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Quality 2.4668

General Product Description

Material number 2.4668

Short name according to EN Alloy 718

AISI / UNS / Alloy Alloy 718, Inconel 718, UNS N07718

Applicable standards WL 2.4668, AMS5662, AMS5663, UNS N07718, ASTM B637, DIN 17744

Treatment solution annealed, bright

Variations

QualityTreatmentShapeDimension (mm)
2.4668solution annealed, brightRoundRound9,53 - 70
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Description

The material 2.4668 / Alloy 718 exhibits excellent corrosion resistance in atmospheres containing CO2, H2S and Cl. Coupled with high temperature resistance and very good cold toughness values. Applications: Oil & gas industry and aerospace.

Chemical composition (in %)

CCrMnMoNiPSNbTiSiAlBCoCuFePbBiSe
Min 0,02 17,0 - 2,8 50,0 - - 4,80 0,65 - 0,3 0,002 - - - - - -
Max 0,08 21,0 0,35 3,3 55,0 0,015 0,015 5,50 1,15 0,35 0,7 0,006 1,0 0,2 rest 0,0005 0,00003 0,0003
ElementMinMax
C 0,02 0,08
Cr 17,0 21,0
Mn - 0,35
Mo 2,8 3,3
Ni 50,0 55,0
P - 0,015
S - 0,015
Nb 4,80 5,50
Ti 0,65 1,15
Si - 0,35
Al 0,3 0,7
B 0,002 0,006
Co - 1,0
Cu - 0,2
Fe - rest
Pb - 0,0005
Bi - 0,00003
Se - 0,0003

Mechanical properties (.7)

Tensile strength Rm 900–1100 N/mm2

0.2% proof stress Rp0.2 500–700 N/mm2

Elongation at break A5 ≥ 12 %

Notched impact energy (ISO-V) – J

Hardness ≤ 277 HB

Magnetizability No

Typical areas of application

aerospace industry

oil and gas industry

turbine and engine components

chemical processing plants

General properties (.7)

Corrosion Resistance

Weldability

Forgeability

Tensionability

= Low
= Very Good

Note

All information in this data sheet has been compiled to the best of our knowledge and belief. It is for information purposes only and does not constitute a assured property or guarantee. For the suitability of the material in specific applications, we recommend carrying out appropriate inspections and tests. Any liability for damage or errors is excluded.