Electron-Beam Welding For Fatigue Critical Applications
- Aerospace Material Specification
- AMS2680C
- Reaffirmed
Scope
Recommended Content
Aerospace Material Specification | Welding, Electron-Beam |
Aerospace Material Specification | Steel, Corrosion-Resistant, Investment Castings 16Cr - 4.1Ni - 0.28Cb - 3.2Cu Homogenization and Solution Heat Treated or Homogenization, Solution, and Precipitation Heat Treated |
Aerospace Material Specification | Titanium Alloy, Investment Castings 6Al - 4V 130 UTS, 120 YS, 6% EL Hot Isostatically Pressed Anneal Optional or When Specified |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | Minimum Parameters To Be Recorded in Welding Procedure | |
TABLE 2A | Internal Discontinuity Limits, Inch/Pound Units | |
TABLE 2B | Internal Discontinuity Limits, SI Units | |
TABLE 3A | Effective Areas of Discontinuities, Inch/Pound Units | |
TABLE 3B | Effective Areas of Discontinuities, SI Units |
Issuing Committee
AMS B Finishes Processes and Fluids Committee
The committee of Finishes, Processes, and Fluids, AMS Committee B, shall prepare, coordinate, and revise documents related to processing technology, such as plating, brazing, coatings and compounds, through the participation of process suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace processes.