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Inconel & Superalloy Speeds & Feeds Calculator 2026

Expert parameters for Inconel 718, Hastelloy, Waspaloy, and nickel-based superalloys. Includes work hardening and ceramic tool analysis.

11 AlloysWork HardeningCeramic ToolsHP Coolant

Calculate Superalloy Parameters

⚠️ SUPERALLOY MACHINING - CRITICAL

  • NEVER let the tool dwell or rub - maintain positive feed at all times
  • • Work hardening occurs rapidly with incorrect parameters
  • • High-pressure coolant (1000+ psi) is strongly recommended
  • • Monitor tools closely - sudden failure is common

1Superalloy Selection

Inconel 718

Machinability: 12%
Composition
52.5% Ni, 19% Cr, 18.5% Fe, 5.1% Nb, 3% Mo
Tensile Strength
1240-1400 MPa
Thermal Cond.
11.4 W/m·K
Hardness (Aged)
HRC 36-44

Applications: Turbine disks, rocket engines, oil & gas

2Operation & Tooling

3Cutting Parameters

Keep DOC above work-hardened layer

🔴 Superalloy Tip: Work hardening is your #1 enemy. Never take light cuts or let the tool dwell. The surface layer hardens rapidly and will destroy subsequent passes. Always maintain positive feed and use depth of cut greater than any previously hardened layer.

Superalloy Machining Guide

Nickel-based superalloys are among the most challenging materials to machine. They maintain high strength at extreme temperatures, work-harden rapidly, and have very low thermal conductivity - all factors that destroy cutting tools quickly.

⚠️ Critical: Work Hardening

Superalloys work-harden rapidly when the tool rubs rather than cuts. This creates a hardened surface layer that damages subsequent cutting passes. Never let the tool dwell, rub, or take light cuts. Always maintain positive feed and use depths greater than any previously hardened layer.

Alloy Families

🔵 Inconel (Ni-Cr-Fe)

Most Common: Inconel 718, 625, 600

General-purpose superalloys with good corrosion and temperature resistance. Inconel 718 is the most frequently machined superalloy.

  • • 718: Turbine disks, rockets - HRC 36-44 aged
  • • 625: Marine, chemical - easier to machine
  • • 600: Heat exchangers, nuclear

🟢 Hastelloy (Ni-Mo-Cr)

Optimized for: Corrosion Resistance

Excellent resistance to aggressive chemicals. Slightly easier to machine than Inconel 718 but still challenging.

  • • C-276: Chemical processing, pollution control
  • • X: Combustion chambers, afterburners

🟣 Waspaloy (Ni-Co-Cr)

Very high strength: Turbine components

Extremely high strength for jet engine disks. Difficult to machine - expect short tool life.

🔴 René (Ni-Co-Mo)

Most Difficult: Single crystal turbine blades

Highest temperature capability. René 80 is used for single-crystal castings. Very low machinability ratings (6-10%).

Speed Reference (Carbide + TiAlN)

AlloyMilling (m/min)Turning (m/min)Machinability
Inconel 60022-5030-6522%
Inconel 62518-4025-5518%
Inconel 71815-3220-4512%
Waspaloy12-2616-3610%
René 4110-2214-328%
René 808-1810-266%

Tool Selection

Carbide (TiAlN, AlCrN)

  • • Most versatile - handles interrupts
  • • Lower speeds but more forgiving
  • • AlCrN coating best for heat resistance
  • • Use for general work

Ceramic (SiAlON, Whisker)

  • • 2-3× higher speeds possible
  • • Requires very rigid setup
  • • NO interrupted cuts - will chip
  • • Use for big-volume roughing

Critical Best Practices

✓ Essential

  • • High-pressure coolant (1000+ psi)
  • • Never let tool dwell or rub
  • • Maintain positive feed always
  • • DOC greater than hardened layer
  • • Sharp, positive-rake geometry
  • • Shortest possible overhang

✗ Avoid

  • • Light cuts (work hardening)
  • • Dry cutting
  • • Interrupted cuts with ceramics
  • • Dull or worn tools
  • • Stopping mid-cut
  • • Ignoring tool wear

Frequently Asked Questions

Inconel and nickel superalloys are challenging due to: 1) Extreme work hardening - the surface hardens rapidly when cut incorrectly, 2) Low thermal conductivity - heat concentrates at the cutting edge, 3) High strength maintained at elevated temperatures, 4) Strong abrasive carbides in the microstructure. These factors destroy tools quickly.

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