BS EN 2119:2017
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated. Wires for rivets. 2 mm ≤ D ≤ 10 mm. Rm ≥ 960 MPa
| Standard number: | BS EN 2119:2017 |
| Pages: | 12 |
| Released: | 2018-01-05 |
| ISBN: | 978 0 580 98674 1 |
| Status: | Standard |
BS EN 2119:2017
This standard BS EN 2119:2017 Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated. Wires for rivets. 2 mm ≤ D ≤ 10 mm. Rm ≥ 960 MPa is classified in these ICS categories:
- 49.025.05 Ferrous alloys in general
BS EN 2119:2017 Aerospace Series - Heat Resisting Alloy FE-PA2601
Introducing the BS EN 2119:2017, a pivotal standard in the aerospace industry, specifically designed for heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). This standard is essential for professionals seeking high-performance materials for demanding aerospace applications. The alloy is solution treated and precipitation treated, ensuring optimal performance in extreme conditions.
Key Features and Specifications
The BS EN 2119:2017 standard encompasses wires for rivets with diameters ranging from 2 mm to 10 mm, ensuring versatility for various applications. The material boasts a remarkable tensile strength, with Rm ≥ 960 MPa, making it ideal for high-stress environments.
- Standard Number: BS EN 2119:2017
- Pages: 12
- Release Date: January 5, 2018
- ISBN: 978 0 580 98674 1
- Status: Standard
Why Choose FE-PA2601 Alloy?
The FE-PA2601 alloy is renowned for its exceptional heat resistance, making it a preferred choice in the aerospace sector. Its unique composition, including elements like Nickel, Chromium, Titanium, Molybdenum, and Vanadium, provides superior strength and durability. This makes it suitable for applications where materials are subjected to high temperatures and mechanical stress.
Applications in Aerospace
In the aerospace industry, materials are often exposed to extreme conditions, including high temperatures and pressures. The FE-PA2601 alloy is engineered to withstand these challenges, making it ideal for use in:
- Aircraft engine components
- High-temperature fasteners
- Structural components requiring high strength and heat resistance
Technical Excellence
The BS EN 2119:2017 standard ensures that the FE-PA2601 alloy meets rigorous quality and performance criteria. The solution treatment and precipitation treatment processes enhance the alloy's mechanical properties, ensuring it performs reliably under stress.
Solution Treatment
This process involves heating the alloy to a high temperature and then rapidly cooling it. This treatment dissolves alloying elements into a solid solution, enhancing the material's ductility and toughness.
Precipitation Treatment
Also known as aging, this process involves reheating the alloy to a lower temperature, allowing precipitates to form. These precipitates strengthen the alloy by hindering dislocation movement, thereby increasing its yield strength and hardness.
Compliance and Quality Assurance
Adhering to the BS EN 2119:2017 standard ensures that the FE-PA2601 alloy is manufactured to the highest quality standards. This compliance guarantees that the material is suitable for critical aerospace applications, providing peace of mind to engineers and manufacturers.
Conclusion
The BS EN 2119:2017 standard for the FE-PA2601 heat resisting alloy is an indispensable resource for aerospace professionals. Its comprehensive guidelines ensure that the alloy meets the stringent demands of the industry, providing exceptional performance in high-temperature and high-stress environments. Whether you're designing aircraft components or manufacturing high-performance fasteners, this standard is your assurance of quality and reliability.