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   Inconel X-750

 
MIL-N-7786, MIL-N-8550, MIL-S-23192, MIL-N-24114; NACE MR-01-75; AFNOR NC 15 FeT, SAE AMS 5542, 5582, 5583, 5598, 5667 - 5671, 5698, 5699, 5747, 7246, UNS N07750; BS HR505; ASTM B 637; ASME SB-637, Boiler Code Section III; Werkstoff Nr. 2.4669
Chemical Requirement
Alloy

%

Ni

Cr

Fe

Nb

Co

C

Mn

Si

S

Cu

Al

Ti

Inconel X-750

Min.

 

14

5.0

0.7

 

 

 

 

 

 

0.4

2.25

Max.

70

17

9.0

1.2

1.00

0.08

1.00

0.5

0.01

0.5

1.0

2.75

Material Notes:
Nickel content above includes cobalt; Nb content above includes Ta. A nickel-chromium alloy similar to INCONEL alloy 600 but made precipitation hardenable by additions of aluminum and titanium. The alloy has good resistance to corrosion and oxidation along with high tensile and creep-rupture properties at temperatures to about 1300°F (700°C). Its excellent relaxation resistance is useful for high-temperature springs and bolts. Used in gas turbines, rocket engines, nuclear reactors, pressure vessels, tooling, and aircraft structures.

 

Physical Properties

Metric

English

Comments

 

Density

8.28 g/cc

0.299 lb/in³

 


Mechanical Properties

 

Tensile Strength, Ultimate

1250 MPa

181000 psi

 Precipitation Hardened. Value at room temperature. Value at 550°C is 1120 MPa.

Tensile Strength, Yield

850 MPa

123000 psi

 Precipitation Hardened. Value at room temperature; 0.2% offset. Value at 550°C is 760 MPa.

Elongation at Break

30 %

30 %

 Precipitation Hardened. Value at room temperature. Value at 550°C is 22%.

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