BS EN 3293:2008
Aerospace series. Bolts, T-head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated. Classification: 1275 MPa/650°C
| Standard number: | BS EN 3293:2008 |
| Pages: | 12 |
| Released: | 2008-04-30 |
| ISBN: | 978 0 580 60319 8 |
| Status: | Standard |
BS EN 3293:2008 Aerospace Series Bolts
Introducing the BS EN 3293:2008 Aerospace Series Bolts, a pinnacle of engineering excellence designed to meet the rigorous demands of the aerospace industry. These bolts are crafted with precision and durability in mind, ensuring they perform exceptionally in the most challenging environments.
Product Overview
The BS EN 3293:2008 standard specifies the requirements for T-head bolts with close tolerance and medium thread length, made from a heat-resisting nickel base alloy known as NI-P100HT (Inconel 718). These bolts are uncoated, providing a raw and robust solution for aerospace applications. With a classification of 1275 MPa/650°C, they are engineered to withstand high stress and temperature conditions, making them ideal for critical aerospace applications.
Key Features
- Material: Heat-resisting nickel base alloy NI-P100HT (Inconel 718)
- Design: T-head, close tolerance, medium thread length
- Classification: 1275 MPa/650°C
- Coating: Uncoated for raw durability
Technical Specifications
| Standard Number | BS EN 3293:2008 |
|---|---|
| Pages | 12 |
| Release Date | April 30, 2008 |
| ISBN | 978 0 580 60319 8 |
| Status | Standard |
Material Excellence: Inconel 718
Inconel 718, the material used in these bolts, is a high-strength, corrosion-resistant nickel chromium material used at temperatures ranging from -423° to 1300°F. It is composed of 50-55% nickel, 17-21% chromium, 4.75-5.5% niobium, and 2.8-3.3% molybdenum, among other elements. This composition provides exceptional resistance to oxidation and corrosion, making it a preferred choice in the aerospace industry.
Applications
The BS EN 3293:2008 bolts are specifically designed for aerospace applications where reliability and performance are paramount. They are suitable for use in:
- Aircraft engines
- Gas turbines
- Rocket motors
- High-temperature fastener applications
Performance Under Pressure
These bolts are engineered to perform under extreme conditions. With a classification of 1275 MPa/650°C, they can withstand high stress and temperature environments, ensuring safety and reliability in critical aerospace applications. The close tolerance design ensures a precise fit, reducing the risk of mechanical failure.
Uncoated for Versatility
The uncoated finish of these bolts provides versatility in application. While coatings can offer additional protection, the uncoated design allows for direct use in environments where additional coatings may not be necessary or could interfere with the bolt's performance.
Compliance and Standards
The BS EN 3293:2008 standard ensures that these bolts meet the stringent requirements of the aerospace industry. Compliance with this standard guarantees that the bolts are manufactured to the highest quality, providing peace of mind to engineers and manufacturers alike.
Conclusion
In summary, the BS EN 3293:2008 Aerospace Series Bolts are a superior choice for aerospace applications requiring high strength, durability, and resistance to extreme conditions. Their design and material composition make them an indispensable component in the aerospace industry, ensuring safety and performance in every application.
BS EN 3293:2008
This standard BS EN 3293:2008 Aerospace series. Bolts, T-head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated. Classification: 1275 MPa/650°C is classified in these ICS categories:
- 49.030.20 Bolts, screws, studs