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Model No: UNS N07500 / Udimet 520

UNS N07500 / Udimet 520 Nickel Alloy

Udimet 520 is a precipitation-hardenable nickel superalloy offering 1,251 MPa tensile strength and 980°C service temperature. Excellent creep, fatigue, and oxidation resistance. Superior to Udimet 500. Ideal for gas turbine blades, discs, and aerospace structural components. ZYTC Alloy is AS9120B and ISO 9001 certified.
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ZYTC Alloy, a professional and reliable Chinese manufacturer and supplier of premium nickel alloys, provides high-performance Udimet 520 (UNS N07500) vacuum-melted, precipitation-hardened wrought nickel-based high-temperature alloy.
 
Developed as an upgraded iteration that compensates for the performance deficiencies of traditional Udimet 500 alloy, Udimet 520 delivers comprehensively optimized mechanical properties and high-temperature stability, making it a superior choice for extreme high-temperature and high-load industrial and aerospace applications.

Core Performance & Temperature Resistance Advantages

Udimet 520 (UNS N07500) is designed for long-term stable service at temperatures up to 980°C. It features excellent comprehensive mechanical properties, including outstanding tensile performance, superior creep resistance, durable stress rupture strength and exceptional fatigue resistance. The alloy also possesses reliable high-temperature oxidation resistance and excellent hot workability, enabling flexible thermal processing and forming.
 
It exhibits extremely stable and superior mechanical performance at room temperature and temperatures below 760°C, effectively filling the performance gaps of Udimet 500 in medium and high-temperature working environments.
 

Standard Mechanical Properties

Udimet 520 maintains balanced high strength and ductility under both room and elevated temperature conditions, with stable and standardized mechanical parameters as follows:

Chemical Composition

ElementContent (%)
Nickel, Ni52.18-59.976
Chromium, Cr18.0-20.0
Cobalt, Co11.0-14.0
Molybdenum, Mo5.50-7.00
Titanium, Ti2.90-3.25
Aluminum, Al1.80-2.30
Tungsten, W0.800-1.20
Carbon, C0.0200-0.0600
Boron, B0.00400-0.0100

Physical Properties

PropertiesMetricImperial
Density8.21 g/cm³0.297 lb/in³
Melting point1371°C2500°F

Mechanical Properties

PropertiesMetricImperial
Tensile strength (@950°C/1740°F)350 MPa50800 psi
Yield strength (@strain 0.200%, temperature 850°C/@strain 0.200%, temperature 1560°F)500 MPa72500 psi
Elongation at break (@50°C/122°F)100%100%
 
 

Fabrication and Heat Treatment

Cold Working

Standard cooling methods are used for cold forming Udimet 520™. Minimization of galling is possible with the usage of heavy duty lubricants and soft die materials though the die life is limited. Tooling is recommended in the cold working process to allow liberal radii and clearances.

Welding

Welding processes recommended for Udimet 520™ include gas-tungsten arc welding, gas metal-arc welding and shielded metal-arc welding. This alloy can be welded by the commonly used welding procedures, and the welding surfaces should be free from paint, crayon markings or oil.

Forging

Udimet 520™ is capable of being forged as it is ductile.

Forming

Conventional methods can be used to form Udimet 520™ with ease as it has good ductility. To obtain good forming results, a powerful equipment is used along with heavy- prevent embrittlement of this alloy at high temperatures.

Machinability

Udimet 520™ can be machined by conventional machining methods. and tThis alloy contains higher strength, gumminess and work-hardening qualities. Usage of water-based coolants is preferred for milling, turning or grinding. Usage of heavy lubricants is preferred for boring, drilling, broaching or tapping operations. Work-hardening of the alloy before the cutting process and chatter can be minimized by tooling and a heavy duty machining equipment.

Aging

Udimet 520™ is treated at three different temperatures to be air-hardened.

  • Heat for 4 h at 1107°C (2025°F) and cool in air.
  • Heat for 24 h at 843°C (1550°F) and cool in air.
  • Heat for 16 h at 760°C (1400°F) and cool in air.

Heat Treatment

Udimet 520™ can be hardened when heat treated.


Industrial & Aerospace Applications

With its outstanding high-temperature resistance, high strength and excellent processability, Udimet 520 superalloy is widely used in core high-temperature components of aerospace, energy and high-end industrial equipment:
  • Aerospace & Aviation: Jet engine turbine blades, turbine discs, missile body and rocket structural components
  • Energy Power Equipment: Gas turbine core components, high-temperature resistant bolts and piston parts
  • High-End Industrial Manufacturing: Precision high-temperature molds and high-stress thermal processing structural parts

Why Choose ZYTC Alloy Udimet 520 Superalloy

As a professional Chinese supplier of aerospace-grade nickel-based superalloys, ZYTC Alloy strictly implements vacuum smelting, standardized precipitation hardening heat treatment and precision processing for all Udimet 520 products. We strictly control material purity, microstructure stability and mechanical property consistency to ensure the alloy's excellent high-temperature creep resistance, fatigue resistance and oxidation resistance.
 
All products are equipped with complete MTR test reports and support third-party authoritative testing. We provide reliable customized processing and batch supply services for global aerospace, defense and high-temperature industrial projects.
 
Contact ZYTC Alloy today to obtain free Udimet 520 technical datasheets, complete performance parameter documents and competitive factory quotations!
 
📧 Email: daisy@zytcsteel.com
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