EN 4500-002:2024
(Main)Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 002: Specific rules for aluminium, aluminium alloys and magnesium alloys
Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 002: Specific rules for aluminium, aluminium alloys and magnesium alloys
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications.
This Part 002 specifies the "Specific rules for aluminium, aluminium alloys and magnesium alloys".
Luft- und Raumfahrt - Metallische Werkstoffe - Regeln für das Erstellen und die Gestaltung von Werkstoffnormen - Teil 002: Besondere Regeln für Aluminium, Aluminiumlegierungen und Magnesiumlegierungen
Die Reihe EN 4500 legt die Regeln für das Erstellen und die Gestaltung von Normen für metallische Werkstoffe für Anwendungen in der Luft- und Raumfahrt fest.
Dieser Teil 002 legt die „Besonderen Regeln für Aluminium, Aluminiumlegierungen und Magnesiumlegie-rungen“ fest.
Série aérospatiale - Matériaux métalliques - Règles pour la rédaction et la présentation des normes de matériaux - Partie 002 : Règles spécifiques à l'aluminium, aux alliages d'aluminium et aux alliages de magnésium
La série EN 4500 spécifie les règles pour la rédaction et la présentation des normes de matériaux métalliques pour les applications aérospatiales.
La présente Partie 002 spécifie les « Règles spécifiques à l'aluminium, aux alliages d'aluminium et aux alliages de magnésium ».
Aeronavtika - Kovinski materiali - Pravila za načrtovanje in predstavljanje standarov za materiale - 002. del: Posebna pravila za aluminij, aluminijeve in magnezijeve zlitine
Skupina standardov EN 4500 določa pravila za načrtovanje in predstavljanje standardov za kovinske materiale za uporabo v aeronavtiki. Ta del 002 določa »Posebna pravila za aluminij, aluminijeve in magnezijeve zlitine«.
General Information
Relations
Overview
EN 4500-002:2024 - published by CEN and approved June 2024 - is Part 002 of the EN 4500 aerospace series. It defines the specific rules for drafting and presenting material standards for aluminium, aluminium alloys and magnesium alloys used in aerospace applications. This document complements the series’ general rules (EN 4500-001) by giving tailored guidance on titles, scope entries, temper and delivery conditions, and the structured presentation of technical requirements for these light alloys.
Key topics
- Scope and purpose: Rules for preparing European material standards specific to aluminium and magnesium alloys within the EN 4500 series framework.
- Title and introduction guidance: How to format titles and introductions consistent with EN 4500-001, including permitted dual use-conditions (e.g., T4 and T42 or T6 and T62) when metallurgically equivalent.
- Temper and delivery conditions: Use and notation of temper codes such as Tx510 / Tx511 (applicable to extruded bars, sections and drawn tubes) and reference to EN 515 for temper designations.
- Table 1 structure: A standardized table layout (multiple parts) for specifying:
- Material designation, chemical composition and melting method
- Form, production method and limit dimensions
- Delivery condition, heat treatment and use condition
- Test samples/test pieces, heat treatment of samples
- Dimensions, cladding thickness, test directions
- Mechanical and physical test entries (tensile, hardness, shear, bending, impact, creep)
- Inspection, marking and dimensional checks, notes and typical use
- Forms, surface and application descriptors: Approved terms for sheets, plates, bars, sections, tubes, forgings, castings and qualifiers (extruded, drawn, rolled, machined, clad, etc.).
- Informative annexes: Examples to illustrate title pages, introductions, completion of scope and Table 1; notes clarify that examples may not correspond to actual standardized products.
Applications and users
- Standards authors and technical committees - to prepare consistent EN material standards for aluminium/magnesium alloys in aerospace.
- Aerospace material engineers and designers - to interpret material specifications and ensure correct temper, form and testing requirements are specified.
- Procurement, quality and inspection teams - to verify supplier documentation, marking, dimensional checks and test reports align with standardized presentation.
- Manufacturers of semi-finished products - to prepare delivery documents and production processes that meet aerospace standard requirements.
Related standards
- EN 4500-001 (General rules for metallic materials series)
- EN 515 (Temper designations for aluminium)
- EN 4259 (Definition of general terms)
- EN 1753 (Magnesium alloys - ingots and castings)
Keywords: EN 4500-002:2024, aerospace standard, aluminium alloys, magnesium alloys, material standards, drafting rules, temper designations, CEN.
Standards Content (Sample)
SLOVENSKI STANDARD
01-oktober-2024
Aeronavtika - Kovinski materiali - Pravila za načrtovanje in predstavljanje
standarov za materiale - 002. del: Posebna pravila za aluminij, aluminijeve in
magnezijeve zlitine
Aerospace series - Metallic materials - Rules for drafting and presentation of material
standards - Part 002: Specific rules for aluminium, aluminium alloys and magnesium
alloys
Luft- und Raumfahrt - Metallische Werkstoffe - Regeln für das Erstellen und die
Gestaltung von Werkstoffnormen - Teil 002: Besondere Regeln für Aluminium,
Aluminiumlegierungen und Magnesiumlegierungen
Série aérospatiale - Matériaux métalliques - Règles pour la rédaction et la présentation
des normes de matériaux - Partie 002: Règles spécifiques à l'aluminium, aux alliages
d'aluminium et au alliages de magnésium
Ta slovenski standard je istoveten z: EN 4500-002:2024
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EN 4500-002
EUROPEAN STANDARD
NORME EUROPÉENNE
August 2024
EUROPÄISCHE NORM
ICS 01.120; 49.025.05; 49.025.15
English Version
Aerospace series - Metallic materials - Rules for drafting
and presentation of material standards - Part 002: Specific
rules for aluminium, aluminium alloys and magnesium
alloys
Série aérospatiale - Matériaux métalliques - Règles Luft- und Raumfahrt - Metallische Werkstoffe - Regeln
pour la rédaction et la présentation des normes de für das Erstellen und die Gestaltung von
matériaux - Partie 002 : Règles spécifiques à Werkstoffnormen - Teil 002: Besondere Regeln für
l'aluminium, aux alliages d'aluminium et aux alliages Aluminium, Aluminiumlegierungen und
de magnésium Magnesiumlegierungen
This European Standard was approved by CEN on 17 June 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 4500-002:2024 E
worldwide for CEN national Members.
Contents Page
European foreword . 4
Introduction . 5
1 Scope . 6
2 Normative references . 6
3 Terms and definitions . 6
4 Rules for drafting a European standard for aerospace metallic materials. 6
4.1 General. 6
4.2 Title . 6
4.2.1 General. 6
4.2.2 Condition T4 and T42 or T6 and T62 . 7
4.2.3 Descriptions . 7
4.3 Introduction . 9
4.3.1 General. 9
4.3.2 Condition Tx510 and Tx511, applicable to extruded bars and sections and drawn tubes . 9
4.4 Scope, normative references, terms and definitions, requirements . 9
4.5 Table 1 (1 of 3) . 9
4.5.1 Line 1: Material designation . 9
4.5.2 Line 2: Chemical composition. 9
4.5.3 Line 3: Method of melting . 9
4.5.4 Line 4.1: Form . 9
4.5.5 Line 4.2: Method of production . 10
4.5.6 Line 4.3: Limit dimension(s) . 10
4.5.7 Line 5: Technical specification . 10
4.5.8 Line 6.1: Delivery condition and Heat treatment . 10
4.5.9 Line 6.2: Delivery condition code . 10
4.5.10 Line 7: Use condition and Heat treatment . 10
4.5.11 Line 8.1: Test sample(s) . 10
4.5.12 Line 8.2: Test piece(s) . 10
4.5.13 Line 8.3: Heat treatment . 10
4.5.14 Line 9: Dimensions concerned . 10
4.5.15 Line 10: Thickness of cladding on each face . 10
4.5.16 Line 11: Direction of test piece . 10
4.5.17 Lines 12 to 16: Tensile (T) . 11
4.5.18 Line 17: Hardness . 11
4.5.19 Line 18: Shear strength . 11
4.5.20 Line 19: Bending . 11
4.5.21 Line 20: Impact strength . 11
4.5.22 Lines 21 to 26: Creep (C) . 11
4.5.23 Line 27: Notes (see line 98) . 11
4.6 Table 1 (2 of 3) . 11
4.6.1 Lines 28 to 94 . 11
4.6.2 Line 95: Marking inspection . 12
4.6.3 Line 96: Dimensional inspection . 12
4.6.4 Line 98: Notes . 12
4.6.5 Line 99: Typical use . 12
4.7 Table 1 (3 of 3) . 12
4.8 Bibliography . 12
Annex A (informative) Completion of title page . 13
Annex B (informative) Completion of the introduction . 14
Annex C (informative) Completion of the scope, normative references, terms and definitions, and
requirements . 15
Annex D (informative) Completion of Table 1 (1 of 3) . 16
Annex E (informative) Completion of Table 1 (2 of 3) . 17
Annex F (informative) Completion of Table 1 (3 of 3) . 22
Annex G (informative) Completion of the bibliography . 26
Bibliography . 27
European foreword
This document (EN 4500-002:2024) 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 XP prEN 4500-2:1997, which was published by ASD-STAN.
The main changes with respect to the previous edition are as follows:
XP prEN 4500-2, 02/1997 — Editorial improvements and update of the scope to change “single mode
fibre core” to “simplex fibre”.
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, Italy,
Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Republic of North
Macedonia, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Türkiye and the United
Kingdom.
Introduction
This document is part of the series of EN metallic material standards for aerospace applications.
The general organization of this series is described in EN 4258.
The EN 4500 series (Aerospace series — Metallic materials — Rules for drafting and presentation of
material standards) is composed by the following documents:
— General rules EN 4500-001;
— Specific rules for aluminium, aluminium alloys and EN 4500-002;
magnesium alloys
— Specific rules for heat-resisting alloys EN 4500-003;
— Specific rules for titanium and titanium alloys EN 4500-004;
— Specific rules for steels EN 4500-005;
— Specific rules for filler metals for welding EN 4500-002 to EN 4500-005;
— Specific rules for filler metals for brazing EN 4500-006.
1 Scope
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards
for aerospace applications.
This Part 002 specifies the “Specific rules for aluminium, aluminium alloys and magnesium alloys”.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements of this document. For dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
EN 515, Aluminium and aluminium alloys — Wrought products — Temper designations
EN 4259, Aerospace series — Metallic materials — Definition of general terms
EN 1753, Magnesium and magnesium alloys — Magnesium alloy ingots and castings
EN 4500-001, Aerospace series — Metallic materials — Rules for drafting and presentation of material
standards — Part 001: General rules
ASTM B275, Standard Practice for Codification of Certain Zinc, Tin and Lead Die Castings
3 Terms and definitions
For the purposes of this document, the terms and definitions given in EN 4259 and EN 4500-001 apply.
For temper designations, the terms and definitions given in EN 515 and EN 1753 apply.
ISO and IEC maintain terminology databases for use in standardization at the following addresses:
— ISO Online browsing platform: available at https://www.iso.org/obp/
— IEC Electropedia: available at https://www.electropedia.org/
4 Rules for drafting a European standard for aerospace metallic materials
4.1 General
Examples given in Annexes are only intended to illustrate the rules for drafting and presentation and
might not correspond to real standardized EN semi-finished products. Technological development can
require the use of terms additional to those listed.
4.2 Title
4.2.1 General
Should be according to EN 4500-001 and Annex A of this document.
Published by American Society for Testing and Materials (ASTM International), available at:
https://www.astm.org/
4.2.2 Condition T4 and T42 or T6 and T62
It is permissible to quote 2 (two) use conditions (e.g. T4 and T42 or T6 and T62) in the same material
standard providing they have the same mechanical properties and are metallurgically the same.
See Annex B.
4.2.3 Descriptions
4.2.3.1 General
The following are examples of some descriptions which may be used.
4.2.3.2 Surface condition entries
a) Where unclad or as manufactured, no entry required.
b) Clad.
c) Machined.
4.2.3.3 Form entries
a) Sheets and strips.
b) Plates.
c) Bars.
The term may be qualified with one or more of the following terms:
1) extruded;
2) drawn;
3) rolled.
d) Sections.
The term may be qualified with the following term:
1) extruded.
e) Bars and sections.
The term may be qualified with the following term:
1) extruded.
f) Tubes.
The term may be qualified with one or more of the following terms:
1) extruded;
2) drawn.
g) Wires.
h) Forging stock.
The term may be qualified with one or more of the following terms:
1) cast;
2) extruded.
i) Forgings.
The term may be qualified with one or more of the following terms:
1) die;
2) hand.
j) Remelting stock.
k) Castings.
The term may be qualified with one or more of the following terms:
1) sand;
2) permanent mould;
3) investment;
4) high-strength.
4.2.3.4 Additional information entries
— With peripheral coarse grain control.
— For structural applications.
— For hydraulic applications.
— For superplastic forming.
— Damage tolerant.
— For the manufacture of rivets.
— For the manufacture of fasteners.
— For machining.
— For welding.
4.3 Introduction
4.3.1 General
Should be according to EN 4500-001 and Annex B of this document.
4.3.2 Condition Tx510 and Tx511, applicable to extruded bars and sections and drawn tubes
Material standards shall be prepared on the basis that all material will be supplied in the Tx511
condition according to EN 515.
These standards can also be used to supply material in the Tx510 condition according to EN 515. In this
case, the scope shall be completed as shown in Annex C of this document.
4.4 Scope, normative references, terms and definitions, requirements
Should be according to EN 4500-001 and Annex C of this document.
4.5 Table 1 (1 of 3)
4.5.1 Line 1: Material designation
Should be according to EN 4500-001 and Annex D of this document.
4.5.2 Line 2: Chemical composition
The chemical composition shall be written in accordance with EN 4500-001 and the following rules:
a) aluminium alloys:
1) wrought products
The order of presentation of elements and chemical composition limits shall conform to that
registered with the Aluminium Association for that alloy designation;
2) cast products
The order of presentation of elements shall conform to the Aluminium Association order used
for wrought products;
b) magnesium alloys:
The order of presentation of elements and chemical composition limits shall conform to that
registered with the American Society for Testing and Materials, Committee B-7; currently listed in
ASTM B275.
4.5.3 Line 3: Method of melting
Not normally used for aluminium, aluminium alloys and magnesium alloys.
4.5.4 Line 4.1: Form
Should be according to EN 4500-001 and Annex D of this document.
4.5.5 Line 4.2: Method of production
Should be according to EN 4500-001 and Annex D of this document, using the applicable terms given
in 4.2.
4.5.6 Line 4.3: Limit dimension(s)
Should be according to EN 4500-001 and Annex D of this document.
4.5.7 Line 5: Technical specification
Should be according to EN 4500-001 and Annex D of this document.
4.5.8 Line 6.1: Delivery condition and Heat treatment
Should be according to EN 4500-001 and use the temper designations given in EN 515 or EN 1753.
See Annex D of this document.
4.5.9 Line 6.2: Delivery condition code
Should be according to EN 4500-001 and Annex D of this document.
4.5.10 Line 7: Use condition and Heat treatment
Should be according to EN 4500-001 and use the temper designations given in EN 515 or EN 1753. See
Annex D of this document, see also 4.2.2.
4.5.11 Line 8.1: Test sample(s)
Should be according to EN 4500-001 and Annex D of this document.
4.5.12 Line 8.2: Test piece(s)
Should be according to EN 4500-001 and Annex D of this document.
4.5.13 Line 8.3: Heat treatment
Should be according to EN 4500-001
...
Frequently Asked Questions
EN 4500-002:2024 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 002: Specific rules for aluminium, aluminium alloys and magnesium alloys". This standard covers: The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications. This Part 002 specifies the "Specific rules for aluminium, aluminium alloys and magnesium alloys".
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications. This Part 002 specifies the "Specific rules for aluminium, aluminium alloys and magnesium alloys".
EN 4500-002:2024 is classified under the following ICS (International Classification for Standards) categories: 01.120 - Standardization. General rules; 49.025.01 - Materials for aerospace construction in general; 49.025.05 - Ferrous alloys in general; 49.025.15 - Non-ferrous alloys in general; 49.025.20 - Aluminium. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 4500-002:2024 has the following relationships with other standards: It is inter standard links to prEN 4500-002. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
You can purchase EN 4500-002:2024 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.
The EN 4500-002:2024 standard is a critical document that outlines the specific rules for the drafting and presentation of material standards, particularly focusing on aluminium, aluminium alloys, and magnesium alloys used in aerospace applications. This standard serves a vital role in ensuring consistency and uniformity across material specifications, which is crucial for safety and performance in the aerospace sector. One of the key strengths of EN 4500-002:2024 is its comprehensive approach to addressing the unique characteristics of aluminium and magnesium alloys. It provides clear guidelines that help manufacturers and specifications writers create documents that are easily understandable and compliant with industry standards. The specificity of this standard facilitates improved communication among stakeholders, including engineers, designers, and quality assurance professionals, thereby promoting an overall higher quality of material selection and usage. Furthermore, the relevance of this standard cannot be overstated. In an industry where material properties can significantly impact the safety and efficiency of aerospace vehicles, having standardized rules for aluminium and magnesium alloys is essential. The guidelines provided in EN 4500-002:2024 not only enhance material traceability but also ensure compliance with international regulations, ultimately leading to more reliable aerospace structures. Additionally, the standard's focus on aluminium and magnesium alloys addresses critical aspects such as mechanical properties, testing methods, and material specifications, which are vital for modern aerospace applications that demand high performance and lightweight solutions. By adhering to EN 4500-002:2024, organizations can enhance their operational practices and contribute to the advancement of aerospace technology. In summary, the EN 4500-002:2024 standard provides essential guidance for the drafting and presentation of material standards specifically for aluminium and magnesium alloys in aerospace. Its strengths lie in fostering uniformity, improving communication, and ensuring compliance with crucial safety and performance metrics in the industry, solidifying its relevance in promoting high-quality aerospace materials.
SIST EN 4500-002:2024 문서는 항공우주 분야에서 사용되는 금속 재료의 표준 초안 작성 및 발표에 대한 규칙을 명시하고 있습니다. 특히, 이 표준은 알루미늄, 알루미늄 합금 및 마그네슘 합금에 대한 구체적인 규칙을 제공하여 금속 재료의 신뢰성을 높이는 데 중요한 역할을 합니다. 이 표준의 강점 중 하나는 항공우주 응용 분야에서의 재료 선택 및 사용에 대한 명확한 가이드라인을 제시한다는 것입니다. 이러한 표준화는 재료 성능의 일관성을 보장하므로, 엔지니어와 연구자들이 신뢰성 있는 자료를 바탕으로 작업할 수 있습니다. 아울러, 다양한 알루미늄 합금과 마그네슘 합금의 특성을 정의하고 이를 통해 설계자들이 최적의 재료를 선택할 수 있도록 돕습니다. EN 4500-002:2024는 금속 재료의 표준화가 필수적인 항공우주 산업의 발전에 기여할 뿐만 아니라, 국제적인 협업을 촉진하는 데에도 매우 중요한 기초 문서로써 기능합니다. 이 표준을 통해 알루미늄 및 그 합금, 마그네슘 합금에 대한 이해가 증진되고, 전 세계적으로 통일된 적용 기준을 마련함으로써 산업 내의 신뢰성을 강화하는 데 기여할 것입니다. 또한, EN 4500 시리즈의 일환으로 제정된 본 표준은 항공우주 산업의 지속적인 혁신과 기술 발전을 지원하는 기반을 마련함으로써, 기업들이 경쟁력을 유지하고 기술적 우위를 확보하는 데 중요한 역할을 할 것입니다. 따라서 SIST EN 4500-002:2024는 금속 재료의 표준화에 기여하는 필수적인 문서로, 관련 업계의 모두에게 매우 유의미한 내용으로 평가됩니다.
標準EN 4500-002:2024は、航空宇宙系列における金属材料に関する文書であり、金属材料の標準のドラフティングおよびプレゼンテーションに関する規則を定めています。本規格の主な焦点は、アルミニウム、アルミニウム合金、マグネシウム合金に関する特定のルールにあり、これにより航空宇宙用途に適した材料標準の整合性が確保されています。 この標準の範囲は非常に広く、航空宇宙産業における金属材料の仕様書の作成における重要なガイドラインを提供します。特に、アルミニウムおよびその合金は、軽量で高強度な性質から、航空機の構造部材に広く使用されているため、本規格の適用が重要です。マグネシウム合金も同様に、軽量化が求められる航空機設計において、特有の特性を活かすためにこの標準が欠かせません。 EN 4500-002:2024の強みは、明確で一貫性のある規則を提供することにより、各種標準の理解と実装を容易にする点です。これにより、関係者は高品質の材料を一貫して使用できるようになり、航空機の安全性や性能の向上に寄与します。また、国際的なビジネス環境においても、この標準が遵守されることで、各国間での材料基準の整合性が促進され、信頼性の向上が見込まれます。 結論として、SIST EN 4500-002:2024は、航空宇宙分野における金属材料の標準化を進めるための核となる基準であり、その重要性は今後ますます高まるでしょう。特に、アルミニウムとマグネシウム合金に関する具体的な規則は、航空宇宙産業の材料技術革新に寄与するものと期待されます。
La norme SIST EN 4500-002:2024 est d'une grande importance pour l'industrie aérospatiale, car elle établit des règles spécifiques pour la rédaction et la présentation des normes matérielles relatives aux matériaux métalliques, en mettant particulièrement l'accent sur l'aluminium, les alliages d'aluminium et les alliages de magnésium. Cette norme fait partie de la série EN 4500, qui encadre les matériaux métalliques utilisés dans les applications aérospatiales. L'un des points forts de cette norme est sa capacité à fournir des directives claires et précises pour la standardisation des matériaux, ce qui est essentiel dans un secteur où la sécurité et la performance sont primordiales. Avec des règles spécifiques énoncées pour l'aluminium et ses alliages, ainsi que pour les alliages de magnésium, la norme aide à garantir que tous les acteurs de l'industrie travaillent à partir de critères communs, réduisant ainsi les risques de confusion et d'erreurs. La pertinence de la norme SIST EN 4500-002:2024 réside également dans sa contribution à l'innovation et à l'évolution des matériaux utilisés dans l'aérospatial. En favorisant l'uniformité dans la présentation des spécifications, les concepteurs et les fabricants peuvent se concentrer sur l'amélioration des performances des matériaux, tout en respectant des exigences de qualité élevées. Cela se traduit par des produits plus fiables et plus sûrs, qui sont cruciaux pour l'aviation moderne. En résumé, la norme SIST EN 4500-002:2024 se positionne comme un outil essentiel pour les professionnels du secteur aérospatial, offrant des lignes directrices robustes qui favorisent la standardisation et l'innovation dans l'utilisation des matériaux métalliques. Sa focalisation sur l'aluminium, les alliages d'aluminium et les alliages de magnésium en fait un référentiel indispensable pour assurer un développement cohérent et de qualité au sein de l'industrie.
Der Standard EN 4500-002:2024 bietet eine umfassende Regelung für die Ausarbeitung und Präsentation von Metallmaterialnormen im Bereich der Luft- und Raumfahrt. Insbesondere fokussiert dieser Teil auf spezifische Regeln für Aluminium, Aluminiumlegierungen und Magnesiumlegierungen, was für die Luftfahrtindustrie von entscheidender Bedeutung ist. Ein wesentlicher Stärke des Dokuments ist die klare Strukturierung, die es den Fachleuten ermöglicht, sich schnell in den relevanten Normen zurechtzufinden. Die detaillierten Vorgaben fördern Einheitlichkeit und Präzision in der Materialdokumentation, was insbesondere bei sicherheitsrelevanten Anwendungen wie der Luft- und Raumfahrt unabdingbar ist. Durch die Definition spezifischer Anforderungen an Aluminium und seine Legierungen gewährleistet der Standard hohe Qualität und Konsistenz in der Produktion sowie Verarbeitung dieser Materialien. Die Relevanz von EN 4500-002:2024 unterstreicht sich durch die ständig wachsenden Anforderungen in der Luftfahrtindustrie hinsichtlich Gewichtsoptimierung und Materialeffizienz. Aluminium und Magnesiumlegerungen sind aufgrund ihrer vorteilhaften Eigenschaften, wie geringes Gewicht und hohe Festigkeit, zentrale Materialien in der Konstruktion moderner Flugzeuge. Die Richtlinien dieses Standards unterstützen die Hersteller dabei, die Herausforderungen bezüglich der Materialauswahl und -verarbeitung effektiv zu meistern. Zusammenfassend lässt sich sagen, dass der Standard EN 4500-002:2024 nicht nur die technischen Anforderungen klar definiert, sondern auch ein fundamentales Instrument für die Gewährleistung von Qualität, Sicherheit und Effizienz in der Verwendung von Aluminium, Aluminiumlegierungen und Magnesiumlegierungen in der Luft- und Raumfahrt darstellt.
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