This specification covers use of the Laser-Wire Deposition process to additively manufacture Titanium 6Al4V products, with anneal and age post-processing.
1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant Hastelloy in the form of pre-alloyed powder. 1.2 Application This powder is intended to be used for the additive manufacturing of aerospace parts via a powder bed process, but usage is not limited to such applications.
Fused Filament Fabrication - Stratasys Fortus 900mc Plus with Type 1, Class 1, Grade 1, Natural Material
This slash sheet is used in conjunction with the Am Polymer base specification AMS 7100 and provides the unique and specific process information for the Ultem 9085 Material processes using the Fortus 900+ machine.
This specification establishes process controls for the repeatable production of aerospace parts by Electron Beam Powder Bed Fusion (EB-PBF). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
AMS for 718 powder to be used primarily for production of additively manufactured components. The powder could also be used for non-AM applications.
This specification establishes the certification requirements for materials to be used in Fused Deposition Modeling (FDM) or other material extrusion additive manufacturing production for aerospace components. This specification outlines the technical information, production guidelines and documentation requirements for FDM® material manufacturer. It will initially target several grades of PEI Copolymer (ULTEMTM 9085) and an enhance flow PEI (ULTEMTM 1010) materials as certified material examples.
This specification establishes the critical controls and requirements for the production of reliable, repeatable, reproducible aerospace parts by Fused Deposition Modeling (FDM) or other material extrusion production. This procedure will establish guidelines that FDM® System users shall follow to approve new machines, processes, materials, etc. Specifically, this specification covers the configuration of the machine, operating software, machine calibration, machine and build parameters, and testing methodology required to create certified additively manufactured aerospace parts. This specification also outlines the FDM system user responsibility for following the established guidelines and documentation requirements. The Stratasys Fortus® 900mc Plus Printer with ULTEMTM 9085 will be used as an example to demonstrate the control needed to create SAE certified aerospace parts manufactured using FDM systems.
This specification establishes process controls for the repeatable production of aerospace parts by High Deposition Rate (HDR). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
This document summarizes data guidelines to establish statistically determined minimum values for the mechanical properties (i.e., static mechanical property) for additive manufactured (AM) metals published in SAE AMS specifications. Such values are not intended to be used in designing actual parts.
To enable consistency across AM specifications the committee considers it necessary to establish definitions for common terms that will be used in applicable AM specifications.
Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate-Ti6Al4V-Stress Relieved
This specification covers titanium 6Al-4V preforms fabricated using Rapid Plasma Deposition™ (RPD™) additive manufacturing process on a Ti-6Al-4V substrate that are subject to post deposition stress relieve.