MG · magnesium

Magnesium Alloy AZ61A (wrought)

A wrought magnesium alloy sitting between AZ31 and AZ80: more strength than AZ31, easier to extrude and form than AZ80, and it machines cleanly.

60 HB260–300 MPa1.80 g/cm³Machinability 8/10

Quoting this material

Typical lead time
15–25 working days
Condition
Extruded
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.

8/10

A wrought magnesium alloy sitting between AZ31 and AZ80: more strength than AZ31, easier to extrude and form than AZ80, and it machines cleanly.

Properties as supplied

ParameterValueUnit
Tensile strength260–300MPa
Yield strength (0.2%)180–200MPa
Elongation12%
Hardness60HB
Thermal conductivity78W/m·K
Modulus of elasticity45GPa

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

Extruded

Heat treatment

Not precipitation hardenable to the extent of a T5 grade; it is a solid-solution strengthened wrought alloy. Annealing is a stress relief after forming.

Achievable surface finish

Typical

Ra 1.6 µm

Best achievable

Ra 0.4 µm

Long runs of extrusions are supplied to a controlled finish; machined ends and fittings finish well.

Tooling and cutting parameters

Cutting speed

  • 300–600 m/min (sharp uncoated carbide)

Feed

  • 0.10–0.35 mm/rev turning · 0.10–0.30 mm/tooth milling

Tooling

  • Sharp uncoated carbide with large clearance

Coolant

  • Mineral-oil mist or dry

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

  • Extruded structural profiles
  • Aerospace brackets and clips
  • Portable equipment frames
  • Sports equipment hardware
  • Electronic device frames

DFM notes for this grade

  • Extrudability is the reason to choose it: AZ61 pushes into a profile that AZ80 cannot, which lets the design use a near-net extrusion and machine only the features
  • Corrosion protection is still mandatory; a machined extrusion end is exactly where a coating system has to be applied and maintained
  • Stiffness is 45 GPa, so a profile has to be deeper than an aluminium equivalent for the same deflection - the extrusion section design carries the load

Questions buyers ask

When is AZ61A chosen over AZ31B?
When the extrusion or the part needs more strength than AZ31 gives but the profile still has to be extruded. AZ61 is the middle grade: more strength than AZ31, more formability than AZ80, and that combination is why it shows up in structural profiles.
Why is the extrusion route important for magnesium?
Because near-net extrusions avoid machining, and magnesium chips are the part of the process that demands the most care. The less swarf a design produces, the simpler and safer the job - that is a real design consideration for the material.

Grades we would quote instead

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