Model No: Inconel 783

Inconel 783

Inconel alloy 783 (UNS R30783/U.S. Patent 5,478,417), is an oxidation-resistant, low expansion, nickel-cobalt-iron alloy with aluminum, chromium, and niobium additions.
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FOB
minimum order :
100 kilograms
Supply Ability :
5000Tonkilograms / Month
Stock Time :
7-10Day
Country of Origin :
China
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Inconel alloy 783 (UNS R30783/U.S. Patent 5,478,417), is an oxidation-resistant, low expansion, nickel-cobalt-iron alloy with aluminum, chromium, and niobium additions. The new alloy is of considerable interest to aircraft gas turbine engine designers and materials engineers for containment and clearance control components such as rings, casings, shrouds and seals for compressors, turbines and exhaust systems.
 
The three-phase age hardenable alloy offers a range o improvements for these applications over alternative alloys in current use: A coefficient of thermal expansion approximately 20% lower than that of Inconel alloy 718. Excellent resistance to oxidation, demonstrated in cyclic tests, at temperatures up to and beyond 1300°F (704°C).
 
Resistance to SAGBO (stress accelerated grain boundary oxidation) comparable to that of Inconel alloy 718, and significantly better than that of Inconel alloy 909. A density of 0.282 lb/in3 (7.81 g/cm3), 5% less than Inconel alloy 718 or Inconel alloy 909, contributing to an important potential improvement in strength-to-weight ratios.
 
Manufacturing/processing characteristics comparable to those of Inconel alloy 718, and less limiting than those of Inconel alloy 909.

Inconel 783 Chemical Composition

ElementContent (%)
Nickel, Ni26-30
Iron, Fe24-27
Aluminum, Al5-6
Chromium, Cr2.5-3.5
Niobium, Nb2.5-3.5
Copper, Cu0.50 max
Manganese, Mn0.50 max
Silicon, Si0.50 max
Titanium, Ti0.10-0.40
Carbon, C0.03 max
Boron, B0.003-0.012
Phosphorus, P0.015 max
Sulfur, S0.005 max
Cobalt, CoBalance

Inconel 783 Physical Properties

PropertiesMetricImperial
Density7.81 g/cm30.282 lb/in3
Melting point1336-1407 °C2437-2565 °F

Inconel 783 Mechanical Properties

PropertiesMetricImperial
Tensile strength1194 MPa171 ksi
Yield strength779 MPa113 ksi
Poisson’s ratio0.310.31
Elastic modulus177.3 GPA25.72 ksi
Elongation at break24%24%

Inconel 783 Thermal Properties

PropertiesMetricImperial
Thermal expansion co-efficient (@93°C/200°F)10.08 µm/m°C5.60 µin/in°F
Thermal conductivity (@21°C/70°F)10.1 W/m-°C71 BTU in/hr.ft².°F
 

Inconel 783 Fabrication and Heat Treatment

Inconel alloy 783 has good fabricability and can be formed, machined, and welded using all the traditional procedures for nickel alloys. This alloy’s reactions are similar to that of Inconel 718

Inconel 783 Machinability

Inconel alloy 783 can be readily machined using the conventional practices for high-strength nickel alloys. In case of rough machining, the material has to be machined in the annealed condition.

Inconel 783 Hot Forming

The temperature range for hot forming of Inconel alloy 783 is from 927°C to 1121°C (1700°F to 2050°F).

Inconel 783 Heat Treatment

To heat treat this super alloy, the material has to solution annealed at 1121°C (2050°F) for 1 h, and air cooled. This should be followed by beta aging at 845°C (1550°F) for 4 h and air cooled to room temperature. Next the material is age hardened at 720°C (1325°F) for 8 h, furnace cooled at 55°C (100°F) for 1 hr to 620°C (1150°F) for 8 h and air cooled.

Inconel 783 Applications

Inconel alloy 783 is widely used in gas turbine applications.
 
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