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Inconel 713C Bar for High-Temperature Gas Turbine Blades & Nozzles
Discover Inconel 713C bar, perfect for high-temperature gas turbine blades and nozzles. Our bars come in sizes of 80*700mm , 80*780mm , and 80*880mm. We support VTB payment for your convenience. Explore its superior high-temperature resistance and high-strength features now!
- Overview
- Specification
- Applications
- FAQs
- Recommended Products
- High-Temperature Resistance: Inconel 713C maintains its strength and integrity even at elevated temperatures, making it ideal for use in gas turbine engines.
- Oxidation and Corrosion Resistance: This alloy offers exceptional resistance to oxidation and corrosion, ensuring long-term durability in extreme environments.
- Excellent Fatigue Resistance: It is designed to withstand thermal cycling and mechanical stresses, ensuring performance in demanding conditions.
- Superior Strength-to-Weight Ratio: With high strength and low density, Inconel 713C is perfect for weight-sensitive applications like turbine blades and nozzles.
- Precise Alloy Composition: Engineered for precise performance, this material meets the strict standards required in aerospace and high-performance turbine applications.
Inconel 713C bar is a nickel-based superalloy designed specifically for high-temperature applications, including gas turbine blades and nozzles. Known for its exceptional resistance to oxidation and thermal fatigue, Inconel 713C is widely used in industries where high-performance materials are critical. Available in sizes of 80*700mm, 80*780mm, and 80*880mm, this alloy offers excellent strength and durability under extreme operating conditions.
Key Features of Inconel 713C bar
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·ft²·°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 |
Applications of Inconel 713C bars
Inconel 713C is primarily used in:
- Gas Turbine Blades & Nozzles: Ideal for high-performance turbine components due to its excellent high-temperature and fatigue resistance.
- Aerospace Industry: Commonly used in aircraft engines and other aerospace applications where high temperatures and mechanical stress are prevalent.
- Power Generation: Used in components for power plants, including turbine blades and exhaust nozzles, where high strength and durability are required.
- Marine Applications: Utilized in turbines and other parts exposed to extreme thermal conditions.
FAQs:
What sizes are available for Inconel 713C bars?
Our Inconel 713C bars are available in the following sizes: 80*700mm, 80*780mm, and 80*880mm.
What industries use Inconel 713C bars?
Inconel 713C is commonly used in the aerospace, power generation, and marine industries, especially for gas turbine blades and nozzles.
Can I use Inconel 713C for high-temperature applications?
Yes, Inconel 713C is designed to perform under extremely high temperatures and is perfect for turbine blades and nozzles exposed to thermal stress.
Do you support VTB payment?
Yes, we support VTB payment for your convenience. Feel free to contact us for more details.
What are the main advantages of using Inconel 713C?
Inconel 713C offers exceptional high-temperature resistance, oxidation resistance, and mechanical strength, making it ideal for demanding applications in turbine technology.
