Material Ti-8Al-1Mo-1V

Technical Reference Library

Ti-8Al-1Mo-1V Titanium Alloy

UNS R54810 AMS 4915 Alloy Type Near-Alpha

Material Overview

Ti-8Al-1Mo-1V is a near-alpha titanium alloy defined by its unusually high 8% aluminum content, paired with small, roughly equal additions of molybdenum and vanadium that provide just enough beta-phase stabilization to aid processing without turning the alloy into a true alpha-beta grade. That heavy alpha-side loading gives the alloy the lowest density of any commercially significant titanium alloy, along with good strength and creep resistance that hold up well at elevated service temperatures.

That combination of low weight and elevated-temperature strength retention is what makes Ti-8Al-1Mo-1V a long-standing choice for jet engine compressor sections — forged compressor blades and discs in particular, where every gram of rotating mass matters and the material has to keep its strength through sustained thermal cycling. It's a purpose-built alloy for that specific role rather than a general-purpose titanium grade.

International Designation Equivalents

Standard Designation
UNS R54810
AMS 4915 (sheet, strip, plate)
AMS 4972 (bar, wire, ring)

Chemical Composition

Element Content
Aluminum (Al) 7.35 – 8.35%
Molybdenum (Mo) 0.75 – 1.25%
Vanadium (V) 0.75 – 1.25%
Iron (Fe) 0.30% max
Oxygen (O) 0.15% max
Carbon (C) 0.08% max
Nitrogen (N) 0.05% max
Hydrogen (H) 0.0125% max
Titanium (Ti) Balance

Machinability Explained

Ti-8Al-1Mo-1V carries the same core titanium machining challenges as any other grade — low thermal conductivity that concentrates heat at the tool edge, a reactive surface that promotes tool wear at elevated cutting temperature, and a tendency to work-harden under a rubbing or dull edge. Where it differs from a heavily beta-stabilized alloy is in the relatively small amount of beta phase present, which tends to make near-alpha grades like this one somewhat more forgiving to cut than the higher-vanadium alpha-beta grades in the same family.

Its very low density also works in the machinist's favor to some degree, since removal rates and cutting forces for a given depth of cut tend to run a bit lighter than on denser titanium alloys. That said, the high aluminum content still promotes chemical reactivity with tool materials at cutting temperature, so the same fundamentals apply: moderate speeds, firm and consistent feeds to stay under any hardened surface layer, rigid setups, and generous coolant flow directed right at the cutting zone.

Overall, this alloy tends to machine somewhat more predictably than the higher-strength alpha-beta titanium grades, though it still demands the discipline any titanium alloy requires — sharp tooling, adequate feed, and no dwelling in the cut.

Recommended Cutting Speeds

Operation Vc (m/min) Vc (SFM)
Turning 65 – 85 215 – 280
Milling 45 – 65 150 – 215
Parting 40 – 55 130 – 180
Grooving 55 – 75 180 – 245
Drilling 55 – 75 180 – 245

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.

Recommended FM Carbide Grades by Operation

Turning

Grade Coating ISO Application Range
FM524 CVD S05 – S10
FM2533 CVD S15

Parting Off

Grade Coating ISO Application Range
FM2543 CVD S20
FM2553 CVD S30

Grooving

Grade Coating ISO Application Range
FM2533 CVD S10

Milling (Indexable)

Grade Coating ISO Application Range
FM125 PVD S15 – S35

Ready to cut Ti-8Al-1Mo-1V? Shop FM Carbide inserts matched to this alloy's turning, parting, grooving, and milling requirements.

Shop Turning & Grooving Inserts Shop Milling Inserts

Recommended Insert Cutting-Edge Geometry

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