Aircraft And Space Vehicle Engineering Official British Standard

BS 2HR 10:2010

Ensure compliance with BS 2HR 10:2010 for high-performance nickel-based alloys in aerospace applications, enhancing safety and reliability.

Overview

BS 2HR 10:2010 is a critical standard in the field of aircraft and space vehicle engineering, focusing on the specification of nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings, and parts. This standard is essential for manufacturers and engineers involved in the production and application of high-performance materials in aerospace applications.

Key Requirements

The standard outlines the specific chemical composition and mechanical properties required for the nickel-based alloy, which includes:

  • Nickel Base: The primary component ensuring excellent corrosion resistance and high-temperature performance.
  • Cobalt (Co 20%): Enhances strength and stability at elevated temperatures.
  • Chromium (Cr 20%): Provides oxidation resistance and contributes to the alloy's overall durability.
  • Molybdenum (Mo 5.9%): Improves strength and resistance to pitting corrosion.
  • Titanium (Ti 2.1%): Aids in the alloy's strength and heat resistance.
  • Aluminium (Al 0.5%): Enhances oxidation resistance and contributes to the alloy's lightweight properties.

In addition to chemical composition, BS 2HR 10:2010 specifies mechanical property requirements, including tensile strength, yield strength, and elongation, ensuring that the materials meet the rigorous demands of aerospace applications.

Implementation Benefits

Adhering to BS 2HR 10:2010 provides several benefits for manufacturers and engineers:

  • Quality Assurance: Compliance with this standard ensures that materials meet stringent quality and performance criteria, reducing the risk of failure in critical applications.
  • Enhanced Performance: The specified alloy composition is designed for high-temperature applications, making it suitable for components exposed to extreme conditions.
  • Streamlined Production: Following a recognised standard simplifies the manufacturing process, as it provides clear guidelines for material selection and processing techniques.

By implementing the specifications outlined in BS 2HR 10:2010, organisations can enhance their production processes and ensure the reliability of their aerospace components.

Compliance Value

Compliance with BS 2HR 10:2010 is not only a matter of meeting industry standards but also a critical factor in ensuring safety and reliability in aerospace applications. The aerospace industry is governed by strict regulations, and adherence to recognised standards is essential for:

  • Regulatory Compliance: Meeting national and international regulations helps organisations avoid legal penalties and ensures market access.
  • Risk Management: Using materials that comply with established standards mitigates the risk of material failure, which can have catastrophic consequences in aerospace operations.
  • Market Competitiveness: Demonstrating compliance with BS 2HR 10:2010 can enhance an organisation's reputation and competitiveness in the aerospace sector.

In summary, BS 2HR 10:2010 serves as a vital reference for the aerospace industry, ensuring that nickel-cobalt-chromium-molybdenum-titanium-aluminium alloys are produced to the highest standards of quality and performance.

Technical Information

Aircraft And Space Vehicle Engineering
BSI Group
978 0 580 67045 9
Specification Details
  • Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5
  • 9, Ti 2
  • 1, Al 0
  • 5)
Official BSI Standard
Instant PDF Download
Industry Recognised

Purchase This Standard

Official Price
£158.00

Purchase the official standard directly from BSI Group. You'll be redirected to the official BSI website to complete your purchase.

Buy from BSI Group
Official BSI Standard
Instant PDF Download
Secure Payment