This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Gamma Titanium-Aluminide Powder for Additive Manufacturing Ti - 48Al - 2Nb - 2Cr
- Aerospace Material Specification
Published June 01, 2021 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers a heat-resistant gamma titanium aluminide alloy in the form of pre-alloyed powder.
This SAE Aerospace Material Specification is intended to provide a specification that will allow powder of gamma titanium-aluminide alloy Ti - 48Al - 2Nb - 2Cr to be procured in the aerospace supply chain for use in additive manufacturing.
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|Table 1||Composition [wt.%]|
|Table 2||Particle size distribution based on powder classification|
|Table 3||Testing requirements|
AMS AM Additive Manufacturing Metals
Welcome to the SAE AMS AM, Additive Manufacturing public forum area.Scope: AMS AM is a technical committee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain aerospace material and process specifications and other SAE technical reports for additive manufacturing, including precursor material, additive processes, system requirements and post-build materials, pre-processing and post-processing, non-destructive testing and quality assurance.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.