EN 2821:2024
(Main)Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Bars for machining - a or D ≤ 200 mm - Rm ≥ 1 310 MPa
Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Bars for machining - a or D ≤ 200 mm - Rm ≥ 1 310 MPa
This document specifies the requirements relating to:
Steel X5CrNiCu15-5 (1.4545)
Consumable electrode remelted
Solution treated and precipitation treated
Bars for machining
a or D ≤ 200 mm
Rm ≥ 1 310 MPa
for aerospace applications.
Luft- und Raumfahrt - Stahl X5CrNiCu15-5 (1.4545) - Mit selbstverzehrender Elektrode umgeschmolzen - Lösungsgeglüht und ausscheidungsgehärtet - Stangen zur spanenden Bearbeitung - a oder D ≤ 200 mm - Rm ≥ 1 310 MPa
No Scope available
Série aérospatiale - Acier X5CrNiCu15-5 (1.4545) - Refondu à l'électrode consommable - Mis en solution et précipité - Barres pour usinage - a ou D ≤ 200 mm - Rm ≥ 1 310 MPa
Le présent document spécifie les exigences relatives à :
Acier X5CrNiCu15 5 (1.4545)
Refondu à l'électrode consommable
Mis en solution et précipité
Barres pour usinage
a ou D ≤ 200 mm
Rm ≥ 1 310 MPa
pour les applications aérospatiales.
Aeronavtika - Jeklo X5CrNiCu15 5 (1.4545) - Pretaljeno s talilno elektrodo - Žarjeno v topilu in utrjeno - Palice za obdelavo - a ali D ≤ 200 mm - Rm ≥ 1310 MPa
Ta dokument določa zahteve, ki se navezujejo na:
jeklo X5CrNiCu15 5 (1.4545),
pretaljeno s taljivo elektrodo,
žarjeno v topilu in utrjeno,
palice za obdelavo,
a ali D ≤ 200 mm,
Rm ≥ 1310 MPa,
za uporabo v aeronavtiki.
General Information
- Status
- Published
- Publication Date
- 13-Aug-2024
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 4/S 3 - Steels & Heat Resisting Alloys
- Current Stage
- 6060 - Definitive text made available (DAV) - Publishing
- Start Date
- 14-Aug-2024
- Completion Date
- 14-Aug-2024
Relations
- Effective Date
- 19-Jan-2023
Overview
EN 2821:2024 is a European standard developed by CEN that specifies stringent requirements for the aerospace-grade steel grade X5CrNiCu15-5 (1.4545). This steel is produced by a consumable electrode remelting process, then subjected to solution treatment and precipitation treatment to meet the mechanical properties necessary for aerospace applications. The standard covers machining bars with a diameter or cross-section of up to 200 mm and a minimum tensile strength (Rm) of 1,310 MPa.
The standard is part of the EN aerospace metal material series and aligns with general aerospace material guidelines to ensure high-quality, high-performance steel products for safety-critical aerospace components.
Key Topics
- Material Specification: Steel grade X5CrNiCu15-5 (1.4545), known for corrosion resistance, high strength, and toughness.
- Manufacturing Process: Consumable electrode remelting to enhance purity and minimize defects.
- Heat Treatments:
- Solution Treatment: Performed at 1,025 – 1,055 °C for at least 30 minutes, followed by rapid cooling.
- Precipitation Treatment: Conducted between 465 – 495 °C for at least 1 hour, enhancing strength and durability.
- Form and Dimensions: Bars designed for machining with diameter or cross-section (a or D) ≤ 200 mm.
- Mechanical Properties:
- Minimum tensile strength (Rm) ≥ 1,310 MPa.
- Proof stress (Rp0.2) ≥ 1,170 MPa.
- Elongation and reduction in area meet aerospace safety factors.
- Hardness values controlled between HB 388–444 or 40–47 HRC.
- Inspection and Testing:
- Microstructural analysis ensuring δ ferrite content ≤ 2%.
- Ultrasonic and visual testing to detect internal and surface defects.
- Compliance with EN 4700-002 technical specifications.
- Quality Assurance: Product qualification as per EN 2043, including traceability, marking, and dimensional inspections.
Applications
EN 2821:2024 steel bars are critical for aerospace structural components requiring:
- High strength-to-weight ratio materials.
- Superior corrosion resistance for long lifecycle in harsh environments.
- Reliability under cyclic loading and extreme temperature variations.
- Precision machining to tight tolerances for complex aerospace parts.
- Use in components such as turbine shafts, fasteners, and critical load-bearing parts in aircraft and aerospace vehicles.
This standard enables manufacturers and aerospace engineers to select and procure consistent, certified steel bars that meet the demanding conditions of aerospace engineering, improving safety and performance of aerospace hardware.
Related Standards
EN 2821:2024 integrates closely with other aerospace and metallic material standards:
- EN 4700-002 - Technical specifications for steel and heat-resisting alloy bars and sections.
- EN 2043 - General requirements for semi-finished aerospace metallic products qualification.
- EN 2951 - Micrographic determination of non-metallic inclusion content in aerospace steels.
- EN 4050-4 - Ultrasonic inspection criteria for aerospace bars and forgings.
- EN 4436 - Testing for δ ferrite content in steel.
- EN 4258 - Overall organization and classification of aerospace metallic material standards.
- EN 4500-005 - Rules for drafting and presentation of aerospace steel material standards.
By adhering to EN 2821:2024 and these associated standards, organizations ensure compliance with aerospace industry best practices, enabling international acceptance and interoperability.
Keywords: EN 2821:2024, aerospace steel standard, X5CrNiCu15-5, consumable electrode remelted steel, precipitation treated steel, solution treated steel, aerospace machining bars, high tensile steel bars, mechanical properties aerospace steel, steel bars for aerospace applications, CEN aerospace standards.
Frequently Asked Questions
EN 2821:2024 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Bars for machining - a or D ≤ 200 mm - Rm ≥ 1 310 MPa". This standard covers: This document specifies the requirements relating to: Steel X5CrNiCu15-5 (1.4545) Consumable electrode remelted Solution treated and precipitation treated Bars for machining a or D ≤ 200 mm Rm ≥ 1 310 MPa for aerospace applications.
This document specifies the requirements relating to: Steel X5CrNiCu15-5 (1.4545) Consumable electrode remelted Solution treated and precipitation treated Bars for machining a or D ≤ 200 mm Rm ≥ 1 310 MPa for aerospace applications.
EN 2821:2024 is classified under the following ICS (International Classification for Standards) categories: 49.025.10 - Steels. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 2821:2024 has the following relationships with other standards: It is inter standard links to EN 2821:2007. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
You can purchase EN 2821:2024 directly from iTeh Standards. The document is available in PDF format and is delivered instantly after payment. Add the standard to your cart and complete the secure checkout process. iTeh Standards is an authorized distributor of CEN standards.
Standards Content (Sample)
SLOVENSKI STANDARD
01-oktober-2024
Aeronavtika - Jeklo X5CrNiCu15 5 (1.4545) - Pretaljeno s talilno elektrodo - Žarjeno
v topilu in utrjeno - Palice za obdelavo - a ali D ≤ 200 mm - Rm ≥ 1310 MPa
Aerospace series - Steel X5CrNiCu15 5 (1.4545) - Consumable electrode remelted -
Solution treated and precipitation treated - Bars for machining - a or D ≤ 200 mm - Rm ≥
1 310 MPa
Luft- und Raumfahrt - Stahl X5CrNiCu15 5 (1.4545) - Mit selbstverzehrender Elektrode
umgeschmolzen - Lösungsgeglüht und ausscheidungsgehärtet - Stangen zur spanenden
Bearbeitung - a oder D ≤ 200 mm - Rm ≥ 1 310 MPa
Série aérospatiale - Acier X5CrNiCu15 5 (1.4545) - Refondu à l'électrode consommable
- Mis en solution et vieilli - Barres pour usinage - a ou D ≤ 200 mm - Rm ≥ 1 310 MPa
Ta slovenski standard je istoveten z: EN 2821:2024
ICS:
49.025.10 Jekla Steels
77.140.60 Jeklene palice in drogovi Steel bars and rods
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EN 2821
EUROPEAN STANDARD
NORME EUROPÉENNE
August 2024
EUROPÄISCHE NORM
ICS 49.025.10 Supersedes EN 2821:2007
English Version
Aerospace series - Steel X5CrNiCu15-5 (1.4545) -
Consumable electrode remelted - Solution treated and
precipitation treated - Bars for machining - a or D 200
mm - Rm 1 310 MPa
Série aérospatiale - Acier X5CrNiCu15-5 (1.4545) - Luft- und Raumfahrt - Stahl X5CrNiCu15-5 (1.4545) -
Refondu à l'électrode consommable - Mis en solution et Mit selbstverzehrender Elektrode umgeschmolzen -
précipité - Barres pour usinage - a ou D 200 mm - Rm Lösungsgeglüht und ausscheidungsgehärtet - Stangen
zur spanenden Bearbeitung - a oder D 200 mm - Rm
1 310 MPa
1 310 MPa
This European Standard was approved by CEN on 26 May 2024.
CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this
European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references
concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN
member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by
translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management
Centre has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia,
Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway,
Poland, Portugal, Republic of North Macedonia, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Türkiye and
United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2024 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2821:2024 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
Introduction . 4
1 Scope . 5
2 Normative references . 5
3 Terms and definitions . 5
4 Requirements . 5
Bibliography . 6
European foreword
This document (EN 2821:2024) has been prepared by ASD-STAN.
After enquiries and votes carried out in accordance with the rules of this Association, this document has
received the approval of the National Associations and the Official Services of the member countries of
ASD-STAN, prior to its presentation to CEN.
This document shall be given the status of a national standard, either by publication of an identical text
or by endorsement, at the latest by February 2025, and conflicting national standards shall be
withdrawn at the latest by February 2025.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. CEN shall not be held responsible for identifying any or all such patent rights.
This document supersedes EN 2821:2007.
The main changes with respect to the previous edition are as follows:
— EN 2821 (P3), 03/2007 — Overall editorial improvements and correction of the French title.
According to the CEN-CENELEC Internal Regulations, the national standards organizations of the
following countries are bound to implement this document: Austria, Belgium, Bulgaria, Croatia, Cyprus,
Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland,
...
La norme EN 2821:2024 fournit des spécifications claires et précises concernant l'acier X5CrNiCu15-5 (1.4545) destiné aux applications aérospatiales. Ce document s'articule autour de plusieurs exigences fondamentales, notamment celles relatives aux électrodes consommables remélangées ainsi qu'aux traitements de solution et de précipitation. La portée de la norme est particulièrement bien définie, car elle s'applique spécifiquement aux barres destinées à l'usinage dont le diamètre (a ou D) est inférieur ou égal à 200 mm, avec une résistance à la traction (Rm) d'au moins 1 310 MPa. Parmi les points forts de la norme, on peut souligner sa clairvoyance dans la définition des exigences techniques pour l'acier inoxydable utilisé dans les environnements critiques de l'aéronautique. Le choix de l'acier X5CrNiCu15-5 (1.4545) est judicieux, car il combine des propriétés mécaniques élevées avec une résistance à la corrosion accrue, ce qui est essentiel pour la longévité des composants aérospatiaux. De plus, le traitement de solution et la précipitation garantissent des caractéristiques mécaniques optimales adaptées aux exigences strictes du secteur. La norme EN 2821:2024 est d'une grande pertinence dans le contexte actuel, où les besoins en matériaux sophistiqués pour l'industrie aéronautique ne cessent de croître. En établissant des directives claires pour la production et l'utilisation des barres pour usinage, elle contribue non seulement à la sécurité aérienne mais aussi à l'efficacité des processus de fabrication. Sa capacité à standardiser les spécifications pour un matériau crucial fait d'elle un outil essentiel pour les ingénieurs et les fabricants de l'industrie aérospatiale.
標準EN 2821:2024は、航空宇宙産業における特定の鋼材仕様について詳細に定義しています。この標準は、X5CrNiCu15-5(1.4545)という鋼材の要件を明確化し、消耗電極の再溶融、溶液処理および析出処理が施されたバーに関する基準を提供しています。特に、この基準では、加工用のバーの直径または長さが200 mm以下であり、引張強度(Rm)が1,310 MPa以上であることが求められています。 この標準の強みは、特定の航空宇宙用途における要求を正確に満たすために設計されている点です。選定された鋼材は、耐食性や耐久性が高く、厳しい航空基準に対応できる特性を持っています。また、消耗電極の再溶融というプロセスによって、均一な品質と性能が確保され、航空機部品の製造において信頼性が高いものとなっています。 さらに、EN 2821:2024は、航空宇宙分野での標準化の重要性を反映しており、関連する産業全体での一貫性と互換性を促進するために役立つ標準として位置付けられています。この文書は、航空宇宙産業が要求する高度な技術基準を満たすための重要な指針を提供しており、業界内の企業にとって有用なリソースとなるでしょう。
EN 2821:2024 표준은 항공 우주 분야에서 사용되는 강철 X5CrNiCu15-5 (1.4545)에 대한 요구사항을 명확히 제시합니다. 이 표준은 소비성 전극 재용융, 용액 처리 및 강유리 처리된 바의 기술적 사양을 포함하고 있으며, 기계 가공을 위한 바의 직경(a 또는 D)이 200 mm 이하이고 항복 힘(Rm)이 1,310 MPa 이상일 때 적용됩니다. 이 표준의 강점 중 하나는 항공 우주 응용을 위한 재료의 일관성과 신뢰성을 보장한다는 점입니다. X5CrNiCu15-5 강철은 내식성과 내열성에서 뛰어난 특성을 발휘하여 극한 환경에서도 안정성을 유지할 수 있습니다. 더욱이, 이 표준은 강철 바의 기계적 성질과 제조 공정에 대한 명확한 지침을 제공하여 제조업체들과 엔지니어들이 요구사항을 충족하는 제품을 생산할 수 있도록 합니다. 이는 항공기 및 우주선과 같은 고도로 전문화된 산업에서 반드시 필요한 품질 보증을 가능하게 합니다. 또한, EN 2821:2024는 항공 우주 산업의 품질 기준을 충족하는 데 있어 매우 중요한 참조 문서로서, 이 표준을 준수하는 제품은 국제적으로 인정받는 신뢰성을 제공합니다. 이는 제조 과정의 효율성을 높이고, 품질 문제를 최소화하며, 고객의 요구에 부합하는 솔루션을 제공합니다. 따라서 이 표준은 항공 우주 분야의 생산성과 안전성을 강화하는 데 필수적인 역할을 합니다.
The EN 2821:2024 standard presents a comprehensive framework for the utilization of Steel X5CrNiCu15-5 (1.4545) in aerospace applications, specifically targeting consumable electrode remelted bars that are solution treated and precipitation treated. This standard is critical for ensuring that components manufactured from this steel meet stringent requirements necessary for the aerospace industry, particularly those concerning material strength and durability. One of the notable strengths of EN 2821:2024 is its detailed specification regarding the mechanical properties of the steel, with a minimum tensile strength (Rm) of 1 310 MPa, which underscores the material's capability to withstand high-stress environments. This high level of performance is vital for ensuring the safety and reliability of aerospace components, making the standard relevant for manufacturers focused on producing high-quality, high-performance materials. The focus on bars for machining, with specified dimensions (a or D ≤ 200 mm), also emphasizes the standard's applicability in practical manufacturing scenarios. This precision in dimensional regulation allows for greater uniformity and predictability in machining processes, ultimately contributing to the overall efficiency and effectiveness of aerospace production. Furthermore, the inclusion of requirements for both solution treatment and precipitation treatment means that this standard not only addresses initial material properties but also the heat treatment processes necessary to enhance the mechanical performance of Steel X5CrNiCu15-5. This dual focus on material characteristics and processing establishes EN 2821:2024 as a pivotal reference point for engineering and manufacturing in the aerospace sector. Overall, the EN 2821:2024 standard embodies key characteristics essential for the aerospace industry, ensuring that materials meet rigorous performance expectations while also providing a practical guide for manufacturing processes. Its specificity in mechanical properties and treatment methods makes it a vital tool for stakeholders involved in aerospace engineering and materials development.
Die Norm EN 2821:2024 bietet eine umfassende Spezifikation für den Einsatz des Stahls X5CrNiCu15-5 (1.4545) in der Luft- und Raumfahrtindustrie. Diese Norm fokussiert sich auf Verbrauchselektroden, die remeltet, lösungsbehandelt und altersbehandelt wurden. Sie behandelt spezifische Anforderungen für Stangen, die für die Bearbeitung vorgesehen sind, und stellt sicher, dass die Dimensionen a oder D ≤ 200 mm eingehalten werden und die Zugfestigkeit Rm ≥ 1 310 MPa erreicht wird. Eine der größten Stärken dieser Norm ist ihre Detailgenauigkeit, die es ermöglicht, dass die spezifischen Eigenschaften und Anforderungen des Werkstoffs X5CrNiCu15-5 (1.4545) für verschiedene Anwendungen in der Luft- und Raumfahrt präzise eingehalten werden. Dies unterstützt nicht nur die Gewährleistung der Qualität und Sicherheit in der Luftfahrt, sondern erhöht ebenfalls die Effizienz in der Bearbeitung und im fertigungstechnischen Prozess. Darüber hinaus ist die Relevanz der Norm EN 2821:2024 unbestritten, da sie den steigenden Anforderungen an Materialstandards in der Luft- und Raumfahrt gerecht wird. Die klare Definition der Materialeigenschaften und -verarbeitungsmethoden trägt maßgeblich dazu bei, die Leistungsfähigkeit und Zuverlässigkeit von Komponenten in einem hochspezialisierten und sicherheitskritischen Bereich zu gewährleisten. Insgesamt stellt die EN 2821:2024 eine wichtige Grundlage für den Einsatz von X5CrNiCu15-5 (1.4545) in der Luft- und Raumfahrt dar und unterstreicht die Notwendigkeit hochwertiger Materialien und optimierter Herstellungsprozesse, um den hohen Standards der Branche gerecht zu werden.










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