Ti-10V-2Fe-3Al (UNS designation R56410), also known as Ti 10-2-3, is a non-ferrous near-beta titanium alloy featuring an excellent combination of strength, ductility, fracture toughness and high cycle fatigue strength. It is typically used in the aerospace industry for critical aircraft structures, such as landing gear.[1]
Ti-10V-2Fe-3Al Chemistry[2]
| V | AL | Fe | O | C | N | H | Y | Ti | Remainder Each | Remainder Total | |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Min | 9 | 2.6 | 1.6 | -- | -- | -- | -- | -- | -- | -- | -- |
| Max | 11 | 3.4 | 2.22 | .13 | .05 | .05 | .015 | .005 | Balance | .1 | .3 |
Ti-10V-2Fe-3Al Markets[3]
- Automobile
Ti-10V-2Fe-3Al Applications[4]
- Airframe components
- Landing gear components
Ti-10V-2Fe-3Al Specifications[5]
- AMS: 4983, 4984, 4986, 4987
- UNS: R56410
References
- ↑ "TIMET 10-2-3 Titanium Alloy". MatWeb.
- ↑ "Ti-10V-2Fe-3Al Titanium Alloy". Rickard Metals.
- ↑ "Titanium Alloy Guide" (PDF). RMI Titanium Company.
- ↑ "Titanium Alloy Guide" (PDF). RMI Titanium Company.
- ↑ "Ti-10V-2Fe-3Al Titanium Alloy". Rickard Metals.
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