Furnace Brazing of Parts in a Vacuum Atmosphere
- Aerospace Material Specification
- AMS2678
- Issued
Scope
Rationale
Recommended Content
Aerospace Material Specification | Furnace Brazing of Parts in a Vacuum Atmosphere |
Aerospace Material Specification | Aluminum Alloy Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr 7075: (-T73 Sheet, -T7351 Plate) Solution Heat Treated and Overaged |
Aerospace Material Specification | Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | PRESSURE VERSUS RECOMMENDED GAUGE TYPE | |
TABLE 2 | THERMOCOUPLE TYPES VERSUS MAXIMUM OPERATING TEMPERATURE | |
TABLE 3 | FILLER METALS |
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.
Reference
Number | Title |
---|---|
AMS2750 | Pyrometry |
AMS2769 | Heat Treatment of Parts in a Vacuum |
ARP1962 | CERTIFICATION OF HEAT TREATING PERSONNEL |
NFPA86D | This document is not part of the subscrption. |