Aircraft And Space Vehicle Engineering Official British Standard

BS 4S 28:1964+A3:2015

Ensure compliance with BS 4S 28:1964 for high-performance nickel-chromium-molybdenum steel in aerospace applications, enhancing safety and reliability.

Overview

BS 4S 28:1964+A3:2015 specifies the requirements for 4 per cent nickel-chromium-molybdenum steel, which is known for its air hardening properties. This standard is crucial for applications in aircraft and space vehicle engineering, where material performance and reliability are paramount. The steel specified in this standard is characterised by a limiting ruling section of 63.5 mm and a tensile strength of 1545 MPa, making it suitable for high-stress environments.

Key Requirements

The standard outlines several key requirements that must be met for compliance. These include:

  • Material Composition: The steel must contain 4 per cent nickel, chromium, and molybdenum, ensuring optimal mechanical properties.
  • Tensile Strength: The material must achieve a minimum tensile strength of 1545 MPa.
  • Heat Treatment: Specific heat treatment processes are prescribed to achieve the desired hardness and toughness.
  • Testing Procedures: Rigorous testing methods must be employed to verify compliance with the standard's requirements.

Implementation Benefits

Adhering to BS 4S 28:1964+A3:2015 provides several practical benefits for manufacturers and engineers:

  • Enhanced Performance: The specified steel offers superior strength and durability, making it ideal for critical components in aerospace applications.
  • Consistency: Compliance with this standard ensures uniformity in material properties, which is essential for safety and performance in aerospace engineering.
  • Quality Assurance: Following the guidelines set forth in this standard helps manufacturers maintain high-quality production processes.
  • Regulatory Compliance: Meeting the requirements of this standard aids in compliance with broader aerospace regulations and standards.

Compliance Value

Compliance with BS 4S 28:1964+A3:2015 is not only a matter of meeting technical specifications but also a strategic advantage in the aerospace industry. By adhering to this standard, organisations can:

  • Reduce Risk: The use of compliant materials mitigates the risk of failure in critical applications, enhancing safety for both operators and passengers.
  • Improve Marketability: Products that meet recognised standards are more likely to be accepted in the competitive aerospace market.
  • Facilitate International Trade: Compliance with British Standards can ease entry into international markets where adherence to recognised standards is a prerequisite.

In conclusion, BS 4S 28:1964+A3:2015 provides essential guidelines for the use of 4 per cent nickel-chromium-molybdenum steel in aerospace applications. By ensuring compliance with this standard, manufacturers can enhance product performance, ensure safety, and maintain a competitive edge in the industry.

Technical Information

Aircraft And Space Vehicle Engineering
BSI Group
978 0 580 88225 8
Specification Details
  • Specification for 4 per cent nickel-chromium-molybdenum steel (Air hardening)
  • (1545 MPa: limiting ruling section 63
  • 5mm)
Official BSI Standard
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