Aerospace Material Specification or AMS, is an SAE standard that ensures metals fulfil stringent performance, and quality standards. Inconel X-750 is a nickel-based alloy with exceptional resistance to heat and corrosion that is specified by AMS 5670. Parag Metals offers it in bars, forgings, and rings, ready for high-demand applications. The specification ensures uniform mechanical properties, dependable performance, and rigorous quality control for each batch, making it a preferred option for engineers.
AMS 5670 is used extensively in aerospace, marine, and high-performance sectors where components are subjected to high stress and harsh conditions. It is used by engineers in gas turbine parts, marine engines, and other machinery where durability and strength are required. Corrosion and oxidation resistance of the alloy make it suitable for long-term use in difficult operating conditions. It also reduces the maintenance requirements, enhancing the dependability of critical machinery.
Inconel X-750 AMS 5670 bars Suppliers in Mumbai, India
One of the key benefits of this alloy is its toughness, and resistance over a range of temperature spectra, working well at extremely low temperatures up to 1100°F (593°C). It is perfect for fasteners, springs, and other high-temperature applications. Engineers are able to form it to exact specifications without compromising strength or performance. AMS 5670 comes in various sizes and conditions to suit diverse industrial requirements. Its versatility enables it to be used in precision parts and in larger structural components. The material’s strength, flexibility, and heat resistance make it the preferred choice for rigorous industrial uses.
Other sizes are available on request. Please contact our sales team for details..
AMS 5670 Specifications We Stock
Alloy
Inconel X-750 (UNS N07750)
Product Forms
Bars, Forgings, Flash-welded Rings, and Stock for forging, flash welded rings, or heading
Condition
Solution Heat Treated at 1800°F (982°C), Precipitation Hardened
Heat Treatment
Solution Heat Treatment at 1800°F (982°C) followed by Precipitation Heat Treatment at 1350°F (732°C) for 8 hours, furnace cool to 1150°F (621°C), then hold at 1150°F for a total precipitation time of 18 hours, air cool.
Typical Applications
Components requiring heat strength from 800°F to 1100°F (427°C to 593°C), such as welded or formed parts that are precipitation heat treated to develop specific properties.