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Model No: Inconel X750 Sheet
AMS 5542 / UNS N07750 / Inconel X750 Sheet
The AMS 5542 specification covers Inconel X750 corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate. Inconel X750 (UNS N07750) is a nickel-chromium alloy that has been strengthened with the additions of titanium and aluminum to improve its characteristics.
Delivery :
FOB
minimum order :
100 kilograms
Supply Ability :
5000Tonkilograms / Month
Stock Time :
7-10Day
Country of Origin :
CHINA
Quantity :
Inconel X750 (UNS N07750) is a nickel-chromium alloy that has been strengthened with the additions of titanium and aluminum to improve its characteristics. Fantastic choice for usage in tough settings because of its excellent corrosion and oxidation resistance. Additionally, even at temperatures as high as 1300°F (700°C), this alloy has exceptional tensile and creep rupture capabilities.
The AMS 5542 specification covers Inconel X750 corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
Chemical Composition
| Element | Content (%) |
|---|---|
| Chromium, Cr | 14-17 |
| Iron, Fe | 5-9 |
| Titanium, Ti | 2.25-2.75 |
| Manganese, Mn | 1 max |
| Niobium, Nb | 0.7-1.2 |
| Copper, Cu | 0.5 max |
| Silicon, Si | 0.5 max |
| Aluminum, Al | 0.4-1 |
| Carbon, C | 0.08 max |
| Sulfur, S | 0.01 min |
| Nickel, Ni | Remainder |
Physical Properties
| Properties | Metric | Imperial |
|---|---|---|
| Density | 8.26 g/cm³ | 0.298 lb/in³ |
| Melting point | 1413°C | 2575°F |
Mechanical Properties
| Properties | Metric | Imperial |
|---|---|---|
| Tensile strength | 1325 MPa | 192.2 ksi |
| Elongation at break (in 51 mm) | 23.60% | 23.60% |
| Reduction of area | 42% | 42% |
Heat Treatments
Sheet, Strip and Plate are available with the following heat treatments
AMS 5542 - 1300°F/20hr, AC (Constant-temperature precipitation treatment). AMS 5542 has high strength up to 1300°F
AMS 5598 - 1350°F/8hr, FC to 1150°F, hold at 1150°F for total precipitation-treating time of 18hr, AC (furnace-cool precipitation treatment. AMS 5598 has high strength up to 1300°F (Increased tensile properties to about 1100°F).
With heat treatment 1400°F/1hr, FC to 1150°F hold at 1150°F for total time of 6hr, AC (short furnace-cool precipitation treatment).
Applications
Aircraft Structures
In aircraft structures, Inconel X750 is used to make components such as high-temperature springs, bolts, and pressure vessels. The alloy’s ability to maintain its properties even at high temperatures ensures that these components are able to withstand the extreme temperatures and loads encountered during flight.
Gas Turbines
Excellent relaxation resistance also makes it useful for use in gas turbine components. Inconel X750 Sheet high strength and durability make it ideal for use in blades and discs, which are subjected to high stress levels during operation.
Rocket Engines
Also used in rocket engines, where its high-temperature resistance, excellent strength, and relaxation resistance make it ideal for use in high-stress components such as combustion chambers and nozzles.
Oil & Gas
Used in pressure vessels and other components in the oil and gas industry due to its corrosion resistance and high-temperature strength.
Energy
Inconel X750 Sheet is used in nuclear reactors, power plants, and other energy-related applications due to its high-temperature resistance and excellent creep rupture properties.
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