Aircraft And Space Vehicle Engineering Official British Standard

BS 2HC 208:1989

Discover compliance benefits and practical applications of BS 2HC 208:1989 for nickel-cobalt-tungsten alloy castings in aerospace engineering.

Overview

BS 2HC 208:1989 provides a comprehensive specification for nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings. This standard is particularly relevant in the fields of aircraft and space vehicle engineering, where high-performance materials are essential for ensuring safety and reliability. The alloy composition includes nickel base (Co 10.0, W 10.0, Cr 9.0, Al 5.5, Mo 2.5, Ti 1.5, Ta 1.5), which is engineered to meet the rigorous demands of aerospace applications.

Key Requirements

The standard outlines specific requirements for the production and testing of these alloy castings. Key aspects include:

  • Material Composition: The precise percentages of each element must be adhered to, ensuring the desired mechanical properties and corrosion resistance.
  • Manufacturing Processes: Guidelines for casting methods, including the necessary controls to maintain quality and integrity throughout production.
  • Testing Procedures: Detailed protocols for mechanical testing, including tensile strength, ductility, and impact resistance, to validate material performance.
  • Documentation: Requirements for traceability and documentation to ensure compliance throughout the supply chain.

Implementation Benefits

Adhering to BS 2HC 208:1989 provides several practical benefits for manufacturers and engineers:

  • Enhanced Performance: The specified alloy composition offers superior mechanical properties, making it suitable for critical aerospace components.
  • Improved Safety: Compliance with this standard helps mitigate risks associated with material failure in high-stress environments.
  • Quality Assurance: Implementing the standard facilitates consistent quality control measures, ensuring that products meet industry expectations.
  • Market Competitiveness: Companies that comply with recognised standards can enhance their market position by demonstrating commitment to quality and safety.

Compliance Value

Compliance with BS 2HC 208:1989 is not just a regulatory requirement but a strategic advantage. It ensures that manufacturers are aligned with best practices in the aerospace sector, which is governed by stringent safety and performance regulations. By adhering to this standard, organisations can:

  • Meet Regulatory Requirements: Fulfil obligations set by aviation authorities and industry bodies.
  • Reduce Liability: Lower the risk of product recalls and liability claims associated with material failures.
  • Facilitate International Trade: Ensure that products meet international standards, aiding in export opportunities.

In conclusion, BS 2HC 208:1989 serves as a critical framework for the production of nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings. Its implementation not only enhances product quality and safety but also provides a competitive edge in the aerospace industry.

Technical Information

Aircraft And Space Vehicle Engineering
BSI Group
0 580 17575 8
Specification Details
  • Specification for nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings (nickel base Co 10
  • 0, W 10
  • 0, Cr 9
  • 0, Al 5
  • 5, Mo 2
  • 5, Ti 1
  • 5, Ta 1
  • 5)
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