Ti-6-2-4-6 is a near-alpha/alpha-beta titanium alloy built for elevated-temperature jet engine components that need both strength and creep resistance in the same part. Its composition, roughly 6% aluminum, 2% tin, 4% zirconium, and 6% molybdenum, gives it a higher beta-stabilizer content than the elevated-temperature near-alpha alloys that came before it, which allows it to be heat treated to higher strength levels while still retaining the creep resistance that tin and zirconium additions provide at operating temperature.
That balance of properties made Ti-6-2-4-6 a popular choice for compressor blades, discs, and other rotating components in gas turbine engines that operate at sustained elevated temperatures, typically up to around 450°C (840°F). Compared to simpler near-alpha alloys, it offers a useful strength advantage without sacrificing the long-term stability those components need to survive years of thermal cycling in service.
On the machine tool, Ti-6-2-4-6 sits above standard Ti-6Al-4V in difficulty, reflecting both its higher strength and its creep-resistant microstructure, though it remains more workable than the very high-strength near-beta grades used in structural aerospace applications.
| Standard | Designation |
|---|---|
| UNS | R56260 |
| SAE / AMS | 4981 |
| Common Name | Ti-6-2-4-6 |
| Element | Content |
|---|---|
| Aluminum (Al) | 5.5 – 6.5% |
| Molybdenum (Mo) | 5.5 – 6.5% |
| Zirconium (Zr) | 3.6 – 4.4% |
| Tin (Sn) | 1.8 – 2.2% |
| Silicon (Si) | 0.06 – 0.10% |
Ti-6-2-4-6 combines the standard difficulties of titanium machining with the added toughness of an alloy engineered to resist creep at elevated temperature. Titanium's thermal conductivity runs at roughly a sixth of steel's, so heat generated in the cut concentrates at the tool tip instead of dissipating into the chip. The molybdenum and zirconium content that give this alloy its creep resistance also mean it resists softening at the temperatures generated during cutting, which accelerates diffusion wear on the tool compared to standard alpha-beta titanium.
Its low modulus of elasticity still applies, so the workpiece deflects more under cutting pressure than steel would, making rigid workholding and short tool overhang essential to avoid chatter and dimensional drift. Titanium's tendency to work-harden under a rubbing or dull edge also carries over, so feed rates need to stay consistently high enough to shear cleanly beneath any hardened surface layer rather than rubbing across it.
Within the titanium family, Ti-6-2-4-6 sits above standard Ti-6Al-4V in difficulty but below the very high-strength near-beta grades such as Ti-5553 and Ti-55531. Expect moderately reduced speeds and shorter tool life relative to Grade 5, with flood coolant and sharp, well-supported cutting edges playing an important role in tool survival.
| Operation | Vc (m/min) | Vc (SFM) |
|---|---|---|
| Turning | 60 – 80 | 200 – 260 |
| Milling | 45 – 60 | 150 – 200 |
| Parting | 35 – 50 | 110 – 160 |
| Grooving | 50 – 70 | 160 – 230 |
| Drilling | 50 – 70 | 160 – 230 |
Values assume favorable cutting conditions: a well-matched insert grade, maximum rigidity in tool and workpiece clamping, good-quality raw material, short tool overhang, and flood coolant. Reduce further for interrupted cuts, thin-wall sections, or reduced rigidity.
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM524 | CVD | S05 – S10 |
| FM2533 | CVD | S15 |
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM2543 | CVD | S20 |
| FM2553 | CVD | S30 |
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM2533 | CVD | S10 |
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM125 | PVD | S15 – S35 |
Ready to cut Ti-6-2-4-6? Shop FM Carbide inserts matched to this alloy's turning, parting, grooving, and milling requirements.
Shop Turning & Grooving Inserts Shop Milling Inserts| Parameter | Value |
|---|---|
| Honing Size | 0.02 – 0.05 mm / 0.001 – 0.002" |
| Rake Angle | 13° – 18° |
| Land Angle | Neutral |
| Land Width | 0.10 – 0.20 mm / 0.004 – 0.008" |
| Ground Insert | Recommended |