BS EN 4318:2025
Aerospace series. Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980). Consumable electrode remelted. Solution treated and precipitation treated. Bars and sections. De ≤ 100 mm. Rm ≥ 960 MPa
| Standard number: | BS EN 4318:2025 |
| Pages: | 12 |
| Released: | 2025-12-22 |
| ISBN: | 978 0 539 31975 0 |
| Status: | Standard |
BS EN 4318:2025 - Aerospace Series: Heat-Resisting Alloy X6NiCrTiMoV26-15 (1.4980)
Introducing the BS EN 4318:2025, a cutting-edge standard in the aerospace industry, designed to meet the rigorous demands of modern engineering. This standard specifies the requirements for the heat-resisting alloy X6NiCrTiMoV26-15 (1.4980), a material renowned for its exceptional performance in high-temperature environments. This alloy is consumable electrode remelted, solution treated, and precipitation treated, ensuring superior quality and reliability.
Key Features and Benefits
The BS EN 4318:2025 standard is meticulously crafted to provide aerospace engineers and manufacturers with a comprehensive guide to utilizing this high-performance alloy. Here are some of the standout features and benefits:
- High Heat Resistance: The X6NiCrTiMoV26-15 alloy is engineered to withstand extreme temperatures, making it ideal for aerospace applications where heat resistance is crucial.
- Exceptional Strength: With a minimum tensile strength (Rm) of 960 MPa, this alloy offers remarkable strength, ensuring durability and longevity in demanding conditions.
- Precision Manufacturing: The consumable electrode remelting process enhances the alloy's purity and uniformity, resulting in superior mechanical properties.
- Versatile Applications: Suitable for bars and sections with a diameter (De) of ≤ 100 mm, this standard provides flexibility for various aerospace components.
- Comprehensive Treatment: The solution and precipitation treatments further enhance the alloy's mechanical properties, ensuring optimal performance.
Technical Specifications
The BS EN 4318:2025 standard is a 12-page document, released on December 22, 2025, and is identified by the ISBN 978 0 539 31975 0. It provides detailed guidelines and specifications for the use of the X6NiCrTiMoV26-15 alloy in aerospace applications.
Standard Number
BS EN 4318:2025
Release Date
December 22, 2025
ISBN
978 0 539 31975 0
Status
Standard
Applications in Aerospace Industry
The aerospace industry demands materials that can perform under extreme conditions, and the X6NiCrTiMoV26-15 alloy is engineered to meet these challenges. Its high heat resistance and strength make it an ideal choice for components such as:
- Jet engine parts
- Turbine blades
- Exhaust systems
- Structural components
By adhering to the BS EN 4318:2025 standard, manufacturers can ensure that their products meet the highest quality and performance standards, providing peace of mind and reliability in critical aerospace applications.
Why Choose BS EN 4318:2025?
Choosing the BS EN 4318:2025 standard means investing in a future-proof solution that aligns with the latest advancements in aerospace technology. This standard not only guarantees the quality and performance of the X6NiCrTiMoV26-15 alloy but also supports innovation and excellence in aerospace engineering.
Whether you are designing new aerospace components or upgrading existing systems, the BS EN 4318:2025 standard provides the assurance and guidance needed to achieve optimal results. Embrace the future of aerospace engineering with this state-of-the-art standard and unlock new possibilities for your projects.
BS EN 4318:2025
This standard BS EN 4318:2025 Aerospace series. Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980). Consumable electrode remelted. Solution treated and precipitation treated. Bars and sections. De ≤ 100 mm. Rm ≥ 960 MPa is classified in these ICS categories:
- 49.025.05 Ferrous alloys in general