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AL-6XN and 254 SMO: Super Austenitic Stainless Machining

AL-6XN and 254 SMO: Super Austenitic Stainless Steel Machining Guide

AL-6XN (UNS N08367) and 254 SMO (UNS S31254) belong to the super austenitic stainless steel family, offering 6% molybdenum content and pitting resistance equivalent numbers (PREN) above 40. These alloys serve in seawater piping, chemical process equipment, flue gas desulfurization systems, and pharmaceutical processing where standard 316L is inadequate. Their high alloy content makes them 40-60% more difficult to machine than conventional austenitic grades, demanding specific insert selections and disciplined parameter management.

Material Comparison

AL-6XN (UNS N08367):

  • Composition: 21% Cr, 24% Ni, 6.3% Mo, 0.22% N, 0.5% Mn
  • Hardness: 170-210 HB (annealed)
  • UTS: 690-830 MPa, elongation 45-55%
  • PREN: 43-48

254 SMO (UNS S31254):

  • Composition: 20% Cr, 18% Ni, 6.3% Mo, 0.22% N, 1.5% Mn, 0.7% Cu
  • Hardness: 180-220 HB (annealed)
  • UTS: 690-860 MPa, elongation 40-50%
  • PREN: 42-46

The key difference for machinability is 254 SMO’s higher manganese (1.5% vs 0.5%) and copper (0.7%) content, which slightly increases work-hardening rate and built-up edge tendency. In practice, AL-6XN machines approximately 10-15% more easily than 254 SMO, but both require the same fundamental tooling approach.

Machinability Factors

  1. High molybdenum content: The 6% Mo forms hard intermetallic phases (sigma, chi, Laves) at grain boundaries during welding or improper heat treatment. In properly annealed material, Mo remains in solid solution but increases cutting forces by 15-20% compared to 316L.
  2. Nitrogen strengthening: The 0.22% N significantly increases yield strength (380-450 MPa vs 240 MPa for 316L), requiring higher cutting forces and generating more heat.
  3. Work hardening: Both alloys work-harden more aggressively than 304 or 316. Surface hardness increases of 80-120 HB per pass are common. Never take light finishing cuts below 0.3mm depth.
  4. Chip toughness: Chips are extremely ductile and resistant to breaking. Chip management requires dedicated chipbreaker geometries and higher feed rates.

Insert Grade Recommendations

Roughing – Both Alloys:

  • Sandvik GC235 (CVD TiCN/Al2O3, stainless-optimized substrate). CNMG 120412 with -MM or -MR chipbreaker. The CVD coating provides crater wear resistance against the abrasive, high-alloy chips.
  • Kennametal KC5025 (PVD TiAlN) or KC5525 for interrupted cuts. CNMG 120412.
  • Seco TP2501 (CVD Duratomic coating) for high-speed roughing where productivity is prioritized over edge life.

Finishing – Both Alloys:

  • Sandvik GC215 (PVD micro-grain carbide). DNMG 150404 with polished rake and 0.01mm edge hone for mirror finish on sealing surfaces.
  • Mitsubishi VP15TF (PVD Miracle coating). Excellent surface finish on austenitic stainless.
  • Tungaloy NS9530 (nano-TiAlN PVD) for finishing below Ra 0.4 micrometers.

Grooving and Parting:

  • Sandvik GC1125 or N123 grade with -RM chipbreaker for N-style grooving blades (3-4mm width).
  • Kennametal KC5010 for parting blades up to 65mm bar diameter.

Cutting Parameters

Turning – AL-6XN:

  • Vc: 90-160 m/min (CVD roughing), 130-220 m/min (PVD finishing)
  • fn: 0.20-0.35 mm/rev roughing, 0.08-0.18 mm/rev finishing
  • ap: 2.0-5.0 mm roughing, 0.3-1.0 mm finishing
  • Coolant: Flood emulsion at 8-10%, 50-70 bar
  • Tool life: 35-70 minutes per edge at 120 m/min

Turning – 254 SMO:

  • Vc: 80-140 m/min (CVD roughing), 120-200 m/min (PVD finishing)
  • fn: 0.18-0.30 mm/rev roughing, 0.08-0.16 mm/rev finishing
  • ap: 2.0-4.5 mm roughing, 0.3-0.8 mm finishing
  • Tool life: 25-55 minutes per edge at 100 m/min

Minimum depth of cut: 0.3mm for both alloys. Cutting within the work-hardened layer causes accelerated flank wear and surface tearing.

Milling Guidelines

Face and Profile Milling:

  • 4-5 flute solid carbide end mills, AlTiN or AlCrN coating, 12-25mm diameter
  • Vc: 70-130 m/min
  • fz: 0.05-0.10 mm/tooth
  • Radial engagement: 50-70% of diameter (peripheral), 5-8% (trochoidal slotting)
  • Axial depth: 0.8-1.5 x diameter
  • Always use climb milling direction

Indexable face milling:

  • Round insert cutters (RCMT 1204) with Sandvik GC225 or Seco TP2501 grades
  • Vc: 100-160 m/min, fz: 0.15-0.25 mm/tooth
  • Positive rake cutter bodies reduce cutting forces by 20-30% on these high-strength alloys

Drilling

  • Solid carbide, 135 deg split point, TiAlN coating, through-tool coolant
  • Vc: 50-90 m/min, fn: 0.06-0.12 mm/rev (8-12mm drills)
  • Peck depth: 2.0-3.0 x diameter, full retract for chip evacuation
  • Coolant pressure: 40-70 bar through tool
  • Expected life: 100-300 holes per drill (10mm x 30mm deep in annealed condition)

Welding and Post-Weld Machining

AL-6XN and 254 SMO are frequently fabricated by welding followed by machining of weld preparations and post-weld surfaces. Critical notes:

  • Intermetallic phases (sigma, chi) can precipitate in the heat-affected zone if cooling rates are too slow. These phases are extremely hard (500+ HB) and destroy cutting tools. Verify proper solution annealing (1150-1200 deg C, water quench) after welding before machining.
  • Machine weld prep bevels before welding whenever possible. Post-weld machining of the HAZ requires reduced speeds (Vc 40-60 m/min) and acceptance of shorter tool life.
  • Use overalloyed filler metals (ERNiCrMo-3 or ERNiCrMo-4) for weld joints that will be machined. The nickel-based weld metal machines more easily than the stainless HAZ.

Flange and Fitting Production

Super austenitic flanges and fittings require multi-operation turning, boring, facing, and grooving. Process recommendations:

  1. Use a single setup on a vertical turret lathe or horizontal turning center with live tooling to minimize re-clamping.
  2. Program roughing operations in sequence from largest to smallest diameter to maintain workpiece rigidity.
  3. Ring-type joint (RTJ) grooves require precise dimensional control. Use dedicated grooving inserts with 0.05mm nose radius and PVD coating for Ra below 1.6 micrometers on groove surfaces.
  4. Bolt holes should be drilled after all turning is complete to avoid interrupted cutting on the OD passes.
  5. Budget 2-3x the machining time of equivalent 316L components for quoting purposes.

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