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Inconel X-750/ Alloy X-750/ UNS N07750/ W. Nr. 2.4669
Inconel X-750/ Alloy X-750/ UNS N07750/ W. Nr. 2.4669

Inconel X-750/ Alloy X-750/ UNS N07750/ W. Nr. 2.4669

Inconel X-750, also known as Alloy X-750, with the UNS designation N07750 and W. Nr. 2.4669, is an age-hardenable nickel-chromium superalloy used for its corrosion and oxidation resistance and high strength at temperatures up to 820 °C (1500 °F), known for its excellent mechanical properties at high temperatures. This alloy exhibits high strength, excellent corrosion resistance, and good fabricability, making it suitable for a wide range of applications. Inconel X-750 is often used in high-temperature environments, including gas turbine components, rocket engines, nuclear reactors, and industrial heating applications. Its combination of high strength and corrosion resistance makes it a valuable material in demanding conditions.

Inconel X-750

Technical Data

Chemical Composition

Nickel (Ni)

70% min

Copper (Cu)

14-17%

Iron (Fe)

5-9%

Titanium (Ti)

2.25-2.75%

Aluminum (Al)

0.4-1%

Niobium+Tantalum (Nb+Ta)

0.7-1.2%

Manganese (Mn)

1% max

Silicon (Si)

0.5% max

Sulfur (S)

0.01% max

Copper (Cu)

0.5% max

Carbon (C)

0.08% max

Cobalt (Co)

1% max

Physical Properties

Density

lb/in3

0.299

 

g/cm3

8.28

Melting Range

°F

2540-2600

 

°C

1393-1427

Curie Temperature

°F

 

 

As hot-rolled

-225

Triple-heat-treated (2100°F/2 hr, A.C.

 +1500°F

 

 

/24 hr, A.C., + 1300°F/20 hr, A.C.)

-193

Magnetic Permeability, 70°F

200H

 

 

As Hot-Rolled

1.0020

 

Triple-heat-treated (2100°F/2 hr, A.C.

+1500°F

 

/24 hr, A.C., + 1300°F/20 hr, A.C.)

1.0035

Emissivity

oxidized surface

 
 

600°F

0.895

 

2000°F

0.925

Linear Contraction during Precipitation Treatment (1300°F/20

 hr)

in/in

 
 

 Hot-Rolled

0.00044

 

20% Cold-Rolled

0.00052

 

Annealed

0.0002

Mechanical Properties

Temperature

Yield strength

Tensile strength

Elongation

Rp 0.2

Rm

A

°C

°F

MPa

ksi

MPa

ksi

%

20

68

975

141.1

1325

192.2

23.6

Inconel X-750

Applications

    Inconel X-750 is utilized in a variety of applications due to its excellent mechanical properties and high-temperature performance. Some typical applications include:

    1. Gas turbine engine components: Inconel X-750 is used in the manufacturing of turbine blades, seals, and other high-temperature components in gas turbine engines due to its strength and corrosion resistance at elevated temperatures.

    2. Rocket engines and space exploration: The alloy is employed in critical components for rocket engines and other aerospace applications where high strength and resistance to extreme temperatures are required.

    3. Nuclear reactors: Inconel X-750 finds use in the construction of reactor core components and other critical parts in nuclear reactors due to its high-temperature strength and resistance to corrosion.

    4. Industrial heating applications: It is used in industrial heating elements, furnace components, and heat-treating fixtures due to its ability to withstand high temperatures and mechanical stress.

    5. Springs and fasteners: Inconel X-750 is commonly used in the manufacturing of springs, fasteners, and other high-stress components where a combination of high strength and corrosion resistance is essential.

    6. Oil and gas industry: It finds applications in downhole and wellhead components, as well as in equipment for sour gas environments, due to its resistance to corrosion and high-temperature properties.

Inconel X-750

Available Products and Standard Specifications

Specifications for Inconel X-750 include the following:

RoBar, Rod and Forgings

Plate, Sheet, and Strip

Wire

ASTM B 637/ASME SB 637

SAE AMS 5542 and 5598

SAE AMS 5698 and 5699

Standard product forms of Inconel X-750 are pipe, tube, sheet, strip, plate, round bar, flat bar, forging stock, hexagon and wire. The products are available in a wide variety of sizes. Please contact us at sales@cocessalloys.com for full information. 

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