The nickel-chromium precipitation-hardenable alloy Inconel X750 is well known for its resistance to oxidation and corrosion, even at elevated temperatures. It is essential to the chemical, nuclear, and aerospace sectors due to its exceptional mechanical qualities and resilience under stress. The performance of Inconel X750 is largely dependent on its chemical composition, which strikes a balance between nickel, chromium, titanium, and aluminium. Its magnetic qualities and conformity to ASTM standards guarantee dependability in difficult applications.
The nickel-chromium alloy X-750 is precipitation-hardened and has a high strength. It is ideal for turbine blades, rocket engines, springs, nuclear reactor components, and industrial gas turbines due to its resistance to high-temperature oxidation, corrosion, and creep. X750 has an advantage in conditions where traditional alloys fail, as it maintains its mechanical strength at extremely high temperatures, unlike stainless steels.
| Element | Percentage (%) |
|---|---|
| Nickel (Ni) | 70.0 min |
| Chromium (Cr) | 14.0 – 17.0 |
| Iron (Fe) | 5.0 – 9.0 |
| Titanium (Ti) | 2.25 – 2.75 |
| Aluminum (Al) | 0.40 – 1.0 |
| Cobalt (Co) | ≤ 1.0 |
| Manganese, Silicon, Copper | ≤ 1.0 each |
Chromium helps the X750 create a durable protective oxide layer that shields it from corrosion and chemical damage. Nickel is appropriate for the chemical and marine sectors because it inhibits the cracking of chloride stress corrosion. This alloy has outstanding resistance to:
With protective coatings, X750 can withstand oxidation up to 1300°F (704°C). Exhaust valves, furnace parts, and turbine blades all benefit greatly from the chromium-rich oxide film’s ability to withstand scaling under cyclic heating. Long-term performance in industrial and aeronautical heating systems is made possible by this steadiness.
The mechanical strength of Inconel X750 is what sets it apart from many high-temperature alloys.
| Property | Value (Typical) |
|---|---|
| Tensile Strength | 130 ksi (895 MPa) |
| Yield Strength (0.2% offset) | 85 ksi (586 MPa) |
| Elongation | 25% |
| Hardness | 321 HB |
| Creep Rupture Strength | 33 ksi (228 MPa) at 1200°F for 100 hours |
These figures demonstrate the X750’s resilience to stress and its capacity to preserve mechanical integrity under harsh nuclear and aerospace environments.
The magnetic properties of Inconel X750 depend on heat treatment. In annealed condition, it is typically non-magnetic, which is advantageous for nuclear and aerospace applications. However, certain precipitation-hardened states may exhibit slight magnetism. This property must be considered when selecting the alloy for precision instrumentation.
ASTM B637-Bars, Forgings, and Forging Stock is one of then X750:
To ensure dependability, these standards control testing procedures, chemical composition, and mechanical performance.
In industries that require resistance to oxidation, corrosion, and high stress, Inconel X750 is still a vital alloy. It is essential for engineers all over the world because of its well-balanced chemical composition, compliance with ASTM standards, adaptable mechanical qualities, and demonstrated performance in nuclear, marine, and aerospace applications.
It contains nickel, chromium, titanium, and aluminum. This Inconel X750 chemical composition creates strength, corrosion resistance, and stability at high temperatures.
Generally, Inconel X750 is non-magnetic in annealed condition but may exhibit slight magnetism after certain heat treatments.
ASTM B637 (bars/forgings), ASTM B408 (alloys), and ASTM B906 (sheets/strips) regulate production and performance.
Inconel 718 offers higher strength, while Hastelloy X withstands higher temperatures. Inconel X750 provides a balance of corrosion resistance, mechanical stability, and cost-effectiveness.
Yes, but post-weld heat treatment is recommended to restore corrosion and oxidation resistance.
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