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Inconel 718 Welding Wire AMS 5832
- Description
-
Material Grade: Inconel 718, Alloy 718, Nickel 718, W.NR 2.4668, UNS N07718, AWS 013, Haynes 718, Nicrofer 5219, Allvac 718, Altemp 718, Pyromet 718, Supermet 718 and Udimet 718.
Standard Specification: AMS 5832
Element
C
Mn
Si
P
S
Cr
Ni
Mo
Cb
Ti
Al
Co
B
Cu
Fe
Min
--
--
--
--
--
17.00
50.00
2.80
4.75
0.65
0.20
--
--
--
Bal
Max
0.08
0.35
0.35
0.015
0.015
21.00
55.00
3.30
5.50
1.15
0.80
1.00
0.006
0.30
Physical Properties:
Density 8.19g/cm³ 0.296 lb/in³; Melting Point 1336°C 2437°F
Coefficient of Expansion 13.0 μm/m °C (20 – 100°C) 7.2 x 10-6 in/in °F (70 – 212°F)
Modulus of Rigidity 77.2 kN/mm² 11197 ksi; Modulus of Elasticity 204.9 kN/mm² 29719 ksiTypical Mechanical Properties – Spring Applications
∗Annealed
Heat Treatment: 1800°F (980°C)
Tensile Strength: 115 – 145 ksi; (790-1000 MPa)
Suggested Operating Conditions: -330°F to 1200°F (-200°C to 650°C)
∗Spring TemperTensile Strength: 190 – 220 ksi; (1310 – 1515 MPa)
Suggested Operating Conditions: -330°F to 1200°F (-200°C to 650°C)
∗Spring Temper + Aged
Heat Treatment: After spring coiling. Age: 1325°F (720°C) for 8 hours, furnace cool to 1150°F and hold for a total aging time of 18 hours.
Tensile Strength: 220 ksi minimum; (1515 MPa)
Suggested Operating Conditions: -330°F to 1200°F (-200°C to 650°C)Applications:
Inconel 718 is widely used in fields of gas turbine components, cryogenic storage tanks, jet engines, pump bodies and parts, rocket motors and thrust reversers, nuclear fuel element spacers, and hot extrusion tooling.
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