1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationAerospace series Metallic materials Rules for drafting and presentation of material standardsPart 005: Specific rules for steelsBS EN 4500-005:2012National forewordThis British S
2、tandard is the UK implementation of EN 4500-005:2012.The UK participation in its preparation was entrusted to Technical CommitteeACE/61, Metallic materials for aerospace purposes.A list of organizations represented on this committee can be obtained onrequest to its secretary.This publication does no
3、t purport to include all the necessary provisions of acontract. Users are responsible for its correct application. The British Standards Institution 2012Published by BSI Standards Limited 2012ISBN 978 0 580 78587 0ICS 49.025.05; 49.025.15Compliance with a British Standard cannot confer immunity from
4、legal obligations.This British Standard was published under the authority of the StandardsPolicy and Strategy Committee on 31 October 2012.Amendments issued since publicationAmd. No. Date Text affectedBRITISH STANDARDBS EN 4500-005:2012EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4500-005 Oc
5、tober 2012 ICS 49.025.10 English Version Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 005: Specific rules for steels Srie arospatiale - Matriaux mtalliques - Rgles pour la rdaction et la prsentation des normes de matriaux - Partie 005: Rgle
6、s spcifiques aux aciers Luft- und Raumfahrt - Metallische Werkstoffe - Regeln fr das Erstellen und die Gestaltung von Werkstoffnormen - Teil 005: Besondere Regeln fr Sthle This European Standard was approved by CEN on 23 June 2012. CEN members are bound to comply with the CEN/CENELEC Internal Regula
7、tions 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
8、. 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
9、 members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, P
10、ortugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2012 CEN All rights of exploitation in any form and b
11、y any means reserved worldwide for CEN national Members. Ref. No. EN 4500-005:2012: EBS EN 4500-005:2012EN 4500-005:2012 (E) 2 Contents Page Foreword 3Introduction .41 Scope 42 Normative references 43 Terms and definitions .44 Rules for drafting and presentation .4Bibliography . 20BS EN 4500-005:201
12、2EN 4500-005:2012 (E) 3 Foreword This document (EN 4500-005:2012) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the appro
13、val of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by April 2013, and conflic
14、ting national standards shall be withdrawn at the latest by April 2013. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to t
15、he CEN/CENELEC Internal Regulations, the national standards organisations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece,
16、Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 4500-005:2012EN 4500-005:2012 (E) 4 Introduction This standard is part of the series of EN meta
17、llic material standards for aerospace applications. The general organisation of this series is described in EN 4258. 1 Scope This European Standard specifies the specific rules for the drafting and presentation of steels material standards for aerospace applications. It should be used in conjunction
18、 with EN 4500-001. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (
19、including any amendments) applies. EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use EN 4500-001, Aerospace series Metallic materials Rules for draftingand presentation of material standards Part 001: General rules
20、EN 10083-1, Steels for quenching and tempering Part 1: general technical delivery conditions 3 Terms and definitions For the purposes of this document, the terms and definitions given in EN 4500-001 apply. 4 Rules for drafting and presentation 4.1 Page 1 Title 4.1.1 General See EN 4500-001 and Examp
21、le 1 of this standard. The following are examples of descriptions which shall be used. BS EN 4500-005:2012EN 4500-005:2012 (E) 5 4.1.2 Method of melting Complete in accordance with EN 4500-001 using one or more of the following terms: air melted; vacuum induction melted; vacuum refined; vacuum arc r
22、emelted; electro-slag remelted; consumable electrode remelted. 4.1.3 Form entries a) sheet, strip, plate; The terms may be qualified with one of the following terms: rolled; cold rolled; hot rolled. b) bar; The term may be qualified with one or more of the following terms: rolled; hot rolled; cold r
23、olled; drawn; extruded; forged. c) section; The term may be qualified with one or more of the following terms: rolled; hot rolled; cold rolled; drawn; extruded; forged. BS EN 4500-005:2012EN 4500-005:2012 (E) 6 d) tube; The term may be qualified with one or more of the following terms: rolled; drawn
24、; extruded; seamless; welded. e) wire; The term may be qualified with one or more of the following terms: hot drawn; cold drawn; hot rolled; cold rolled. f) forging stock; g) forgings; h) remelting stock; i) castings; The term may be qualified with one or more of the following terms: sand; chill; in
25、vestment; centrifugal; hot isostatically pressed (hipped). j) ring; The term may be qualified with one or more of the following terms: rolled; forged; welded. BS EN 4500-005:2012EN 4500-005:2012 (E) 7 4.1.4 Additional information entries for structural applications; for pressure applications; for th
26、e manufacture and fasteners; for the manufacture of rivets; for machining; for forged rings; for rolled rings; for welding; for the manufacture of bearings; for carburizing or other thermo-chemical treatment; for nitriding. 4.2 Page 2 See EN 4500-001. 4.3 Page 3 See EN 4500-001 and Example 2 of this
27、 standard. 4.4 Page 4 4.4.1 Page 4, line 1: Material designation See EN 4500-001 and Example 3 of this standard. 4.4.2 Page 4, line 2: Chemical composition The chemical composition shall be written in accordance with EN 4500-001 and the order of presentation of elements shall conform to the followin
28、g rules: C, Si, Mn, P, S, Cr, Mo, Ni; Al, As, B, Co, Cu, N, Nb, Pb, Sn, Ti, V, W, Zr; all other elements except hydrogen shall be written in alphabetical order of their chemical symbols; H; ratio and/or total of above elements. BS EN 4500-005:2012EN 4500-005:2012 (E) 8 4.4.3 Page 4, line 3: Method o
29、f melting See EN 4500-001 and Example 3 of this standard, using the terms listed in 4.1.2. 4.4.4 Page 4, line 4.1: Form See EN 4500-001 and Example 3 of this standard. 4.4.5 Page 4, line 4.2: Method of production See EN 4500-001 and Example 3 of this standard, using the applicable terms given in 4.1
30、. 4.4.6 Page 4, line 4.3: Limit dimension(s) See EN 4500-001 and Example 3 of this standard. For steels, the equivalent diameter Defor determining the limiting dimensions is obtained as follows: for uniform single shapes, use the information given in EN 10083-1; for non-uniform shapes, use the proce
31、dure given in EN 10083-1. 4.4.7 Page 4, line 5: Technical specification See EN 4500-001 and Example 3 of this standard. 4.4.8 Page 4, line 6.1: Delivery condition and Heat treatment See EN 4500-001 and Example 3 of this standard. Use one or more of the following terms: not heat treated; softened; an
32、nealed; solution treated; precipitation treated; hardened; tempered; sub-zero treated; cold worked; descaled; machined ground. 4.4.9 Page 4, line 6.2: Delivery condition code See EN 4500-001 and Example 3 of this standard. BS EN 4500-005:2012EN 4500-005:2012 (E) 9 4.4.10 Page 4, line 7: Use conditio
33、n and Heat treatment See EN 4500-001 and Example 3 of this standard. Use the terms given in 4.4.8 or state: Delivery condition. 4.4.11 Page 4, line 8.1: Test sample(s) See EN 4500-001 and Example 3 of this standard. 4.4.12 Page 4, line 8.2: Test piece(s) See EN 4500-001 and Example 3 of this standar
34、d. 4.4.13 Page 4, line 8.3: Heat treatment See EN 4500-001 and Example 3 of this standard. 4.4.14 Page 4, line 9: Dimensions concerned See EN 4500-001 and Example 3 of this standard. 4.4.15 Page 4, line 10: Thickness of cladding on each face Not applicable to steel. 4.4.16 Page 4, line 11: Direction
35、 of test piece See EN 4500-001 and Example 3 of this standard. 4.4.17 Page 4, lines 12 to 16: Tensile (T) See EN 4500-001 and Example 3 of this standard. 4.4.18 Page 4, line 17: Hardness See EN 4500-001 and Example 3 of this standard. 4.4.19 Page 4, line 18: Shear strength See EN 4500-001 and Exampl
36、e 3 of this standard. 4.4.20 Page 4, line 19: Bending See EN 4500-001 and Example 3 of this standard. 4.4.21 Page 4, line 20: Impact strength See EN 4500-001 and Example 3 of this standard. 4.4.22 Page 4, lines 21 to 26: Creep (C) See EN 4500-001 and Example 3 of this standard. BS EN 4500-005:2012EN
37、 4500-005:2012 (E) 10 4.4.23 Page 4, line 27: Notes (see line 98) See EN 4500-001 and Example 3 of this standard. 4.5 Page 5, lines 28 to 99 4.5.1 Page 5, line 29: Reference heat treatment See EN 4500-001 and Example 4 of this standard. 4.5.2 Page 5, lines 30 to 94 The relevant lines shall be comple
38、ted in accordance with EN 4500-001, see Example 4 of this standard. 4.5.3 Page 5, line 95: Marking inspection See EN 4500-001 and Example 4 of this standard. 4.5.4 Page 5, line 96: Dimensional inspection See EN 4500-001 and Example 4 of this standard. 4.5.5 Page 5, line 98: Notes See EN 4500-001 and
39、 Example 4 of this standard. 4.5.6 Page 5, line 99: Typical use See EN 4500-001 and Example 4 of this standard. 4.6 Page 6, line 100: “Product qualification“ See EN 4500-001 and Example 5 of this standard. BS EN 4500-005:2012EN 4500-005:2012 (E) 11 Example 1: Completion of title Aerospace series Ste
40、el 100Cr6 (1.3505) Air melted Annealed Bar for machining D 100 mm 900 MPa Rm 1 100 MPa Srie arospatiale Acier 100Cr6 (1.3505) labor lair Recuit Barres pour usinage D 100 mm 900 MPa Rm 1 100 MPa Luft- und Raumfahrt Stahl 100Cr6 (1.3505) Lufterschmolzen Geglht Stangen zur spanenden Bearbeitung D 100 m
41、m 900 MPa Rm 1 100 MPa BS EN 4500-005:2012EN 4500-005:2012 (E) 12 Example 2: Completion of page 3 Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organisation of this series is described in EN 4258. This standard has been pre
42、pared in accordance with EN 4500-005. 1 Scope This European Standard specifies the requirements relating to: Steel 100Cr6 (1.3505) Air melted Annealed Bar for machining D 100 mm 900 MPa Rm 1 100 MPa for aerospace applications. NOTE Other common designation: 100C6, AECMA: FE-PL 31, ASD STAN: FE-PL 18
43、01. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any a
44、mendments) applies. EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use EN 4500-005, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 005: Specific rules for steel EN
45、4700-001, Aerospace series Steel and heat resisting alloys Wrought products Technical specification Part 001: Plate, sheet and strip BS EN 4500-005:2012EN 4500-005:2012 (E) 13 Example 3: Completion of page 4 1 Material designation Steel 100Cr6 (1.3505) 2 Chemical composition % Element C Si Mn P S Cr
46、 Mo Ni Al Cu Ti V O2Fe min. 0,95 0,15 0,25 1,35 Basemax. 1,10 0,35 0,45 0,015 0,010 1,65 0,10 0,40 0,50 0,30 0,50 0,30 25 *) 3 Method of melting Air melted 4.1 Form Bar for machining 4.2 Method of production Rolled 4.3 Limit dimension(s) mm D 100 5 Technical specification EN 4700-002 6.1 Delivery co
47、ndition Annealed Solution treatedHeat treatment 800 C 850 C 100 C 1 050 C / t 30 min WQ or AQ 6.2 Delivery condition code A U 7 Use condition Solution treated Delivery condition Heat treatment Delivery condition + 1 000 C 1 050 C / t 30 min WQ or AQ Characteristics 8.1 Test sample(s) EN 4700-002 8.2
48、 Test piece(s) EN 4700-002 8.3 Heat treatment Use condition 9 Dimensions concerned mm D 100 10 Thickness of cladding on each face % 11 Direction of test piece L 12 T Temperature C Ambient 13 Proof stress Rp0,2MPa 180 14 Strength RmMPa 450 Rm 650 15 Elongation A % 45 16 Reduction of area Z % 17 Hardness HBW 187 18 Shear strength RcMPa 19 Bending k 20 Impact strength KU 60; notch direction ST 21 C Temperature C 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 Elongation at rupture A % 27 Notes (see line 98) *) BS EN 4500-005:2
