Material W-545

Technical Reference Library

W-545

Type Fe-Ni-Cr Superalloy Nickel ~26% Chromium ~13.3%

Material Overview

W-545 is an iron-base, nickel-chromium precipitation-hardening superalloy cross-referenced to AISI 665 and UNS S66545. It belongs to the same general Fe-Ni-Cr-Mo-Ti family as A-286 and Discaloy, but carries a distinctly higher nickel content (~26%) than a typical PH stainless, which pushes it further toward true superalloy territory in terms of elevated-temperature strength retention while still remaining an economical, iron-base alternative to a full nickel-base grade.

Alloys in this family are widely used for gas-turbine hot-section hardware in aviation, naval, and industrial power-generation service: turbine blades, guide vanes, discs, high-pressure compressor discs, and combustor components that need to hold strength and creep resistance at elevated temperature without the cost and machining difficulty of a full nickel-base superalloy. Like other members of this family, W-545 is precipitation-hardened via titanium and aluminum additions after an initial solution anneal.

International Designation Equivalents

Standard Designation
AISI 665
UNS S66545

Chemical Composition

Element Amount
Iron (Fe) Balance (~53%)
Nickel (Ni) 26%
Chromium (Cr) 13.3%
Molybdenum (Mo) 1.8%
Manganese (Mn) 1.5%
Silicon (Si) 0.8%
Aluminum (Al) 0.15%
Carbon (C) 0.08%

All values fall within the published AISI 665 / UNS S66545 composition ranges. Minor/trace elements not published in the source record are omitted rather than estimated.

Machinability Explained

W-545 machines as a step up in difficulty from a standard PH stainless like 17-4PH, reflecting its higher nickel content and superalloy-oriented chemistry. Its combined chromium and molybdenum content resist abrasive wear well in service, but that same resistance translates into faster flank wear on the cutting tool, and the alloy's reduced thermal conductivity compared with plain alloy steel concentrates heat at the tool-chip interface rather than carrying it away in the chip.

The alloy work-hardens readily under light or interrupted cuts, so maintaining a steady, adequate chip load is important to avoid raising a hardened skin that is tougher to remove on the next pass. Because it retains a meaningful share of its strength at elevated temperature - more so than a conventional PH stainless - tool edges stay under real mechanical load even as cutting temperatures climb, favoring sharp, positive-rake geometries, rigid workholding, and generous coolant delivery. Coated carbide grades developed for superalloys and high-temperature stainless steels are the standard choice for this alloy family, and machining in the solution-annealed condition before final aging is recommended wherever the process allows it.

Recommended Cutting Speeds

Application Vc (m/min) Vc (SFM)
Turning 135-185 440-610
Milling 100-140 330-460
Parting 85-115 280-380
Grooving 120-160 390-520
Drilling 120-160 390-520

General starting-point ranges for iron-base PH superalloys of this type in the solution-annealed condition. Actual optimal speeds depend on tool grade, coating, rigidity, and coolant strategy.

Recommended FM Carbide Grades by Operation

Turning

Grade Coating ISO Application Range
FM524 CVD S05 - S10
FM2533 CVD S15

Parting / Grooving

Grade Operation Coating ISO Application Range
FM2543 Parting CVD S20
FM2553 Parting CVD S30
FM2533 Grooving CVD S15

Milling

Grade Coating ISO Application Range
FM125 PVD S15 - S35

Ready to cut W-545? Shop FM Carbide inserts engineered for iron-base heat-resistant superalloys.

Shop Turning & Grooving Inserts Shop Milling Inserts

Recommended Insert Cutting-Edge Geometry

Honing Size 0.02-0.05 mm / 0.001-0.002"
Rake Angle 12° - 16°
Land Angle Neutral
Land Width 0.10-0.20 mm / 0.004-0.008"
Ground Insert Recommended