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Inconel 713C,600,601,617,625,690,718,X750
DLX
Bright Annealed
Customized
ISO9001, ROHS
10kg
15-30 Days
Industry,Military,Aerospace
Product Description
Inconel 713C is a precipitation-hardened nickel-chromium alloy widely recognized for its excellent high-temperature strength and oxidation resistance. It is commonly used in aerospace and UAV engine systems where materials must withstand prolonged exposure to extreme heat and mechanical stress.
This alloy maintains structural integrity at temperatures up to 980°C (1800°F), making it ideal for turbine-related components. Its chemical composition, including aluminum and molybdenum, enhances creep resistance and long-term stability.
Our Inconel 713C rods are available in the following standard sizes:
80 × 780 mm
80 × 880 mm
80 × 700 mm
Exceptional heat resistance for high-temperature environments
Excellent creep and fatigue resistance
Superior oxidation and hot corrosion resistance
High structural stability under thermal stress
Designed for aerospace and UAV engine components
Precision machining and consistent quality
Supports secure international payments including VTB
Specification
Chemical Composition (wt.%)
| Element | Content (AMS 5391) |
|---|---|
| Chromium (Cr) | 12.00 – 14.00 |
| Molybdenum (Mo) | 3.80 – 5.20 |
| Niobium + Tantalum (Nb+Ta) | 1.80 – 2.80 |
| Aluminum (Al) | 5.50 – 6.50 |
| Titanium (Ti) | 0.50 – 1.00 |
| Carbon (C) | 0.08 – 0.20 |
| Boron (B) | 0.005 – 0.015 |
| Zirconium (Zr) | 0.05 – 0.15 |
| Silicon (Si) | ≤ 0.50 |
| Manganese (Mn) | ≤ 0.25 |
| Iron (Fe) | ≤ 2.50 |
| Copper (Cu) | ≤ 0.50 |
| Nickel (Ni) | Balance |
| Property | Value |
|---|---|
| Density | 7.91 g/cm³ |
| Melting Range | 1260 – 1288 °C |
| Thermal Expansion Coefficient | 5.92 – 9.48 ×10⁻⁶ /°F (70–2000°F) |
| Thermal Conductivity | 146 – 334 BTU·in/hr·ft⊃2;·°F |
| Tensile Strength | ≥ 760 MPa (110 ksi) |
| Yield Strength (0.2%) | ≥ 690 MPa (100 ksi) |
| Elongation | ≥ 3% |
| Hardness | HRC 30 – 42 |
| Creep Rupture Strength (980°C / 30h) | 152 MPa |
| Max Service Temperature | ≤ 900 °C |
Application Field
Inconel 713C round bars are widely used in advanced engineering fields, including:
UAV (Unmanned Aerial Vehicle) engine components
Aerospace turbine blades and hot-section parts
Military and defense equipment
Gas turbine systems
High-temperature structural components
Power generation and thermal equipment
About us
CHANGZHOU DLX ALLOY CO, LTD was established in 2002 and has got ISO9001 International Quality Management System Certificate and SGS Certificate. Our factory is professional in researching and producing special alloy material. From melting, drawing, heat treatment, finishing and testing .We offer nickel-based, copper-based, and iron-based alloys, including super alloy, welding materials, anti-corrosion alloy, precision alloy, FeCrAl alloy, NiCr alloy, CuNi alloy, thermocouple and etc, in the form of wire, strip, ribbon, bar, tube, plate.
FAQ
A: It offers excellent high-temperature strength, oxidation resistance, and creep resistance, which are critical for UAV engine performance and durability.
A: Standard sizes include 80×780 mm, 80×880 mm, and 80×700 mm.
A: Inconel 713C can operate effectively at temperatures up to approximately 980°C (1800°F).
A: Yes, we support VTB payment along with other secure international payment methods.
A: Yes, it is widely used in aerospace and UAV systems due to its excellent mechanical and thermal properties.
A: Yes, material test certificates and other documentation can be provided upon request.
