BS EN 3510:2019
Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Solution treated and precipitation treated. Bars and sections. De ≤ 100 mm
Standard number: | BS EN 3510:2019 |
Pages: | 12 |
Released: | 2019-10-03 |
ISBN: | 978 0 539 04397 6 |
Status: | Standard |
BS EN 3510:2019 Aerospace Series: Heat Resisting Alloy FE-PA2602 (X4NiCrTiMoV26-15)
Welcome to the world of advanced aerospace materials with the BS EN 3510:2019 standard. This comprehensive document is an essential resource for professionals in the aerospace industry, providing detailed specifications for the heat resisting alloy FE-PA2602, also known by its chemical designation X4NiCrTiMoV26-15. This standard is crucial for those involved in the manufacturing and application of high-performance materials in aerospace engineering.
Key Features of BS EN 3510:2019
- Standard Number: BS EN 3510:2019
- Pages: 12
- Release Date: October 3, 2019
- ISBN: 978 0 539 04397 6
- Status: Standard
About the Alloy: FE-PA2602 (X4NiCrTiMoV26-15)
The FE-PA2602 alloy is a high-performance material specifically designed to withstand extreme temperatures and conditions, making it ideal for aerospace applications. This alloy is solution treated and precipitation treated, ensuring optimal strength and durability. The standard covers bars and sections with a diameter (De) of ≤ 100 mm, providing precise guidelines for manufacturing and quality assurance.
Applications in Aerospace
The aerospace industry demands materials that can endure high stress and temperature variations. The FE-PA2602 alloy is engineered to meet these challenges, offering exceptional heat resistance and mechanical properties. It is commonly used in the production of critical components such as turbine blades, engine parts, and structural elements that require reliable performance under extreme conditions.
Benefits of Using FE-PA2602 Alloy
- Heat Resistance: Capable of maintaining structural integrity at high temperatures.
- Durability: Enhanced strength and toughness through solution and precipitation treatment.
- Versatility: Suitable for a wide range of aerospace applications.
- Precision: Detailed specifications ensure consistent quality and performance.
Why Choose BS EN 3510:2019?
Adhering to the BS EN 3510:2019 standard ensures that your aerospace components are manufactured to the highest quality and safety standards. This document provides a comprehensive framework for the production and testing of the FE-PA2602 alloy, ensuring that your products meet the rigorous demands of the aerospace industry.
Comprehensive Guidelines
The standard offers detailed guidelines on the chemical composition, mechanical properties, and testing methods for the FE-PA2602 alloy. By following these guidelines, manufacturers can ensure that their products are consistent, reliable, and meet the necessary performance criteria.
Quality Assurance
Implementing the BS EN 3510:2019 standard in your manufacturing process provides a robust quality assurance framework. This ensures that every batch of material produced meets the stringent requirements set forth in the standard, reducing the risk of defects and enhancing the overall reliability of your aerospace components.
Conclusion
The BS EN 3510:2019 standard is an indispensable resource for aerospace professionals seeking to utilize the FE-PA2602 heat resisting alloy. With its detailed specifications and comprehensive guidelines, this standard ensures that your products are manufactured to the highest quality and performance standards. Embrace the future of aerospace materials with the BS EN 3510:2019 standard and ensure your components are ready to meet the challenges of tomorrow's aerospace industry.
BS EN 3510:2019
This standard BS EN 3510:2019 Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Solution treated and precipitation treated. Bars and sections. De ≤ 100 mm is classified in these ICS categories:
- 49.025.05 Ferrous alloys in general
This document specifies the requirements relating to:
Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15)
Solution treated and precipitation treated
Bars and sections
De � 100 mm
for aerospace applications.