Inconel 713C Nickel Alloy Plate 7.913 G/Cm³ Density 2b / Ba Surface Treatment
Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades.Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C).
Inconel 713C sheet Chemical Compositons:
| Alloy | % | Ni | Cr | Fe | Mn | Si | Mo | Zr | Ti | Cu | Co | Al | C | S |
| 713C | Min. | Bal | 12.0 | - | - | - | 3.8 | 0.05 | 0.5 | - | 1.8 | 5.5 | - | - |
| Max. | 14.0 | 2.5 | 0.25 | 0.5 | 5.2 | 0.15 | 1.0 | 0.5 | 2.8 | 6.5 | 0.20 | 0.015 |
Inconl 713CSheet Physical properties
| Density | 7.913 g/cm³ |
| Melting point | 1260℃-1288℃ |
Inconel 713C Products Mechinabity Physical
● High-speed tungsten-cobalt or molybdenum-tungsten-vanadium toolsCutting lubricants:
Chlorinated, sulfurized fatty mineral oil
Rich emulsion of 10 parts water and 1 part soluble oil
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
Inconel 713C Weledablity
- Inconel 713C can be used in applications using very low restraint
- Use Inco-Weld A electrode
- Flash-butt weld
- Inconel 713C is also good for hydrogen-atmosphere brazing with normal high-heat brazing alloy with electroplated mating surfaces
Inconel 713C Applications
Inconel 713C is most commonly used for jet engine gas turbine blades.
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