Heat Treatment of Titanium and Titanium Alloys
- Aerospace Material Specification
- AMSH81200C
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Heat Treatment of Titanium and Titanium Alloys |
| Aerospace Material Specification | Steel, Corrosion-Resistant, Sand and Centrifugal Castings 16Cr - 4.1Ni - 0.22Cb (Nb) - 2.8Cu Solution Heat Treated |
| Aerospace Material Specification | Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion- and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed |
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 1 | SOLUTION HEAT TREATING SCHEDULE FOR RAW MATERIALS AND SEMI-FINISHED PARTS | |
| TABLE 2 | MAXIMUM QUENCH DELAY | |
| TABLE 3 | AGING SCHEDULE | |
| TABLE 4 | STRESS RELIEF SCHEDULE | |
| TABLE 5 | ANNEALING SCHEDULE | |
| Unnamed Dataset 12 | ||
| TABLE 6 | APPROXIMATE BETA TRANSUS TEMPERATURES | |
| TABLE 7 | 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 |
| ASTME1447 | 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. |
| ASTME8/E8M | This document is not part of the subscrption. |