Heat Treatment of Titanium and Titanium Alloys
- Aerospace Material Specification
- AMSH81200
- Issued
Scope
Recommended Content
| Aerospace Material Specification | Titanium Alloy, Sheet 6Al - 2Sn - 2Zr - 2Mo - 2Cr - 0.15Si Annealed |
| Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Unnamed Dataset 4 | ||
| Unnamed Dataset 5 | ||
| Unnamed Dataset 6 | ||
| TABLE I | Solution heat treating schedule for raw materials and semi-finished parts | |
| TABLE II | Maximum quench delay. | |
| TABLE III | Aging schedule | |
| TABLE IV | Stress relief schedule | |
| TABLE V | Annealing Schedule | |
| Unnamed Dataset 12 | ||
| TABLE VI | Approximate beta transus temperatures. | |
| TABLE VII | Required mechanical tests. |
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 |
|---|---|
| AMS2750 | PYROMETRY |
| AMS2801 | HEAT TREATMENT OF TITANIUM ALLOY PARTS |
| ASTME148 | This document is not part of the subscrption. |
| ASTME290 | This document is not part of the subscrption. |
| ASTME3 | This document is not part of the subscrption. |
| ASTME8 | This document is not part of the subscrption. |
| MIL-STD-45662 | This document is not part of the subscrption. |