Titanium Alloy Castings, Investment 6Al - 4V Hot Isostatic Pressed, Anneal Optional
- Aerospace Material Specification
- AMS4991F
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Titanium Alloy, Investment Castings 6Al - 4V 130 UTS, 120 YS, 6% EL Hot Isostatically Pressed Anneal Optional or When Specified |
Aerospace Material Specification | Casting, Structural Investment, Titanium Alloy 6Al - 4V Hot Isostatically Pressed |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Table 1 | Composition | |
Table 2 | Minimum tensile properties | |
Table 3 | Minimum tensile properties | |
Table 4 | Minimum tensile properties | |
Table 5A | Negative surface discontinuity limits, inch/pound units | |
Table 5B | Negative surface discontinuity limits, SI units | |
Table 6A | Shrinkage limits, inch/pound units | |
Table 6B | Shrinkage limits, SI units | |
Table 7 | Gas holes and foreign material limits | |
Table 8 | Background discontinuity limits | |
Table 9 | Surface blending limits |
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
Number | Title |
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AMS2249 | CHEMICAL CHECK ANALYSIS LIMITS Titanium and Titanium Alloys |
AMS2694 | REPAIR WELDING OF AEROSPACE CASTINGS |
AMS2750 | PYROMETRY |
AMS2804 | IDENTIFICATION Castings |
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