High Quality Inconel 718/Gh4169/Uns No7718/Mo3 Plate

Product Details
Customization: Available
Product Type: Sheet
Material: Ni Cr
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Number of Employees
15
Year of Establishment
2012-02-06
  • High Quality Inconel 718/Gh4169/Uns No7718/Mo3 Plate
  • High Quality Inconel 718/Gh4169/Uns No7718/Mo3 Plate
  • High Quality Inconel 718/Gh4169/Uns No7718/Mo3 Plate
  • High Quality Inconel 718/Gh4169/Uns No7718/Mo3 Plate
  • High Quality Inconel 718/Gh4169/Uns No7718/Mo3 Plate
  • High Quality Inconel 718/Gh4169/Uns No7718/Mo3 Plate
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Basic Info.

Model NO.
Inconel 718
Condition
Bright, Annealed
Color
Bright
Size
1.2mm, 1.6mm, 2.0mm, 3.17mm, 4.76mm
Packing
Wooden Case
Transport Package
Wooden Case
Specification
Customized
Trademark
Ualloy
Origin
China
HS Code
750522000
Production Capacity
500 Tons/Year

Packaging & Delivery

Package Size
50.00cm * 50.00cm * 40.00cm
Package Gross Weight
50.000kg

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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