Material – DIN WL 2.4668

Standard Specification for Aerospace; Heat-Resisting Nickel Alloy Bars and Wire for Screws and Bolts

Group - Non-Ferrous Nickel Alloys

Sub Group - DIN WL 2.4668 Aerospace; Heat-Resisting Nickel Alloy Bars and Wire for Screws and Bolts

Application - Intended for Valve, Pump, General Engineering, Automotive and other Industries

Grade Belongs to the Industry - Bars and Wire for Screws and Bolts

Chemical Composition
CarbonC %0.020 - 0.080
SiliconSi %0.350 max.
ManganeseMn %0.350 max.
ChromiumCr %17.000 - 21.000
MolybdenumMo %2.800 - 3.300
AluminiumAl %0.300 - 0.700
NiobiumNb %4.800 - 5.500
PhosphorusP %0.015 max.
SulphurS %0.015 max.
BoronB %0.002 - 0.006
CobaltCo %1.000 max.
TitaniumTi %0.700 - 1.150
NickelNi %50.000 - 55.000
LeadPb %0.002 max.
SilverAg %0.0005 max.
Heat Treatment
As-Cast or Annealing or Age Hardning
Mechanical Properties
Tensile Strength in Mpa960 min.
Yield Strength in Mpa550 min.
Elongation in %5 min.
Reduction of Area in %8 min.
Hardness in BHN277 min.
Impact in Joule-

Cross Reference Table

Material Standard Country Grade Belong to the Industry
Inconel 718 SAE USA Tube
N07718 UNS USA Tube
B670 N07718 ASTM USA Plate, Sheet and Strip
B983 N07718 ASTM USA Pipe and Tube
B834 N07718 ASTM USA Pipe Flange, Fitting and Valve
B637 N07718 ASTM USA Bar and Forging
SB-637 N07718 ASME USA Bar and Forging