CS · carbon steel

Carbon Steel 4340 (40NiCrMo)

Tougher and harder than 4140 at the same strength, and it machines accordingly - expect lower speeds, shorter tool life and a real grinding allowance after heat treatment.

217–255 HB annealed · 36–40 HRC quenched and tempered1,100–1,200 MPa (Q&T)7.85 g/cm³Machinability 5/10

Quoting this material

Typical lead time
12–18 working days
Condition
Annealed, or quenched and tempered to the specified hardness
Achievable finish
Ra 1.6 µm annealed 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.

5/10

Tougher and harder than 4140 at the same strength, and it machines accordingly - expect lower speeds, shorter tool life and a real grinding allowance after heat treatment.

Properties as supplied

ParameterValueUnit
Tensile strength (Q&T)1,150MPa
Yield strength (Q&T)1,000MPa
Elongation (Q&T)12%
Hardness (annealed)230HB
Thermal conductivity38W/m·K
Modulus of elasticity205GPa

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, or quenched and tempered to the specified hardness

Heat treatment

Deep-hardening nickel-chromium-molybdenum steel. Oil quench from 830–860 °C, temper to the required strength and toughness. The nickel gives it the notch toughness that 4140 lacks at high strength - that is why it is used for the parts where a crack means a failure, not a repair.

Achievable surface finish

Typical

Ra 1.6 µm annealed

Best achievable

Ra 0.4 µm

At the delivered hardness the finishing pass is a grind; plan for it and put the allowance on the drawing.

Tooling and cutting parameters

Cutting speed

  • 100–180 m/min annealed (carbide) · 60–90 m/min at 38 HRC

Feed

  • 0.12–0.25 mm/rev turning · 0.06–0.15 mm/tooth milling

Tooling

  • Tough coated carbide; CBN for hard turning

Coolant

  • High-pressure flood

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 landing gear and structural fittings
  • High-load shafts and axles
  • Heavy-duty gear and pinion blanks
  • Pressure vessel and tooling components
  • Marine propeller shafting

DFM notes for this grade

  • The notch toughness that justifies the price is destroyed by a sharp corner or a poor surface finish - radii and finish are functional on this material
  • Nitriding or hard chrome after heat treatment is common; both need the pre-treatment geometry to allow for the case
  • Cost is roughly 1.5–2× 4140 plus a longer cycle - specify it because the load demands it, not as a safety margin

Questions buyers ask

When is 4340 worth the premium over 4140?
When the part is fatigue- or impact-critical at high strength. 4340 keeps its toughness at 1,100 MPa where 4140 becomes notch sensitive - for a landing-gear component, a high-load axle or a part where a crack is unacceptable, that difference is the whole justification.
Can 4340 be welded?
Technically with a controlled procedure: preheat, an appropriate filler, and post-weld heat treatment. In practice it is avoided on the parts that need 4340 in the first place. Welding a 4340 part usually means the joint should have been a forging or a bolted connection.

Grades we would quote instead

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