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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.030 Fasteners for aerospace construction>49.030.20 Bolts, screws, studs>BS EN 3308:1996 Screws, normal hexagonal head, threaded to head, in titanium alloy, anodized, MoS<sub>2</sub> lubricated. Classification. 1100 MPa (at ambient temperature) /315°C
immediate downloadReleased: 1996-12-15
BS EN 3308:1996 Screws, normal hexagonal head, threaded to head, in titanium alloy, anodized, MoS<sub>2</sub> lubricated. Classification. 1100 MPa (at ambient temperature) /315°C

BS EN 3308:1996

Screws, normal hexagonal head, threaded to head, in titanium alloy, anodized, MoS<sub>2</sub> lubricated. Classification. 1100 MPa (at ambient temperature) /315°C

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Standard number:BS EN 3308:1996
Pages:12
Released:1996-12-15
ISBN:0 580 26607 9
Status:Standard
BS EN 3308:1996 Titanium Alloy Screws

BS EN 3308:1996 Titanium Alloy Screws

Introducing the BS EN 3308:1996 standard for screws, a comprehensive classification that sets the benchmark for high-performance fasteners. These screws are designed with a normal hexagonal head and are threaded to the head, crafted from premium titanium alloy. They are anodized and lubricated with MoS2 to ensure optimal performance and durability.

Unmatched Strength and Durability

These screws are engineered to withstand extreme conditions, offering a tensile strength of 1100 MPa at ambient temperature. They are also capable of maintaining their integrity at elevated temperatures up to 315°C. This makes them ideal for applications where both strength and heat resistance are critical.

Key Features

  • Material: Titanium Alloy
  • Head Type: Normal Hexagonal
  • Threading: Threaded to Head
  • Surface Treatment: Anodized
  • Lubrication: MoS2 (Molybdenum Disulfide)
  • Tensile Strength: 1100 MPa at ambient temperature
  • Temperature Resistance: Up to 315°C

Why Choose BS EN 3308:1996 Screws?

These screws are not just about meeting standards; they are about exceeding expectations. The use of titanium alloy ensures that they are lightweight yet incredibly strong, making them perfect for aerospace, automotive, and industrial applications where weight and strength are crucial factors.

The anodized finish provides an additional layer of protection against corrosion, enhancing the longevity of the screws even in harsh environments. The MoS2 lubrication reduces friction, ensuring smooth installation and removal, which is particularly beneficial in applications requiring frequent maintenance.

Applications

The BS EN 3308:1996 screws are versatile and can be used in a wide range of applications, including:

  • Aerospace: Ideal for aircraft construction and maintenance due to their high strength-to-weight ratio and temperature resistance.
  • Automotive: Perfect for high-performance vehicles where durability and weight reduction are essential.
  • Industrial Machinery: Suitable for machinery that operates under high stress and temperature conditions.
  • Marine: Excellent for use in marine environments due to their corrosion resistance.

Technical Specifications

For those who require detailed technical information, the BS EN 3308:1996 standard is documented over 12 pages, providing comprehensive guidelines and specifications. Released on December 15, 1996, this standard is a testament to the enduring quality and reliability of these screws.

Standard Number: BS EN 3308:1996

Pages: 12

Released: 1996-12-15

ISBN: 0 580 26607 9

Status: Standard

Conclusion

When it comes to choosing screws that offer unparalleled strength, durability, and performance, the BS EN 3308:1996 titanium alloy screws stand out as the superior choice. Whether you are in the aerospace, automotive, industrial, or marine sector, these screws provide the reliability and efficiency you need to ensure the success of your projects.

Invest in quality and performance with BS EN 3308:1996 screws, and experience the difference that precision engineering and superior materials can make.

DESCRIPTION

BS EN 3308:1996


This standard BS EN 3308:1996 Screws, normal hexagonal head, threaded to head, in titanium alloy, anodized, MoS2 lubricated. Classification. 1100 MPa (at ambient temperature) /315°C is classified in these ICS categories:
  • 49.030.20 Bolts, screws, studs