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Laser-Powder Bed Fusion (L-PBF) Produced Parts, Steel, Corrosion and Heat-Resistant, 15.0Cr - 4.5Ni - 3.5Cu - 0.30Nb (15-5), Hot Isostatic Pressed, Solution and Precipitation Heat Treated (H1025)

2024-02-26
WIP
AMS7069
This specification covers a corrosion-resistant steel alloy in the form of parts produced by laser-powder bed fusion (L-PBF) that are subjected to post-deposition hot isostatic press (HIP), solution and precipitation heat treated (H1025) condition. The application is for parts typically requiring corrosion resistance and high strength up to 600 °F (316 °C) with good ductility and strength, but usage is not limited to such applications.
Standard

Machine Qualification for Fusion-Based Metal Additive Manufacturing

2024-02-16
WIP
AMS7032A
This standard has notes/guidance narratives interspersed throughout. These notes/guidance narratives are identified by a header and by text in italics.This standard defines a series of requirements that results in a specific AM machine qualified to produce material (see GN1) in compliance to an aerospace materials specification. The machine control and/or configuration types are discussed in the next sections.
Standard

Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate, Ti-6Al-4V, Stress Relieved

2024-01-19
WIP
AMS7004A
This specification covers preforms fabricated up through 5.5 inches (140 mm) inclusive in deposition width thickness (see 8.2.5) using a Plasma Arc Directed Energy Deposition (PA-DED) additive manufacturing process on a Ti-6Al-4V substrate that are subjected to post-deposition stress relief heat treatment. This is a wire fed additive manufacturing process. If required by the CEO, preforms may require subsequent machining to meet requirements for their intended final part application.
Standard

In-Situ Process Monitoring Considerations for Metal Fusion Additive Manufacturing

2023-12-01
WIP
ARP7068
This document defines a recommended practice for addressing metal additive manufacturing (AM) In-Situ Process Monitoring (ISPM) for all fusion-based metal AM machines. In general, this applies to powder bed fusion (PBF) and wire- or powder-fed directed energy deposition (DED) technologies. Plasma, electron beam or lasers are applicable energy source(s).
Standard

Additional Guidance for Metal Powder Feedstock for Additive Manufacturing

2023-10-11
WIP
AIR7359
This document is a collection of comments on topics relevant to AMS powder feedstock production and procurement. In some instances it provides explanation of characteristics not controlled in AMS-AM powder feedstock specifications and the rationale for exclusion (e.g. limitation of applicability or maturity of standardized inspection techniques). In other cases it provides additional context on the reason for structuring requirements in AMS documents one way instead of other available options.
Standard

Niobium Alloy Powder for Additive Manufacturing, Nb - 10Hf - 1Ti

2023-04-20
WIP
AMS7060
Form This specification covers a high elevated temperature strength niobium alloy in the form of pre-alloyed powder. Application This powder has been used typically as feedstock in additive manufacturing of components. Material properties are influenced by the additive manufacturing process and subsequent heat treatment, see the final material specification for application guidance.
Standard

Powder Sampling Strategies for Closed Loop Additive Manufacturing Equipment

2023-04-20
WIP
ARP7302
This SAE Aerospace Recommended Practice (ARP) describes methods to collect powder from an additive manufacturing (AM) powder bed process when executed by closed loop equipment. The methods recommended here are meant to provide opportunities to demonstrate conformance to powder specification requirements when required as part of process control for the associated AM activity.
Standard

Copper Alloy Powder for Additive Manufacturing, Cu - 1Cr - 0.15Zr

2023-04-19
WIP
AMS7059
Form This specification covers a moderate-to-high conductivity and strength copper alloy and improved wear resistance in the form of pre-alloyed powder. Application This powder has been used typically as feedstock in additive manufacturing of components. Material properties are influenced by the additive manufacturing process and subsequent heat treatment, see the final material specification for application guidance.
Standard

Nickel Alloy Powder for Additive Manufacturing, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb

2023-04-19
WIP
AMS7001A
Form This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder. Application This powder has been used typically as feedstock in additive manufacturing of components. Material properties are influenced by the additive manufacturing process and subsequent heat treatment, see the final material specification for application guidance.
Standard

Cold Spray Additive Manufacturing (CSAM) Process

2023-01-25
WIP
AMS7057
This specification establishes process controls for the repeatable implementation of the Cold Spary Additive Manufacturing (CSAM) process for the manufacturing of metallic and metal-non-metal blend components. It is intended to be used for aerospace parts (preforms) manufactured using Additive Manufacturing (AM) metals and metal-non-metal blend materials, but usage is not limited to such applications.
Standard

Laser Powder Bed Fusion (LPBF) Produced Parts, 3.5Cr – 7.5Ni – 16.3Co – 1.75Mo – 0.2W – (0.10 – 0.15 C)

2023-01-18
WIP
AMS7056
This specification covers a premium aircraft-quality alloy steel in the form of parts produced by laser powder bed fusion (LPBF) that are subjected to post-deposition stress relief (SR; optional), hot isostatic press (HIP), solution heat treatment, and tempering aging operations. Parts may require subsequent machining, or surface finishing to meet specific application requirements, which are not covered in this specification.
Standard

GUIDANCE ON THE USE OF THE AMS-AM STANDARDS FRAMEWORK

2022-11-29
WIP
ARP7066
This document describes and gives examples of how the SAE-AMS-AM standards framework can be used to establish the proper procedures and controls for additively manufacturing aerospace conponents.
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