Aircraft And Space Vehicle Engineering Official British Standard

BS EN 2818:2009

Discover BS EN 2818:2009 for aerospace steel compliance, ensuring high performance and safety in aircraft and space vehicle engineering.

Overview

BS EN 2818:2009 is a crucial standard within the aerospace sector, specifically addressing the requirements for steel FE-PM1802 (X5CrNiCu15-5). This standard outlines the specifications for consumable electrode remelted steel that has undergone solution treatment and precipitation treatment. The focus is on forgings with a diameter of less than or equal to 200 mm and a minimum tensile strength (Rm) of 1070 MPa. This standard is essential for ensuring the integrity and performance of components used in aircraft and space vehicle engineering.

Key Requirements

  • Material Specification: The standard specifies the chemical composition and mechanical properties of steel FE-PM1802, ensuring it meets the rigorous demands of aerospace applications.
  • Manufacturing Process: It details the consumable electrode remelting process, which enhances the material's properties through controlled solidification.
  • Treatment Processes: The standard mandates solution treatment and precipitation treatment to improve strength and ductility.
  • Dimensional Limits: Forgings must have a diameter not exceeding 200 mm, ensuring suitability for various aerospace components.
  • Tensile Strength: A minimum tensile strength of 1070 MPa is required, which is critical for the structural integrity of aerospace components.

Implementation Benefits

Adopting BS EN 2818:2009 offers several practical benefits for manufacturers and compliance professionals:

  • Enhanced Material Performance: The specified treatments and processes lead to superior mechanical properties, ensuring that components can withstand the extreme conditions encountered in aerospace applications.
  • Standardisation: Compliance with this standard facilitates consistency in manufacturing processes, which is vital for quality assurance in aerospace engineering.
  • Risk Mitigation: By adhering to the standard, manufacturers can reduce the risk of material failure, thereby enhancing safety and reliability in aircraft and space vehicles.
  • Market Acceptance: Compliance with BS EN 2818:2009 is often a prerequisite for acceptance in the aerospace industry, making it easier for manufacturers to enter or compete in the market.

Compliance Value

Compliance with BS EN 2818:2009 not only meets regulatory requirements but also demonstrates a commitment to quality and safety in aerospace engineering. This standard is recognised across Europe and serves as a benchmark for material performance in the aerospace sector. By following the guidelines set forth in this standard, organisations can ensure that their products meet the necessary safety and performance criteria, ultimately contributing to the overall success of aerospace projects.

In conclusion, BS EN 2818:2009 is a vital standard for manufacturers involved in the production of aerospace components. Its comprehensive requirements for material properties, manufacturing processes, and treatment protocols ensure that products are not only compliant but also capable of performing under the demanding conditions of flight. Adhering to this standard is essential for maintaining the integrity and safety of aircraft and space vehicles.

Technical Information

Aircraft And Space Vehicle Engineering
BSI Group
978 0 580 68928 4
Specification Details
  • Aerospace series
  • Steel FE-PM1802 (X5CrNiCu15-5)
  • Consumable electrode remelted
  • Solution treated and precipitation treated
  • Forgings
  • a or D ≤ 200 mm
  • Rm ≥ 1070 MPa
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