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
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)