NI · superalloy

Nickel Superalloy Inconel 738 (cast, vacuum melted)

A cast nickel superalloy for turbine blades, supplied as a casting rather than bar. The cast skin is abrasive and hard, and the alloy work-hardens like 718.

~380 HB (cast and aged)~1,000 MPa (cast, at room temperature)8.11 g/cm³Machinability 1/10

Quoting this material

Typical lead time
25–40 working days
Condition
Investment cast, then solution treated and aged
Achievable finish
Ra 3.2 µm (as cast) typical · Ra 0.8 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.

1/10

A cast nickel superalloy for turbine blades, supplied as a casting rather than bar. The cast skin is abrasive and hard, and the alloy work-hardens like 718.

Properties as supplied

ParameterValueUnit
Tensile strength (cast)~1,000MPa
Creep resistanceTo 980°C
Hardness (cast, aged)~380HB
Casting formInvestment, vacuum melted-
Thermal conductivity11.1W/m·K
WeldabilityPoor (repair only, controlled)-

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

Investment cast, then solution treated and aged

Heat treatment

Solution treat and age after casting. The whole point of the alloy is creep and oxidation resistance at 850–980 °C in a cast form, which a wrought alloy cannot match at that temperature.

Achievable surface finish

Typical

Ra 3.2 µm (as cast)

Best achievable

Ra 0.8 µm

Cast surfaces are usually machined only where a fit or a seal is needed; the rest of the blade stays as cast.

Tooling and cutting parameters

Cutting speed

  • 15–35 m/min (carbide)

Feed

  • 0.05–0.12 mm/rev turning · 0.04–0.08 mm/tooth milling

Tooling

  • Fine-grain carbide, tough substrate; remove the cast skin with a ceramic or a dedicated roughing grade

Coolant

  • High-pressure flood, and the casting skin will consume the first tool

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

  • Turbine blades and vanes
  • Industrial gas turbine hot section
  • Aerospace engine hot components
  • Power generation turbine parts
  • High-temperature cast structural parts

DFM notes for this grade

  • Machining a casting means starting from a shape you did not design: the stock allowance varies, so the first operation is to establish a datum from the casting, not to a nominal size
  • The as-cast skin is abrasive and often decades-hardened at the surface; expect the first tool to be consumed removing it
  • Repair welding is limited and controlled - a casting with a defect is usually replaced rather than repaired in a job shop

Questions buyers ask

Why is a turbine blade cast rather than machined from bar?
Because the properties needed at 900 °C cannot be produced in a wrought bar, and the internal cooling passages of a modern blade cannot be machined. Casting gives the shape and the creep resistance; machining only produces the root and tip fits.
What does a shop actually machine on a turbine blade?
The root fixing - the fir-tree or dovetail that locates the blade in the disc - and the tip. Those are the tolerance-critical features; the aerofoil and the cooling holes are produced by the casting and the subsequent processes.

Grades we would quote instead

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