This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Heat Treatment of Titanium and Titanium Alloys
- Aerospace Material Specification
- AMSH81200D
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers the heat treatment of titanium and titanium alloy mill products (raw material), including wrought and cast products, by material producers. This specification also covers furnace equipment requirements, test procedures, and general information for heat treating procedures, heat treating temperatures, and material test procedures for the heat treatment of titanium and titanium alloys. It also describes procedures that, when followed, have produced the desired properties within the limitations of the respective alloys.
Rationale
AMS-H-81200D revises the temperature uniformity (3.2.1.7).
Recommended Content
| Aerospace Material Specification | Heat Treatment of Titanium Alloy Parts |
| Aerospace Material Specification | Shot Peening |
| Aerospace Material Specification | Heat Treatment Wrought Nickel Alloy and Cobalt Alloy Parts |
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 |
|---|---|
| AMS2750F | Pyrometry |
| AMS2801B | 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. |
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.