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Titanium Alloy Bars, Wire, Forgings, and Rings 6Al - 6V - 2Sn Annealed
- Aerospace Material Specification
- AMS4978H
- Revised
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings 4.000 inches (101.60 mm) and under in diameter, or least distance between parallel sides and stock of any size for forging or flash welded rings (see 8.6).
Rationale
AMS4978G results from a Five-Year Review and update of this specification that includes the addition of ASTM E539 and ASTM E2994 (3.1) and removal of sample size allowance for hydrogen of Table 1 (covered by ASTM E1447).
Recommended Content
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Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1 | Composition | |
| Table 2A | Tensile properties, inch/pound units | |
| Table 2B | Tensile properties, SI units |
Issuing Committee
AMS G Titanium and Refractory Metals Committee
The committee of Titanium, Beryllium, and Refractory Materials, AMS Committee G, is responsible for preparation, revision, review and approval of documents related to aerospace application of these materials. Included are titanium, beryllium, and refractory metallic such as molybdenum, tantalum, and columbium. The committee provides a forum for interchange of experience and ideas among industry representatives, both suppliers and users, along with interested government agencies, to ensure the utility, proper technical content, and industry acceptance of published documents.
Reference
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