• Inconel 718/Gh4169/Uns No7718/Mo3/Na 51/Nc19fenb Alloy Wire/Rod
  • Inconel 718/Gh4169/Uns No7718/Mo3/Na 51/Nc19fenb Alloy Wire/Rod
  • Inconel 718/Gh4169/Uns No7718/Mo3/Na 51/Nc19fenb Alloy Wire/Rod
  • Inconel 718/Gh4169/Uns No7718/Mo3/Na 51/Nc19fenb Alloy Wire/Rod
  • Inconel 718/Gh4169/Uns No7718/Mo3/Na 51/Nc19fenb Alloy Wire/Rod
  • Inconel 718/Gh4169/Uns No7718/Mo3/Na 51/Nc19fenb Alloy Wire/Rod

Inconel 718/Gh4169/Uns No7718/Mo3/Na 51/Nc19fenb Alloy Wire/Rod

Product Type: Wire
Material: Ni Cr
Condition: Bright, Annealed
Color: Bright
Size: 1.2mm, 1.6mm, 2.0mm, 3.17mm, 4.76mm
Packing: Wooden Case
Customization:
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Basic Info.

Model NO.
Inconel 718
Transport Package
Wooden Case
Trademark
Ualloy
Origin
China
HS Code
750522000
Production Capacity
500 Tons/Year

Product Description

Inconel 718

Available in any of the profile options

A Nickel-Chromium alloy being precipitation hardenable and having high creep-rupture strength at high temperatures to about 700 C (1290F). It has higher strength than Inconel X-750 and better mechanical properties at lower temperatures than Nimonic 90 and Inconel X-750.

Chemical Composition Specifications Designations Key Features Typical Applications
Element Min % Max %
C - 0.08
Mn - 0.35
Si - 0.35
P - 0.015
S - 0.015
Cr 17.00 21.00
Ni 50.00 55.00
Mo 2.80 3.30
Nb/Cb 4.75 5.50
Ti 0.65 1.15
Al 0.20 0.80
Co - 1.00
Ta - 0.05
B - 0.006
Cu - 0.30
Pb - 0.0005
Bi - 0.00003
Se - 0.0003
Fe bal
AMS 5662
AMS 5663
AMS 5832
AMS 5962
ASTM B637
GE B5OTF14/15
GE B14H89
ISO 15156-3
(NACE MR 0175)
W.NR 2.4668
UNS N07718
AWS 013
Good creep rupture strength at high temperatures
Higher strength than Inconel X-750
Better mechanical properties at lower temperatures than Nimonic 90 & Inconel X-750
Age hardenable
High temperature dynamic applications
Gas Turbines
 
Space Craft
 
Pumps
 
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 ksi
 
Heat Treatment of Finished Parts
Condition as supplied by Alloy Wire Type Temperature Time (Hr) Cooling
C F
No. 1 or Spring Temper Anneal
Age Harden
Total Age
980
720
620
1800
1330
1150
1
8
18
Air
Furnace
Air
No. 1 or Spring Temper
(for ISO 15156-3 / NACE MR 0175)
Anneal
Age Harden
1010
790
1850
1455
2
6
Air
Air
No. 1 Temper or Spring Temper Age Harden
Total Age
720
620
1330
1150
8
18
Furnace
Air
 
Properties
Condition Approx. tensile strength Approx. operating temperature
N/mm2 ksi C F
Annealed 800 - 1000 116 - 145 - -
No 1 Temper 1000 - 1200 145 - 175 - -
Spring Temper 1300 - 1500 189 - 218 - -
No 1 Temper + Annealed + Aged 1250 - 1450 181 - 210 -200 to +550 -330 to +1020
No 1 Temper + Aged 1520 - 1720 220 - 250 Contact Alloy Wire Technical Dept
Spring Temper + Annealed + Aged 1250 - 1450 181 - 210 -200 to +550 -330 to +1020
Spring Temper + Aged 1700 - 1950 247 - 283 Contact Alloy Wire Technical Dept
 

The above tensile strength ranges are typical. If you require different please ask.

 

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