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Inconel® 718 Nickel Alloy – AMS 5662 – UNS N07718

Inconel® 718 Nickel Alloy – AMS 5662 – UNS N07718

400 series stainless steel

Nickel Alloy 718, frequently called Inconel® 718, is a precipitation hardenable corrosion and heat-resistant nickel alloy available in bars, forgings, sheets and plates. AMS 5662 and AMS 5663 limit sizes 10” and less between parallel sides with maximum cross-section area of 78 in2 for bars and finished forgings. It is a multiple melted alloy including VIM and/or VAR processes.

 

The alloy has high strength and creep rupture properties up from cryogenic temperatures to 1300° F, along with corrosion resistance and weldability with resistance to cracking. Nickel Alloy 718 has good resistance to oxidation and corrosion at temperatures and atmospheres in jet engine and gas turbine operations. It is also corrosion resistant to acids, sea water and sour oil and/or gas.

<<Inconel® 718 Nickel Alloy – AMS 5662 – UNS N07718 DATA SHEET>>

Chemical Composition:

Symbol Element Min % Max %
C Carbon 0.08%
Mn Manganese 0.35%
Si Silicon 0.35%
P Phosphorus 0.015%
S Sulfur 0.015%
Cr Chromium 17.00% 21.00%
Ni Nickel 50.00% 55.00%
Mo Molybdenum 2.80% 3.30%
Cb (Nb) Columbium (Niobium) 4.75% 5.50%
Ti Titanium 0.65% 1.15%
Al Aluminum 0.20% 0.80%
Co Cobalt 1.00%
B Boron 0.006%
Cu Copper 0.30%
Pb Lead 0.0005% (5 ppm)
Bi Bismuth 0.00003% (0.3 ppm)
Fe Iron remainder

 

Minimum Tensile Properties at Room Temperature:

Sample Orientation per Diameter or Least Distance between Parallel Sides Tensile Strength Yield Strength 0.2% Offset Elongation in 4D Reduction of Area
Longitudinal
Size 10” and under
185 ksi 150 ksi 12% 15%
Long Transverse
Forgings 5” and under
180 ksi 150 ksi 10% 12%
Long Transverse
Forgings Over 5” & ≤ 10”
180 ksi 145 ksi 10% 12%
Transverse
Bars 5” and under
180 ksi 150 ksi 6% 8%
Transverse
Bars Over 5” & ≤ 10”
180 ksi 145 ksi 6% 8%

* Precipitation Heat Treated per AMS 5662 Paragraph 3.5.1.2

 

Tensile Properties at 1200°F:

Sample Orientation per Diameter or Least Distance between Parallel Sides Tensile Strength Yield Strength 0.2% Offset Elongation in 4D Reduction of Area
Longitudinal
Size 5” and under
145 ksi 125 ksi 12% 15%
Longitudinal
Size over 5% and ≤ 10”
145 ksi 122 ksi 12% 15%
Long Transverse
Forgings 5” and under
140 ksi 125 ksi 10% 12%
Long Transverse
Forgings Over 5” & ≤ 10”
140 ksi 122 ksi 10% 12%
Transverse
Bars 5” and under
140 ksi 125 ksi 6% 8%
Transverse
Bars Over 5” & ≤ 10”
140 ksi 122 ksi 6% 8%

* Precipitation Heat Treated per AMS 5662 Paragraph 3.5.1.2
* Samples at 1200° F per AMS 5662 Paragraph 3.5.1.2.1.2

 

Inconel®718 Nickel Applications:

Nickel Alloy 718 aerospace applications are jet engines, rocket motors, spacecraft, and fasteners. It is also used in oil and gas applications such as logging tools, pump shafts, fishing tools, and wellhead components.

 

Common Trade Names:

Nickel 718

Inconel® 718

Alloy 718

ATI 718

ATI 718Plus®

Pyrowear® 718

Nicrofer 5219 Nb

DIN 2.4668

W-Nr 2.4668 (Werkstoff Number)

 

Common Specifications:

AMS 5662 Bars, Forgings, Rings

AMS 5663 Bars, Forgings, Rings

AMS 5664

AMS 5596 Sheet, Plate, Strip

AMS 5597 Sheet, Plate, Strip

AMS 5441 718Plus® ATI

ASTM B637

ASME SB-637

UNS N07718

B50T69

B50TF15

C50TF13

DMD 424.22

EMS 55446

EMS 55476

EMS 52503

NACE MR0175 (Oil & Gas)

API 6A718 (Oil & Gas)

ISO 9723

 

Fabrication

Forging: 2050°F max for hot-working. Hot-cold working from 1700/1850°F

Machinability: Can be machined in either annealed or age-hardened condition

Welding: Weldable in either the annealed or age-hardened condition

 

Heat Treatment

Solution Treatment : 1700°- 1850° then air cool

Precipitation Hardening : 1325° F for 8 hours, furnace cool to 1150° F

We also supply
MARS190 D6AC AMS 4130
AMS 4340 MOD AMS 4340 AMS 4330 MOD
AMS 9310 AMS 13-8 PH AMS 15-5 PH
AMS 17-4 PH AMS 625 AMS 718
AerMet® 100 Maraging 250 Maraging 300
Maraging 350 Titanium Grade 5 Ti-6Al-4V ELI Titanium

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