TI · titanium

Titanium Ti-6Al-4V (Grade 5)

The alloy the whole titanium reputation comes from. Published index around 20–25% against B1112 = 100%; low thermal conductivity puts the heat in the tool edge, and it work-hardens the moment the cutter rubs.

349 HB (~36 HRC)950 MPa4.43 g/cm³Machinability 3/10

Quoting this material

Typical lead time
12–20 working days
Condition
Annealed (mill annealed); also supplied in STA where higher strength is required
Achievable finish
Ra 1.6 µm typical · Ra 0.4 µm best
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Machined in-house to your drawing: see the precision CNC machining service and the machine and inspection capability it runs on.

Machinability

Our own 1–10 shop ranking, not a published index: 10 is free-cutting brass C360, 1 is Inconel 718. It ranks how a material behaves on the floor - cycle time, chip control and tool life together. Where a published index exists it is quoted in the note.

3/10

The alloy the whole titanium reputation comes from. Published index around 20–25% against B1112 = 100%; low thermal conductivity puts the heat in the tool edge, and it work-hardens the moment the cutter rubs.

Properties as supplied

ParameterValueUnit
Tensile strength950MPa
Yield strength (0.2%)880MPa
Elongation14%
Hardness349HB
Thermal conductivity6.7W/m·K
Modulus of elasticity113.8GPa

Hardness, tensile and thermal figures are typical published values for the condition stated. Actual mill certificates govern; send the specification with the drawing and we confirm against the certificate before the material is cut.

Condition

Annealed (mill annealed); also supplied in STA where higher strength is required

Heat treatment

Solution treatment and ageing (STA) raises the strength above the annealed condition, and it is done by the mill or a specialist heat treater, not in a machine shop. Annealing after welding relieves stress without changing the phase structure.

Achievable surface finish

Typical

Ra 1.6 µm

Best achievable

Ra 0.4 µm

Surface finish is functional on fatigue parts: a machined scratch in titanium is a crack initiator, and shot peening is often specified to put the surface into compression.

Tooling and cutting parameters

Cutting speed

  • 40–80 m/min (carbide)

Feed

  • 0.08–0.20 mm/rev turning · 0.05–0.12 mm/tooth milling

Tooling

  • Uncoated fine-grain carbide, sharp positive rake, generous corner radius; no honed edges

Coolant

  • High-pressure flood, aimed at the edge; through-tool wherever possible

Starting points for carbide on a rigid setup, not a guarantee. The right numbers depend on the machine, the toolholder and the fixturing - ask and we will say what we would actually run.

Typical applications

  • Aircraft structural fittings and brackets
  • Medical implants (with ELI grades)
  • Aerospace engine mount components
  • Motorsport and high-performance fasteners
  • Subsea and offshore hardware

DFM notes for this grade

  • Keep the tool engaged: a dwell or a spring pass work-hardens the surface and the next cut has to get under a skin that is now much harder
  • Rigidity is everything - titanium deflects the tool and the part, and chatter in a thin rib will crack the part or the tool before it scrapes the finish
  • Sharp corners and rough finishes are fatigue initiators in a part that is usually specified for fatigue: radii and finish are design requirements here, not shop choices

Questions buyers ask

Why does titanium need such low cutting speeds?
Because titanium conducts heat away from the cut at roughly a third of steel and a sixteenth of aluminium. All the heat stays in the cutting zone, so the edge reaches softening temperature at a cutting speed where steel would be comfortable. Higher speed does not cut faster - it destroys the tool.
Can Ti-6Al-4V be heat treated to a higher strength?
Yes, by solution treatment and ageing, which takes it to roughly 1,100 MPa. It is a mill or specialist operation with a controlled cycle, and it changes the machining behaviour - the STA condition is harder and more notch sensitive than the annealed material we normally cut.

Grades we would quote instead

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