Material Ti-7Al-4Mo

Technical Reference Library

Ti-7Al-4Mo Titanium Alloy

UNS R56740 AMS 4970 Alloy Type Alpha-Beta

Material Overview

Ti-7Al-4Mo is one of the earlier high-strength alpha-beta titanium alloys developed for aerospace service, predating the industry's later shift toward Ti-6Al-4V as the default workhorse grade. Its 7% aluminum content is higher than what's used in Ti-6Al-4V, giving stronger alpha-phase stabilization, while a 4% molybdenum addition provides the beta-stabilizing balance. The result is an alloy that can be solution treated and aged to reach higher strength levels than the standard Grade 5 material, along with good creep resistance at moderately elevated temperatures.

Because of that strength and creep performance, Ti-7Al-4Mo built its reputation in rotating and structural jet engine hardware — compressor disks, blades, and spacers, along with other high-load aerospace structural components — where its ability to be heat treated to higher strength levels than Grade 5 made it attractive before newer alloys took over many of those roles. It remains in service and in specification today, even though it's seen less often in new designs than more modern titanium grades.

International Designation Equivalents

Standard Designation
UNS R56740
AMS 4970 (bar, wire, forgings — solution treated and aged)

Additional cross-references could not be independently confirmed and have been omitted rather than guessed.

Chemical Composition

Element Content
Aluminum (Al) ~7%
Molybdenum (Mo) ~4%
Iron (Fe) 0.30% max
Oxygen (O) 0.20% max
Carbon (C) 0.10% max
Nitrogen (N) 0.050% max
Hydrogen (H) 0.013% max
Titanium (Ti) Balance (~89%)

Machinability Explained

Ti-7Al-4Mo is a genuinely demanding alloy to cut, and its higher aluminum content compared to Ti-6Al-4V only adds to the challenge. The same fundamentals apply as with any titanium grade: thermal conductivity too low to carry heat away from the cutting edge efficiently, a reactive surface chemistry that promotes diffusion wear against carbide tooling at elevated temperature, and a strong tendency to work-harden if the cutting action isn't clean and consistent.

Because this alloy is frequently used in the heat-treated, higher-strength condition to take advantage of its elevated mechanical properties, it also tends to run harder and generate more cutting force than as-annealed titanium at a comparable speed. That calls for slower cutting speeds, higher and steadier feed rates to avoid rubbing, and heavy, well-directed coolant flow to manage both temperature and chip evacuation.

Rigid setups, sharp and properly honed cutting edges, and conservative depths of cut all matter here. Expect tool life on Ti-7Al-4Mo to run shorter than on Ti-6Al-4V, and plan speeds and feeds accordingly rather than defaulting to Grade-5 parameters.

Recommended Cutting Speeds

Operation Vc (m/min) Vc (SFM)
Turning 55 – 75 180 – 245
Milling 40 – 55 130 – 180
Parting 35 – 45 115 – 150
Grooving 45 – 65 150 – 215
Drilling 45 – 60 150 – 200

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-7Al-4Mo? Shop FM Carbide inserts matched to this alloy's turning, parting, grooving, and milling requirements.

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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