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Alloy 718 – High‑Performance Nickel‑Chromium Steel

Alloy 718 is a precipitation hardenable nickel chromium alloy. As the major alloy elements are molybdenum, niobium + tantalum, aluminium and titanium, Alloy 718 gives exceptionally high yield, good corrosion resistance, tensile and creep rupture properties at temperatures up to 700°C (1300F). Broder Metals Group stocks Alloy 718 in sizes from 1/2” (12.7 mm) to 4” (101.6 mm) backed up by key sizes above this core range. Our stock is bought to API 6A 718 and NACE and as such meets most application uses for the oil industry to maximise resistance to stress corrosion cracking or treated to give maximum strength and high creep resistance and weldability. Different heat treatments are available: Solution annealed and Age hardened.

Properties

General

PropertyValueComment

Grain size

2 μm

Maximum, ASTM E112

Dimension

PropertyValue

Length

12.7 - 103.6 mm

Mechanical

PropertyTemperatureValueComment

Charpy impact energy, V-notch

-60.0 °C

68 J

Average

Charpy impact energy, transverse

-60.0 °C

47 J

Single value

Elongation

23.0 °C

20 %

Hardness, HBW

23.0 °C

298 - 363 [-]

Hardness, Rockwell C

23.0 °C

32 - 40 [-]

Reduction of area

23.0 °C

35 %

Tensile strength

23.0 °C

1034 MPa

Yield strength Rp0.2

23.0 °C

120 - 145 MPa

Chemical properties

PropertyValueComment

Aluminium

0.4 - 0.6 %

Bismuth

5E-5 %

Boron

6E-3 %

Calcium

3E-3 %

Carbon

0.045 %

Chromium

17 - 21 %

Cobalt

1 %

Copper

0.23 %

Iron

Balance

Lead

1E-3 %

Magnesium

6E-3 %

Manganese

0.35 %

Molybdenum

2.8 - 3.3 %

Nickel

55 %

Other

4.78 - 5.2 %

Cb+Ta

Phosphorus

0.01 %

Selenium

5E-5 %

Silicon

0.35 %

Sulfur

0.01 %

Titanium

0.8 - 1.15 %

Technological properties

Property
Application areas

Ideal applicationsfor Alloy 718 are in oil tools, such as gate valves, choke stems, etc., and high strength applicationssuch as fasteners and turbines.


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