Inconel 718  

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SPECIFICATIONS :

AMS 5589 DIN 2.4668 SPS M275
AMS 5590 DIN 2.4688 SPS M637
AMS 5596 GE B14H89 UNS N07718
AMS 5597 GE B50 TF14  
AMS 5662 GE B50 TF69  
AMS 5663 GE B50TF14  
AMS 5664 GE B50TF15  
AMS 5832 PWA 1009  
ASTM B637 PWA 1010  
ASTM B670 PWA 1033  
RBO 170-153    


CHEMISTRY DATA :

Aluminum 0.2 - 0.8
Boron 0.006 max
Carbon 0.08 max
Chromium 17 - 21
Cobalt 1 max
Copper 0.3 max
Iron Balance
Manganese

0.35 max

Molybdenum 2.8 - 3.3
Nickel 50 - 55
Niobium 4.75 - 5.5
Phosphorus 0.015 max
Silicon 0.35 max
Sulphur 0.015 max
Titanium 0.65 - 1.15S

GENERAL INFORMATION :

  • Principal Design Features
    This is a high-strength, high-temperature resistant and corrosion resistant nickel-chromium alloy. It is suitable for use at cryogenic temperatures and also for use in air up to 1300F. The alloy is readily worked and can be age-hardened.

  • Applications
    Applications include gas turbine hot section components and cryogenic storage tanks.

  • Physical Data

    Density (lb / cu. in.) 0.29
    Specific Gravity 7.98
    Specific Heat
    (Btu/Ib/DegF-[32-212 Deg F)
    0.104
    Electrical Resistivity
    (microhm – cm (at 68Deg F)
    753
    Melting Point (Deg F) 2420
    Poissons Ratio 0.284
    Thermal Conductivity 77
    Mean Coeff Thermal 
    Expansion
    7.3
    Magnetic Permeability 1.001
    Modulus of Elasticity Tension 29

  • Forms & Shapes :
    Wire, Sheet, Plate, Strip, Round Bars, Hexagonal, Flats, Square, Angle, Channel, Blanks, Tubes, Billets, Pipes, Pipe Fittings, Forging Rings, Special Shape Forgings, Fasteners Etc.

Nickel & Alloy
Aluminum & Alloy
Stainless Steel
Titanium & Alloy
Copper & Alloy