Inconel X750 Superalloys to SAE AMS 5542N (2007)
Inconel X750 - Specification & Application
- SAE AMS 5542N (2007) - Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe Annealed
- SAE AMS 5582F (2012) - Nickel Alloy, Corrosion and Heat-Resistant, Seamless Tubing 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Solution Heat Treated, Precipitation Hardenable to 155 ksi (1069 MPa) Tensile Strength
- SAE AMS 5598E (2007) - Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95 (Cb (Nb) + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode, Remelted or Vacuum Induction Melted, Solution Heat Treated, Precipitation-Hardenable
- SAE AMS 5667N (2015) - Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Equalized, Precipitation Hardenable
- SAE AMS 5668J (2007) - Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 7.0Fe - 2.5Ti - 1.0Cb (Nb) - 0.70Al 2100°F (1149°C) Solution and Precipitation Heat Treated
- SAE AMS 5669B (1965) - Alloy Bars, Corrosion and Heat Resistant Nickel Base - 15.5Cr - 0.95 (Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted
- SAE AMS 5670F (2005) - Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe 1800°F (982°C) Solution Heat Treated, Precipitation-Hardenable
- SAE AMS 5671G (2007) - Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted 1800°F (982°C) Solution Heat Treated, Precipitation Hardenable
- SAE AMS 5698G (2007) - Nickel Alloy, Corrosion and Heat-Resistant, Wire 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe No. 1 Temper, Precipitation Hardenable
- SAE AMS 5699G (2007) - Nickel Alloy, Corrosion and Heat-Resistant, Wire 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Spring Temper, Precipitation Hardenable
- SAE AMS 5747D (2006) - Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe Solution Heat Treated, Precipitation Hardenable
- SAE AMS 5779E (2003) - Alloy Welding Electrodes, Covered, Corrosion and Heat-Resistant 75Ni - 15Cr - 1.5 (Cb+Ta) - 1.9Ti - 0.55Al - 5.5Fe
- SAE AMS 5583E (2013) - Nickel Alloy, Corrosion and Heat-Resistant, Seamless Tubing 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Vacuum Melted Solution Heat Treated, Precipitation Hardenable to 170 ksi (1172 MPa) Tensile Strength
- SAE J 467b (1968) - Special Purpose Alloys ("Superalloys")
- SAE J 470 (1976) - Wrought nickel and nickel-related alloys
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe Annealed
Chemical composition(wt.%) of Inconel X750 grade: to SAE AMS 5542N (2007)
Elements |
Min.(≥) |
Max.(≤) |
Similar |
Remarks |
C |
- |
0.08 |
|
|
Mn |
- |
1.0 |
|
|
Si |
- |
0.5 |
|
|
S |
- |
0.01 |
|
|
P |
- |
0.015 |
|
|
Cu |
- |
0.5 |
|
|
Fe |
5.0 |
9.0 |
|
|
Co |
- |
1.0 |
|
|
Nb |
0.70 |
1.20 |
|
|
Cr |
14.0 |
17.0 |
|
|
Ni |
70 |
- |
|
|
Al |
0.40 |
1.00 |
|
|
Ti |
2.25 |
2.75 |
|
|
Inconel X750 - Detail
Inconel X750, Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe Annealed
Mechanical properties of grade Inconel X750 SAE AMS 5542N (2007)
Proof strength Rp0.2 (MPa) |
Tensile strength Rm (MPa) |
Impact energy KV (J) |
Elongation at fracture A (%) |
Reduction in cross section on fracture Z (%) |
As-Heat-Treated Condition |
Brinell hardness (HBW) |
164 (≥) |
757 (≥) |
32 |
31 |
23 |
Solution and Aging, Annealing, Ausaging, Q+T,etc |
141 |
Physical properties of grade Inconel X750 SAE AMS 5542N (2007)
Property |
Density kg/dm3 |
Temperature T °C/F |
Specific heat J / kgK |
Thermal conductivity W/mK |
Electric resistance µΩ·cm |
Modulus of elasticity kN/mm2 |
Expansion rate |
913 (≥) |
415 (≥) |
22 |
14 |
32 |
Solution and Aging, Annealing, Ausaging, Q+T,etc |
333 |
Temp. °C/°F |
Creep strain limit (10000h) (Rp1,0) N/mm2 |
Creep rupture strength (10000h) (Rp1,0) N/mm2 |
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|
|
|
|
176 |
317 |
232 |
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Product shapes we supply: