May 07, 2026 Leave a message

Super Alloy Inconel 713C Casting Round Rods Guide

In the aerospace and power generation industries, turbine rotors are core components of engines, operating in some of the world's most demanding environments. At speeds exceeding 100,000 rpm and temperatures reaching 1800°F (982°C), the tolerance for material failure is zero.

 

As a Tier 1 supplier of high-temperature alloys, Gnee Alloy offers premium Inconel 713C bars specifically designed for these critical components. Our master alloy bars, produced using a vacuum ion melting (VIM) process, possess the metallurgical stability required to push the limits of modern turbine technology.

Contact our professionals to recommend the right alloy for your project

 
Super Alloy Inconel 713C Casting Round Rods Buying Guide
 
Super Alloy Inconel 713C Casting Round Rods

Super Alloy Inconel 713C Casting Round Rods Buying Guide

Inconel 713C cast round bars are precipitation-hardening nickel-chromium-based superalloys designed for high-temperature, high-stress applications up to 1800°F (980°C), such as gas turbine blades and integral bladed disks. These bars (UNS N07713) exhibit excellent resistance to thermal fatigue and are typically manufactured using vacuum investment casting processes for use in the aerospace and industrial energy sectors.

What are the properties of Inconel 713c material?

Inconel 713c exhibits extremely high corrosion resistance. Upon heating, a thick, stable oxide layer forms on the surface, providing protection. This material maintains its strength over a wide temperature range. This metal alloy is particularly suitable for applications with temperatures up to 900°C.

Inconel 713c Material

Inconel 713C Specifications and Availability

Diameter Range: Precision casting process, diameter range from 6.0 mm to 300 mm.

Equivalent Alloy: Inconel 713LC (low carbon alloy), commonly used to enhance ductility.

Surface Finish: Typically supplied in cast, black, or polished condition.

 

1. Inconel 713C Alloy Rod Technical Specifications

Property Value / Specification
UNS Number UNS N07713
Material Standard AMS 5391 / GE C50TF15
Melting Technology 100% Vacuum Induction Melting (VIM)
Standard Diameters Φ75mm, Φ80mm, Φ100mm
Operating Temp Up to 1800°F (982°C)
Primary Strength Creep Rupture Strength (Precipitation Hardened)

 

2. Chemical Composition Of Inconel 713c Rods

Alloy % Ni Cr Fe Mn Si Mo Zr Ti Cu Co Al C S
713C Min. Bal 12.0 - - - 3.8 0.05 0.5 - 1.8 5.5 - -
Max. 14.0 2.5 0.25 0.5 5.2 0.15 1.0 0.5 2.8 6.5 0.20 0.015

 

3. Physical Properties Of Inconel 713c Rods

Density 7.913 g/cm³
Melting point 1260℃-1288℃

Click to download the Inconel 713C alloy PDF file now

 

4. Stress fracture and creep properties of Inconel 713C round bars

Temperature Stress Rupture Life Notes
650°C 550 MPa ~100 hours Short-term
650°C 450 MPa ~1,000 hours Long-term
700°C 350 MPa ~100 hours Short-term
700°C 280 MPa ~1,000 hours Long-term
760°C 240 MPa ~100 hours -
800°C 250 MPa ~100 hours Short-term
800°C 200 MPa ~1,000 hours Long-term
850°C 180 MPa ~100 hours -
900°C 150 MPa ~100 hours Short-term
900°C 120 MPa ~1,000 hours Long-term
950°C 100 MPa ~100 hours Short-term
950°C 70-80 MPa ~1,000 hours Long-term

 

Inconel 713C round bar creep strength

Temperature Creep Strength (0.1% / 100h)
800°C ~200 MPa

 

5. Inconel 713C Casting Bar Size Capability

Parameter Typical Range Tolerance
Diameter 10 – 100 mm ±0.2 – ±0.5 mm
Length 50 – 300 mm ±0.5 – ±1.0 mm
Minimum Diameter 8 – 10 mm -
Dimensional Tolerance Grade CT7 – CT9 ISO 8062
Surface Roughness (As-Cast) Ra 3.2 – 6.3 µm -
Surface Roughness (After Machining) Ra 0.8 – 1.6 µm Requires subsequent machining

Contact us to customize Inconel 713C products to fit your project dimensions

 

6. Typical applications of Inconel 713C bar stock

Jet aircraft turbine blades and guide vanes
Industrial gas turbine components
Automotive turbocharger rotors

Industrial gas turbine components
Industrial gas turbine components
Jet aircraft turbine blades and guide vanes
Jet aircraft turbine blades and guide vanes
Automotive turbocharger rotors
Automotive turbocharger rotors

 

Why Choose Gnee as Your Nickel-Based Alloy Supplier

✅ Over 18 years of export experience, products sold to more than 80 countries

✅ Certified by ISO, SGS, and BV

✅ Global inventory of Inconel, Hastelloy, Incoloy, and Monel alloy tubing, plates, and bars

✅ Custom processing services available – including cutting, polishing, CNC machining, and packaging

✅ Fast delivery within 7-15 days, supported by global logistics partners

Gnee Steel inconel 713C Certificate

Gnee Steel inconel 713C Certificate

 

📦 Packaging and Shipping

All Nickel Based Alloy products are packaged using the following methods:

Wooden pallets or crates

Moisture-proof packaging

Labels with furnace number, standard, and size labels

Shipped worldwide by sea, air, or express

Gnee Steel inconel 713C Product Packing

 Gnee Steel inconel 713C Product Packing

Contact us for the latest export price quote for 713C Alloy

FAQ

 

Q: Why is Inconel 713C preferred over 718 for turbine rotors?
A: While Inconel 718 is a fantastic alloy, it loses significant strength above 1200°F (650°C). For the "hot end" of a turbine, where temperatures reach 1800°F, the Creep Rupture Strength of 713C is far superior, making it the only choice for integral rotors.

 

Q: How do you ensure batch-to-batch consistency for long-term projects?
A: We utilize standardized VIM melting protocols and ICP-MS testing for every heat. This ensures that the Al/Ti balance remains identical across years of supply, which is critical for maintaining stable casting parameters.

 

Q: Do you offer annual supply contracts for OEM manufacturers?
A: Yes. We specialize in Annual Supply Contracts that protect our clients from nickel price volatility and ensure a steady flow of premium feedstock for high-volume production.

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