Subscribe to our Newsletter
Model No: Ti-6Al-2Sn-4Zr-2Mo Forging
AMS 4976 / UNS R54620 / Ti-6Al-2Sn-4Zr-2Mo Forging
The AMS 4976 specification covers a Ti-6Al-2Sn-4Zr-2Mo alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal diameter or least distance between parallel sides and 9 in2 (58 cm2) and under in cross-sectional area and forging stock of any size.
Delivery :
FOB
minimum order :
100 kilograms
Supply Ability :
5000Tonkilograms / Month
Stock Time :
7-10Day
Country of Origin :
CHINA
Quantity :
The AMS 4976 specification covers a Ti-6Al-2Sn-4Zr-2Mo (UNS R54620) alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal diameter or least distance between parallel sides and 9 in2 (58 cm2) and under in cross-sectional area and forging stock of any size. The material specification also calls out Solution and Precipitation Heat Treated condition also known as Annealed state.
Titanium alloy Ti6242 has high mechanical properties and especially creep resistance up to about 500°C. Its low density, high strength and good toughness also give it an advantage in moving and high temperature applications.
Stainless has a number of qualified sources in stock and a variety of diameters to suit your application needs. This product can also be custom made or cut into slugs by our service centres. Each material is delivered with its producer’s certificate of origin in order to guarantee you total transparency and complete traceability.
Chemical composition
| Element | Content % |
| Al | 5.50-6.75 |
| Sn | 1.80-2.20 |
| Zr | 3.60-4.40 |
| Mo | 1.80-2.20 |
| C | <0.05 |
| Fe | <0.10 |
| Si | 0.06-0.10 |
| O | <0.15 |
| H | <0.0125 |
| Y | <0.005 |
| N | <0.05 |
| Ti | solde |
Forgeability/Usability
The grade can be hot forged, the beta transus is close to about 1000°C. Machining of this grade requires sufficient coolant to limit heating.
Heat treatments
From an annealed condition, quenching followed by ageing (STA) heat treatment is possible on this grade. For a diameter of 120mm, a treatment of the type 980°C/1h/Air followed by ageing at 593°C/8h/Air will enable a level of mechanical strength of the order of 980 MPa to be obtained at room temperature and the hot strength at 480°C will be close to 700 MPa with an elongation generally higher than 12%.
Applications
- Structural Components: In the fuselage, 6Al-2Sn-4Zr-2Mo may be used in the manufacture of various structural components, such as beams, frames, and stringers. These components help to give the fuselage its strength and stiffness and are responsible for resisting loads and stresses that are imposed on the aircraft during flight.
- Engines: In an aircraft engine, 6Al-2Sn-4Zr-2Mo may be used in the manufacture of various structural components, such as turbine blades, discs, and vanes. These components are subjected to high temperatures and stresses during operation, and the use of 6Al-2Sn-4Zr-2Mo helps to ensure that they are strong and able to withstand these conditions.
- Other Mechanical Components: In a missile, 6Al-2Sn-4Zr-2Mo may be used in the manufacture of structural components, such as the body and fins, as well as in the guidance system and propulsion system. The structural components of a missile must be strong and able to withstand the stresses of flight, and the use of Ti-6Al-2Sn-4Zr-2Mo helps to ensure that these components are able to do so.
Lork Group is metal material manufacturer and exporter in China
The experts at Lork Group are ready to help you choose the most suitable type of Metal for your .
We have built a reputation as a trusted partner for quality materials, distributing numerous grades of stainless steel,nickel alloy,Precision Alloy andhard-to-find metals. Our raw metal bars, rings, plates, pipes, and tubing are available from stock.
To learn more about the Lork Group metal difference and our material offerings stainless steel and super alloy, contact us or request a quote today.
