Titanium 6-6-2
Titanium 6-6-2, AMS 4918, is a high-performance titanium alloy, specifically Ti-6Al-6V-2Sn, known for its exceptional strength, toughness, and resistance to elevated temperatures. With a composition that includes aluminum, vanadium, and tin, AMS 4918 offers a tensile strength of 145-155 ksi and a yield strength of 135-170 ksi, making it ideal for demanding applications and high-performance structural uses. Its balanced combination of elements ensures reliability and durability in critical environments.
United Performance Metals stocks Ti-6-6-2 plate sizes 0.250" - 4.000". Some of the common applications for this product include aircraft structures, engine components, landing gear parts, heat exchangers, and pressure valves.
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Inventory Size Ranges for Titanium 6-6-2
| Type | Thickness | AMS Standards | UNS | Get a Quote |
|---|---|---|---|---|
| Plate | 0.250" - 4.000" | AMS 4918 | UNS R56620 | Get a Quote |
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Characteristics of Titanium 6-6-2
This grade of titanium alloy can be heated treated to higher strengths and heavier section sizes compared to that of Ti-6AL-4V. Ti-6-6-2 possesses excellent strength, corrosion resistance, and a medium level of fabricability.
Working with Titanium 6-6-2
Titanium 6-6-2 is readily finish-forged from 1650°F (899°C) with a minimum finishing temperature of 1,400°F (760°C). Minimum reductions of about 35% in the alpha-beta range are recommended to obtain specification properties.
This product can be difficult to cold form due to its high strength and large amount of springback. Annealed material may be hot-formed up to 1,500°F (816°C). Hot sizing or creep forming is generally performed at 1,000 - 1,300°F (538 - 704°C), however, any heating above 1,100°F (593°C) results in surface contamination and the contaminated layer must subsequently be removed by machining or proper pickling.
Titanium 6-6-2-can be successfully welded using the inert gas shielded, fusion-welding process, but the heat affected zone will have considerably lower ductility and toughness compared to the parent metal. Some improvement in ductility can be obtained by using commercially pure titanium filler wire to dilute the beta-stabilizing elements, and by using a post-weld treatment.
Other industry standards we comply with:
- MMS 1203
- DMS 1879
Common Trade Names
- Ti-6-6-2
- Ti-6AL-6V-2Sn
- ATI 6-6-2â„¢ (Allegheny Technologies)
Industry Applications for Titanium 6-6-2
- Aircraft structural components
- Engine components
- Landing gear parts
- Heat exchangers
- Pressure valves
Chemical Composition
| Element | Min | Max | |
|---|---|---|---|
| Al | Aluminum | 5.0 | 6.0 |
| C | Carbon | - | 0.05 |
| V | Vanadium | 5.0 | 6.0 |
| N | Nitrogen | - | 0.04 |
| Sn | Tin | 1.5 | 2.5 |
| H | Hydrogen | - | 0.015 |
| Fe | Iron | 0.35 | 1.0 |
| Y | Yttrium | - | 0.005 |
| Cu | Copper | 0.35 | 1.0 |
| O | Oxygen | - | 0.20 |
| Ti | Titanium | - | Balance |
| - | Other | 0.40 | - |
Physical Properties
| Property | Value |
|---|---|
| Density | 4.54 g/cm3 (0.14 lb/in3) |
| Melting Point | ~1,650°C (3,000°F) |
| Modulus of Elasticity | 114 GPa (16.5 x 106 psi) |
| Thermal Conductivity | ~6.6 W/m·K |
Mechanical Properties
| Tensile Strength | Yield Strength | Elongation Percent |
|---|---|---|
145-155 ksi | 135-170 ksi | 6-10% |