Elementum 3D to lead project focused on modeling additive geometries with novel materials for aerospace applications

Elementum 3D (E3D) was recently awarded $500,000 in funding through the America Makes Cooperative Agreement to lead a project focused on modeling additive geometries with novel materials for aerospace applications under Phase 2 of the High Temperature Applications Using Additive Manufacturing Program. The United States Department of Defense (DoD) recognizes the critical importance of high-velocity missile system capability to support the U.S. warfighter. These systems offer rapid response and accurate delivery of weapons effects through highly contested environments. E3D, specializing in the creation of advanced metals, composites, and ceramics to support additive manufacturing (AM) processes, will partner with Rolls-Royce, Applied Optimization, and the Applied Research Lab at Penn State University to advance high-temperature airframe materials and manufacturing technology to ensure that the U.S. military has a superior advantage over its adversaries.


Funded by the Office of the Secretary of Defense Manufacturing Technology (OSD ManTech) Program and Air Force Research Laboratory, E3D will work to leverage its proprietary Ni230-RAM1 material for additively manufactured heat shield tiles for turbine engines. Ni230-RAM1 is a highly crack-resistant modification of Haynes 230 nickel superalloy, which, though generally considered weldable, experiences extensive microcracking in laser powder bed fusion (LPBF) printing.


The project objective is to combine advanced material technologies with computational models to solve cracking and warping issues in LPBF printing of nickel superalloys. E3D’s reactive additive manufacturing (RAM) material technology will largely address cracking issues; and computational modeling using measured material property and in-situ process monitoring data as inputs, will predict geometry-dependent warping behavior. The model will also generate geometry-specific process parameters to prevent distortion.


The results of the 18-month project should enable more predictable and reliable LPBF printing of distortion-prone nickel superalloys and form a basis for predictive tools that can be applied to other material systems. Greater reliability will ultimately result in fewer scrap builds and reprints, increased efficiency, lower costs, and overall improved operating performance to meet the demanding requirements of high-velocity flight. 

Registration for the Emerging AM Materials still open! The 1.5 hour webinar kicks off on Wednesday, August 2nd at 11am EST.


This webinar provides a wonderful opportunity to learn...

  • why AM refractory alloys (tungsten, rhenium, WRe, tantalum, and C103) are gaining significant traction in medical, nuclear energy, and aerospace.


  • what new alloys and manufacturing processes are enabling extreme environment robotic space exploration.


  • why is there a resurgence of interest in printable oxide dispersion strengthened (ODS) alloys.
Free Registration

Annual team building event gets messy



On July 22, Elementum 3D employees joined forces to finish the “Tough Mudder,” located in Byers, Colorado. This was the fourth straight year the “Elementum 3D TOUGH” team has crossed the finish line.

 

The Tough Mudder event is more than just a grueling 10-mile course with 30 uniquely challenging obstacles, it is our annual teambuilding event. It a messy, sloppy and muddy course filled with extremes that tests everyone’s stamina, agility, and skill, but it also builds connections with teammates from different departments, improves company morale, and inspired some friendly competition with between teammates and departments

Upcoming Events

WEBINARS

Emerging AM Materials: August 2 | 11am - 12:30pm ET


TRADESHOWS

FORMNEXT: November 7-10 | Frankfurt, Germany | Booth 11.1-C62


JPL qualifies Elementum 3D A6061-RAM2 material for flight hardware production

The quest for new materials for use in space exploration has found success in additive manufacturing.


On April 21, 2021, NASA released two technical standards: NASA-STD-6030, Additive Manufacturing (AM) Requirements for Crew Spacecraft Systems, and NASA-STD-6033, Additive Manufacturing Requirements for Equipment and Facilities Control. The sole purpose of these standards is to integrate AM into the development and manufacture of flight hardware to reduce cost, optimize mission capabilities and advance aeronautic applications.


Fast forward to 2023, NASA/JPL recently announced that they have established a flight-qualified process for producing hardware using metal AM materials. A6061-RAM2 and Ti64 are the first materials approved for the infusion of AM technology into spacecraft and rovers. The manufacturing of flight hardware using a qualified additive manufacturing process are conducted at JPL's additive manufacturing center. The rigorous qualifying process satisfies the NASA-STD-6030 requirements. The QMP ensures a consistent process using specified controls of the raw material feedstock and an evaluation of the process capability for each AM machine, all which are documented in a configuration controlled QMP record.



Elementum 3D is thankful for NASA/JPL. Their relentless drive to advance the complexity of spaceflight hardware is setting the bar for the rest of the AM community. Their uncompromising approach to quality is what all AM disciplines need to strive for to produce greater AM adoption.

We've updated the IN625-RAM2 datasheet

The Elementum 3D team continues the improve its products for the ever-changing additive manufacturing landscape. The updated IN625-RAM2 datasheet adds new high-productivity print parameters to provide optimal parts production needs for any customer. The RAM constituents added to IN625 add a yield strength boost for as-printed parts allowing for quicker parts development and production without needing heat treatment. The team has also developed 60µm parameters that yield higher surface finishes than the previously offered 40µm parameters.


Here are the updates:



  • The addition of multiple layer thickness printing parameters
  • Mechanical properties at different layer heights
  • Density
  • Surface finish

Elementum 3D

400 Young Court, Unit 1

720-545-9016

www.elementum3d.com

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