OrangeSea
CNC & Precision Engineering
Inconel 718
HomeMaterialsInconel 718
Nickel Superalloy

Inconel 718

The toughest material we machine — proven process, predictable results.

Tensile Strength
1275 MPa
Density
8.19 g/cm³
Max Temp
700°C continuous
Machinability

Inconel 718 is a nickel-chromium superalloy developed for gas turbine components that must maintain full strength at temperatures that would cause other alloys to creep and fail. It is arguably the most difficult material to machine in common engineering use — it work-hardens on contact, generates extreme cutting heat (low thermal conductivity, 11.4 W/m·K), and wears carbide tooling at a rate 5–10× faster than stainless steel. Every 'CNC machine shop' can cut Inconel. Very few can cut it repeatedly to tight tolerances without excessive scrap, tool breakage, and unpredictable cycle times. OrangeSea CNC machines Inconel 718 and 625 to aerospace and energy standards daily — with documented feeds, speeds, tooling brands, and coolant pressures that deliver first-time quality.

Technical Data

Material Properties

Tensile Strength (aged)
1275–1430 MPa
Yield Strength (aged)
1034–1100 MPa
Elongation
12%
Hardness (aged)
363 HB
Density
8.19 g/cm³
Thermal Conductivity
11.4 W/m·K (very low)
Machinability
Extremely difficult (1/5)
High Temp Capability
Full strength to 700°C
Oxidation Resistance
Excellent to 980°C
Creep Resistance
Excellent — turbine standard

Capabilities

Why CNC Machine IN-718?

01

Proven Daily Process

We machine Inconel every working day. Our CAM engineers have optimised toolpaths, tooling selection (ceramic and CBN inserts), cutting data, and coolant strategy for IN718 and IN625.

02

Extreme Temperature Parts

No other common alloy retains strength and resists creep at temperatures up to 700°C — essential for gas turbine, jet engine, and downhole oil tool applications.

03

Oxidation Proof

Inconel 718 forms a stable, adherent oxide layer that resists further oxidation up to 980°C — components function without coating in high-temperature oxidising environments.

04

Material Traceability

All Inconel supplied with full Mill Test Reports, heat lot certs, and chemical composition reports. AMS 5662/5664 spec sourcing available for aerospace orders.

05

Third-Party Inspection

We welcome customer TPI and DNV/BV/SGS inspection witnesses for critical Inconel orders. Our facility and documentation meet aerospace and energy audit expectations.

Use Cases

What We Machine in IN-718

Aerospace
Turbine disc slots, combustion liner components, exhaust nozzle hardware, thrust reverser parts
Energy & Oil
Downhole tool bodies, wellhead components, subsea valve internals, compressor seal rings
Power Generation
Gas turbine components, steam turbine hardware, heat exchanger tubing fixtures
Nuclear
Reactor internals, control rod components, pressure vessel hardware

Engineering Tips

Design for Machining — IN-718

Machine in the annealed (solution-treated) condition where possible — aged Inconel is significantly harder and faster to work-harden

Ceramic cutting inserts (SiC or Si3N4) are preferred for roughing at high speeds — carbide for finishing passes. Never use HSS

Use high-pressure coolant (70+ bar) directed precisely at the cutting edge — heat is the primary cause of tool failure in Inconel machining

Never dwell in the cut — a stopped cutter in contact with Inconel causes immediate work-hardening and probable tool failure on restart

Budget for 5–10× tooling consumption compared to stainless 316L. Per-piece price reflects this — cheaper quotes usually reflect inadequate tooling strategy

Surface Options

Available Finishes

As-machined
Bead blast
Electropolish
Electroless nickel (rare)
Thermal spray coating (customer-applied)

Get Started

Ready to Machine in IN-718?

Upload your design files and get a detailed quote within 24 hours. Tolerances to ±0.01 mm, ships worldwide from Shenzhen.