Alloy Information Report for Inconel™ 713C

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General Characteristics of Inconel™ 713C

Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). It’s a nickel-chromium alloy that’s ideally suited for jet engine gas turbine blades.

Chemical Composition of Inconel™ 713C

• Carbon 0.20
• Manganese 1.0 max
• Sulfur 0.015 max
• Silicon 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 remainder

Applications of Inconel™ 713C

• Jet engine gas turbine blades

Machinability of Inconel™ 713C

• Machine with single–point cemented tungsten-cobalt grade and tungsten-tantalum-cobalt grade tools or
• High-speed tungsten-cobalt or molybdenum-tungsten-vanadium tools
• Cutting lubricants:
  • Chlorinated, sulfurized  fatty mineral oil
  • Rich emulsion of 10 parts water and 1 part soluble oil
• Surface and cylindrical grind with wheels:
  • Aluminum oxide
  • Vitrified bond of medium or soft hardness and medium open structure
  • Use 1 pound of sal soda with 25 gallons of water, or chemically active grinding coolant

Weldabiltiy of Inconel™ 713C

• Applications using very low restraint
• Use Inco-Weld A electrode
• Flash-butt weld
• Good for hydrogen-atmosphere brazing with normal high-heat brazing alloy with electroplated mating surfaces

To Send a Request for Quote for Inconel™ 713C, please Click Here, or call 1.973.276.5000 or fax 1.973.276.5050.