Pyromet® 41

UNS #N07041

Pyromet® 41 is a precipitation hardening, nickel-base, high-temperature alloy possessing very high strength in the 1200-1800°F (649-982°C) temperature range. This alloy is designed for use in severely stressed high temperature applications with good oxidation resistance. This alloy an excellent candidate for critical aircraft engine components.

Type Analysis

  • Carbon (Maximum) 0.06-0.12
  • Silicon (Maximum) 0.2
  • Nickel (Nominal) Balance
  • Titanium (Nominal) 3.00-3.30
  • Manganese (Maximum) 0.1
  • Chromium (Nominal) 18.00- 20.00
  • Cobalt (Nominal) 10.00-12.00
  • Molybdenum (Nominal) 9.00 - 10.50
  • Iron (Nominal) 5
  • Aluminum (Nominal) 1.40 -1.60
  • Boron (Nominal) 0.003- 0.010

Applications

Jet engine and high speed airframe components including afterburner parts, Turbine casings, Wheels, Buckets, Bolts, Fasteners,

Applicable Specifications

  • AMS 5712
  • AMS 5800 (Weld Rod - Chem Only)
  • AMS 5713

Billet

Rounds

Wire

Technical Information

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