deposited material. Part image source: GKN Aerospace.

Designing for DED

Designing for DED can be broken down into the opportunistic aspects, called Design for AM (DfAM), and the restrictive aspects, called Modify for AM (MfAM), as described in a previous TBGA article. Tables 1-3 illustrate key design considerations before, during and after deposition and note whether they are DfAM or MfAM considerations. The supporting software is just as important as calibrated hardware in a successful DED build. Part slicing, deposition path planning, which is the sequence of deposited beads, and control of layer (bead) height are critical, and all have cross-cutting and inter-related impacts on design.

Table 1: Key DED Design Considerations for Substrate and Feedstock

  Substrate Feedstock
Consideration Size, material, and temper

 

Use of substrate as sacrificial or integral to part Deposition of different materials and functionally graded materials Material form effect on surface finish
Impact Insufficient heat dissipation, inability to fit final part in DED preform Design flexibility, part performance, and cost Ability to design with location specific material performance Some processes may require finish machining or other surface smoothing
DfAM or MfAM MfAM DfAM DfAM MfAM

 

Table 2: Key DED Design Considerations for Deposition

  Deposition
Consideration Melt pool size and bead width/height Motion platform degrees of freedom Start / Stop / Transition locations with different material properties Thermal cycling and stress build up create part warpage
Impact Dictates deposition geometries, feature resolution, and number of beads required Features may be limited by self-supporting angle Add sacrificial deposition for Start/Stop outside of final part or locate in less critical area Part may require intermediate stress relief during deposition or other design compensation
DfAM or MfAM DfAM and MfAM DfAM and MfAM MfAM MfAM

 

Table 3: Key DED Design Considerations Post-Deposition

Machining Non-Destructive Evaluation
Consideration Fixturing and datum locations Ability to alternate deposition and machining Surface interface with NDE and/or geometry compatibility Thinner sections in very large parts
Impact Inability to machine final part from preform Unitization, design flexibility, and cost Requires more expensive NDE, intermediate machining prior to NDE or inability to use that feature Ability to perform NDE to a greater level of sensitivity
DfAM or MfAM MfAM DfAM MfAM DfAM

 

DED Applied

I recently checked in with several leading developers of DED processes to showcase the variety of designs being built. The first is my former GKN Aerospace team, who are developing titanium Laser Wire DED with Oak Ridge National Laboratory in Tennessee. They have explored process parameters to create different bead widths to build walls ranging from 3mm up to 20mm, as shown in Figure 2. Their system has a flip/tilt fixture for the substrate which adds 2 additional degrees of freedom to the robot mounted deposition head enabling the exploration of more complex overhangs and double-sided deposition, which is great for managing distortion; Figure 3 shows a part built with double sided deposition that will be subsequently machined 100%. The Oak Ridge National Laboratory team used the same process to produce the fin shaped part shown in Figure 4; the diamond shaped holes showcase a design feature tailored to process capability.

Figure 2: Two 3 bead wide walls built on the same Laser Wire DED system using different key process variables. Source: GKN Aerospace.

 

Figure 3: Titanium Laser Wire DED deposited part. Source: GKN Aerospace.

 

Figure 4: Partially machined fin shaped titanium Laser Wire DED deposited part showing design examples of process compatible holes. Source: Oak Ridge National Laboratory Manufacturing Demonstration Facility.

Moving out to Colorado, the aluminum article shown in Figure 5, was produced as a single component without parasitic support material using Big Metal Additive’s multi-axis hybrid DED and machining process. This seating module for a marine transport vehicle is 6 feet wide, 2 feet deep and almost 3 feet tall. The design originates from an inspiration of generative design, and the CAD model was created from convergent modeling methods. There are overhang angles greater than 45 degrees and several converging and diverging connecting geometries with this challenging structure.

Figure 5: Aluminum DED structure built by Big Metal Additive.

DED enables the use of multiple materials for tailored performance. For components, like the rocket nozzle shown in Figure 6, regions with concentrated heat loads can be fabricated out of higher temperature materials while other areas can be fabricated out of higher strength materials. Built by FormAlloy in California with a small melt puddle powder-fed DED process, the rocket nozzle with internal cooling channels was built first, followed by the addition of the flange and the clad on the outer diameter. This component demonstrates the ability to build, add features and/or repair, and clad with a single DED process.

Figure 6: Rocket nozzle built with powder-fed DED by FormAlloy.

These examples show just a few of the design possibilities enabled by DED but many more geometries are being created including:

  • 1+ meter satellite fuel tank domes built with Electron Beam / Wire DED by Lockheed Martin
  • Tooling repair / re-manufacture for automotive dies using hybrid powder-fed Laser DED and machining
  • Like for like replacement flying 787 floor grid brackets built by Norsk Titanium
  • Large steel bridge built by MX3D in Amsterdam (I stood on an early prototype!)

DED as a Tool

DED is a tool that is finding its way into quite a few manufacturing toolboxes, though I doubt Wallace D. Wattles was considering DED when he said, “It is essential to have good tools, but it is also essential that the tools should be used in the right way.” Whether contemplating our next family build activity or the build plan for a large metal component, it is critical to select the right process for the job. Understanding the DfAM and MfAM characteristics of specific processes is a fantastic starting point for a DED design journey.

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