Inconel 713c
Inconel 713c
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Inconel 713c

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. 

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Inconel 713C Alloy Properties (Theoretical)


Appearance

Metallic powder or solid in various forms

Melting Point

1260-1288 °C

Boiling Point

N/A

Density

7.913 g/cm3

Electrical Resistivity

144 µΩ·cm (20 °C)

Tensile Strength

110 psi


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

Packing:

All Wenzhou Taixin Steel's products are packed, stored, transported according to the international regulation. The products are wrapped with anti-rust paper and steel rings to prevent damage. Identification labels are tagged according to standard specification or customer's instructions. Special packing is available as per customer's requirement.Ply wooden box are available for special protection. Other kinds of packing can be offered if request.


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