Titanium Alloy Bars, Forgings, and Rings 6al 4v Extra Low Interstitial (Eli) Duplex Annealed, Fracture Toughness
- Aerospace Material Specification
This specification covers a titanium alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
These products have been used typically for parts requiring a combination of high tensile strength up to 750 degrees F (399 degrees C) and high fracture toughness, but usage is not limited to such applications.
|Aerospace Material Specification||Titanium Alloy Bars, Forgings, and Rings 6Al - 4V Extra Low Interstitial (ELI) Duplex Annealed, Fracture Toughness|
|Aerospace Material Specification||Steel, Corrosion and Heat Resistant, Forgings 12.5Cr (410) Enhanced Fracture Toughness, Annealed|
|Aerospace Material Specification||Steel, Sheet, Strip, and Plate 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) (H-11)|
Data Sets - Support Documents
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.