AMS5391/ Inconel 713C high temperature alloy

• Inconel 713C is a precipitation hardenable, nickel-chrominium base cast alloy, which possesses excellent strength properties up to 1800°F. The alloy has good castability, remarkable resistance to oxidation and thermal fatigue and outstanding structural stability
• Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades
• Chemical composition:
  • Carbon: 0.20
  • Manganese: 1.0 max
  • Sulfur: 0.015 max
  • Silicone: 1.0 max
  • Chromium: 11.0-14.0
  • Molybdenum: 3.5-5.5
  • Titanium: 0.25-1.25
  • Aluminum: 5.5-6.5
  • Iron: 5.0 max
  • Columbium: + Ta 1.0-3.0
  • Nickel balance
• Applications: most commonly used for jet engine gas turbine blades