Closed-die forgings
Near-net shapes for impellers, fittings and frames, with grain flow following the part contour.
2B50 is a refined version of the 2A50 forging alloy, with chromium and titanium added for finer grain and more consistent properties in complex die forgings. It is used for aircraft fittings, engine-casing parts and impellers built to GB and HB standards. Metline supplies 2B50-T6 die and free forgings with full certification to customers worldwide.

2B50, formerly LD6, shares the Al-Mg-Si-Cu base of 2A50 but adds 0.01 – 0.20 % chromium and a controlled 0.02 – 0.10 % titanium. Chromium suppresses recrystallisation and coarse surface grain in forgings, while titanium refines the cast grain of the billet. The result is a forging alloy with more uniform properties in complex shapes.
Like 2A50, it has excellent hot plasticity and fills thin ribs and deep cavities well, so it is used for complex closed-die forgings: airframe fittings, joints, frames, engine-casing parts, guide-vane rings and compressor impellers. Where heat resistance above about 150 °C is needed, 2A70 or 2A80 are the usual alternatives.
A note on data: some published sheets show 2B50 with 1.4 – 1.8 % magnesium and around 1 % nickel. That is the 2A70 composition, not 2B50, and should be corrected before ordering.
Limits per GB/T 3190.
| Element | Limit | Comment |
|---|---|---|
| Copper (Cu) | 1.8 – 2.6 | Strengthening |
| Silicon (Si) | 0.7 – 1.2 | Forms Mg2Si |
| Magnesium (Mg) | 0.40 – 0.80 | Strengthening |
| Manganese (Mn) | 0.40 – 0.80 | Grain control |
| Chromium (Cr) | 0.01 – 0.20 | Inhibits recrystallisation and coarse grain |
| Titanium (Ti) | 0.02 – 0.10 | Grain refiner |
| Iron (Fe) | 0.7 max | Impurity |
| Nickel (Ni) | 0.10 max | Impurity (Fe + Ni ≤ 0.7) |
| Zinc (Zn) | 0.30 max | Impurity |
| Others each / total | 0.05 / 0.10 | |
| Aluminium | Remainder |
2B50 forgings are specified at the same minimum levels as 2A50 in the common aviation standards, with the benefit of more uniform results across complex parts.
| Direction | Property | Free forgings (T6) | Die forgings (T6) |
|---|---|---|---|
| Longitudinal (L) | Tensile strength Rm | ≥ 365 MPa | ≥ 380 MPa |
| Longitudinal (L) | Yield strength Rp0.2 | — | ≥ 275 MPa |
| Longitudinal (L) | Elongation A5 | ≥ 8 – 9 % | ≥ 10 – 11 % |
| Long transverse (LT) | Tensile strength Rm | ≥ 345 MPa | ≥ 365 MPa |
| Long transverse (LT) | Elongation A5 | ≥ 6 % | ≥ 7 % |
| Short transverse (ST) | Tensile strength Rm | ≥ 335 MPa | ≥ 345 MPa |
| Short transverse (ST) | Elongation A5 | ≥ 4 % | ≥ 5 % |
| — | Hardness | ≈ 95 HBS | ≈ 100 HBS |
Minimum values as commonly quoted from GJB 2351 and HB 5204 for forgings of typical section; limits depend on section thickness and the standard revision. The ordered standard and certificate govern.
Near-net shapes for impellers, fittings and frames, with grain flow following the part contour.
Blocks, discs and stepped shapes for machining, used for prototypes and low volumes.
Upset and ring-rolled blanks for rotating and casing parts.
Round and square forged bar for heavy machined components.
Forgings are produced through qualified forging partners to your drawing. Achievable size and weight depend on the forging route and heat-treatment equipment, so feasibility is confirmed for each drawing rather than quoted from a generic table.
| Factor | 2B50 | 2A50 | 2A70 | 2A14 / 2014 |
|---|---|---|---|---|
| Forgeability | Excellent | Excellent | Good | Good |
| Grain uniformity | Better (Cr, Ti) | Good | Good | Good |
| Heat resistance | Fair | Fair | Very good | Fair |
| Room-temperature strength | Medium–high | Medium–high | Medium–high | High |
Choose 2B50 over 2A50 when a complex forging needs consistent properties throughout; choose 2A70 when the part runs hot; choose 2A14 when maximum room-temperature strength matters.
2B50 adds chromium (0.01 – 0.20 %) and controlled titanium (0.02 – 0.10 %) to the 2A50 base, giving finer, more uniform grain and more consistent properties in complex forgings.
Only as an impurity (0.10 % max). Data sheets that show around 1 % nickel and 1.4 – 1.8 % magnesium are describing 2A70, not 2B50.
Die forgings are commonly specified at about 380 MPa minimum tensile and 275 MPa yield strength longitudinally, with lower transverse values.
Moderately. As a copper-bearing alloy it should be anodised, conversion coated or painted for aerospace service.
Yes. Metline supplies forgings worldwide with EN 10204 3.1 certificates, inspection reports and export packing.
Send the drawing, standard and quantity. We will confirm feasibility, inspection and a delivered price.