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Inconel 718

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UNS Number N07718


Inconel 718 is an age-hardenable nickel-chromium alloy that combines corrosion resistance with high strength and good fabricability. It has a high creep-rupture strength at temperatures up to 700℃. Its excellent relaxation resistance contributes to its application in springs. 


Applications:
Inconel 718 is applied in Gas turbine engines, rocket motors, nuclear reactors and spacecraft, etc.

Forms of Inconel 718 Available at BAIDE ALLOY
• Sheet
• Plate
• Bar
• Wire

Inconel 718 Chemical composition:

Alloy % Ni Cr Fe Mo Nb Co C Mn Si S Cu Al Ti
718 Min. 50 17 balance 2.8 4.75





0.2 0.7
Max. 55 21 3.3 5.5 1 0.08 0.35 0.35 0.01 0.3 0.8 1.15


Inconel 718 Physical properties:

Density 8.2 g/cm³
Melting point 1260-1340 ℃


Inconel 718 Alloy minimum mechanical properties in the roomtemperature:

Alloy Tensile strength
Rm N/mm²
Yield strength
R P0. 2N/mm²
Elongation
A 5 %
Brinell hardness HB
Solution treatment 965 550 30 ≤363


ASTM Specifications

Sheet/Plate Bar
B670 B637


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Tel: 0086-523-89558188, 89550188  
Fax: 0086-523-89555688
Email:  sales@jsbdalloy.com
Factory Add:
Alloy Industrial Park of Shiyan Town, Dongtai, Jiangsu, China
Office Add:
Room 110, Building 1, No. 98 Fenghuang West Road, Taizhou City, Jiangsu China.
 

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