Steel products
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Alloy 718
Nickel Alloy 718, also known as Inconel 718®, is a precipitation hardenable/corrosion and heat-resistant nickel alloy with excellent tensile and impact strength at extreme temperatures from cryogenic environment up to 1300℉/704℃.
- Applications
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- Aviation: Jet Engine Components / Rocket Motors / Fasteners / Thrust Reversers
- Gas Turbine Components
- Cryogenic Storage Tanks - Applicable specifications
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UNS: N07718
AMS5662: Solution treated / Precipitation-Hardenable bars, forgings, and rings.
AMS5663: Solution and Precipitation Heat Treated bars, forgings, and rings
AMS5596: Sheet, Strip and Plate (Annealed)Alloy 718 C Mn Si P S Cr Ni Mo Nb Ti Ingredient values ≦0.08 ≦0.35 ≦0.35 ≦0.015 ≦0.015 17.00～21.00 50.00～55.00 2.80～3.30 4.75～5.50 0.65～1.15 - Mechanical Properties
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- Hardness at Solution Treated Condition≦277HB(AMS5662)
- Hardness at Aged Condition≧331HB or equivalent(AMS5663)
- Response to heat treatmenthardness(HB) ≦277
- Processability and characteristics
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Our Stock Portfolio:
Applicable Specifications:
AMS5662/AMS5663 Capable of/B50TF15(Chemistry Only)/C50TF13(Chemistry Only)
ASME SB637/ASTM B637/UNS N07718
RR9000/SABRe/GE-S-400(S-Spec-35)/GE-S-1000(S-Spec-35-1)
Cert In accordance with EN 10204 3.1 -
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