DIN EN 2817-2010 Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted Solution treated and precipitation treated Bar for machining a or D 200 mm R 1070.pdf

1、 DEUTSCHE NORMApril 2010DIN EN 2817 ICS 49.025.10 Luft- und Raumfahrt Stahl FE-PM1802 (X5CrNiCu15-5) mit selbstverzehrender Elektrode umgeschmolzen, lsungsgeglht und ausgehrtet, Stangen zur spanenden Bearbeitung, a oder D 200 mm, Rm 1 070 MPa; Deutsche und Englische Fassung EN 2817:2009 Aerospace se

2、ries Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted, Solution treated and precipitation treated, Bar for machining, a or D 200 mm, Rm 1 070 MPa; German and English version EN 2817:2009 Srie arospatiale Acier FE-PM1802 (X5CrNiCu15-5) Refondu llectrode consommable Mis en solution et viei

3、lli, Barres pour usinage, a ou D 200 mm, Rm 1 070 MPa; Version allemande et anglaise EN 2817:2009 Gesamtumfang 17 SeitenNormenausschuss Luft- und Raumfahrt (NL) im DIN DIN Deutsches Institut fr Normung e.V. Jede Art der Vervielfltigung, auch auszugsweise, nur mitGenehmigung des DIN Deutsches Institu

4、t fr Normung e.V., Berlin gestattet. Alleinverkauf der Normen durch Beuth Verlag GmbH, 10772 Berlin Preisgruppe 8 www.din.de www.beuth.de !$ Kerbrichtung T; + 35 bei 30 C 80; Kerbrichtung T + 35 bei 30 C 55; Kerbrichtung L + 25 bei 30 C 21 Temperatur C 22 Beanspruchungs-dauer h 23 Kriechbean-spruchu

5、ng aMPa 24 Bleibende Dehnung a % 25 Zeitstandbe-anspruchung RMPa 26 C Bruchdeh-nung A % 27 Bemerkungen (siehe Zeile 98) DIN EN 2817:2010-04 EN 2817:2009 (D) 7 EN 4436 2 1 je Schmelze 3 Entspricht dem oberen Blockende. 30 Mikrogefge 7 Der -Ferritgehalt darf 2 % nicht berschreiten. Siehe EN 4700-2.34

6、Korngre 7 G 5 Siehe EN 4700-2. 44 uere Fehler 1 Sichtprfung Siehe EN 4700-2.50 Reinheit/Gehalt an Einschlssen (mikroskopische Reinheit) 7 Kategorie 4 Siehe EN 4700-2 Klasse Zustand Schrfegrad 1 Flecken A 2 Weie Flecken A3 Radialseigerung A51 Makrogefge 7 4 Ringmuster B Siehe EN 4700-2. 6 a oder D 10

7、0 mm kann entweder am Erzeugnis oder in einem frheren Fertigungsstadium geprft werden. 61 Innere Fehler 7 Klasse 3 95 Prfung der Kennzeichnung Siehe EN 4700-2.96 Maprfung Siehe EN 4700-2. 98 Bemerkungen 99 Typische Anwendung DIN EN 2817:2010-04 EN 2817:2009 (D) 8 Siehe EN 2043. 100 Produktqualifikat

8、ion Das Qualifikationsprogramm ist zwischen Hersteller und Kufer zu vereinbaren. DIN EN 2817:2010-04 EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2817 November 2009 ICS 49.025.10 English Version Aerospace series Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted, Solution treated a

9、nd precipitation treated, Bar for machining, a or D 200 mm, Rm 1 070 MPa Srie arospatiale Acier FE-PM1802 (X5CrNiCu15-5) Refondu llectrode consommable Mis en solution et vieilli, Barres pour usinage, a ou D 200 mm, Rm 1 070 MPa Luft- und Raumfahrt Stahl FE-PM1802 (X5CrNiCu15-5) mit selbstverzehrende

10、r Elektrode umgeschmolzen, lsungsgeglht und ausgehrtet, Stangen zur spanenden Bearbeitung, a oder D 200 mm, Rm 1 070 MPa This European Standard was approved by CEN on 8 August 2009. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving th

11、is 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 Management Centre or to any CEN member. This European Standard exists in three official versions

12、 (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 Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bu

13、lgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDA

14、RDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2817:2009: EEN 2817:2009 (E) 2 Foreword This document

15、 (EN 2817:2009) 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 approval of the National Associations and the Official

16、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 May 2010, and conflicting national standards shall be withdrawn at the la

17、test by May 2010. 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 the CEN/CENELEC Internal Regulations, the national stan

18、dards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, P

19、ortugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. DIN EN 2817:2010-04 EN 2817:2009 (E) 3 Introduction This European Standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described

20、 in EN 4258. This standard has been prepared in accordance with EN 4500-5. DIN EN 2817:2010-04 EN 2817:2009 (E) 4 1 Scope This European Standard specifies the requirements relating to: Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted Solution treated and precipitation treated Bar for mac

21、hining a or D 200 mm Rm 1 070 MPa for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document

22、(including any amendments) applies. EN 2043, Aerospace series Metallic materials General requirements for semi-finished product qualification (excluding forgings and castings) 1)EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards a

23、nd their use EN 4436, Aerospace series Steel Test methods Determination of ferrite content1)EN 4500-5, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 5: Specific rules for steels1) EN 4700-002, Aerospace series Steel and heat resisting alloys Wroug

24、ht products Technical specification Part 002: Bar and section 1)1) Published as ASD-STAN Prestandard at the date of publication of this standard. DIN EN 2817:2010-04 EN 2817:2009 (E) 5 1 Material designation Steel FE-PM1802 (X5CrNiCu15-5) Element C Si Mn P S Cr Mo Ni Cu Nb + Ta Fe 2 min. 14,0 3,5 2,

25、5 5 C Chemical composition % max. 0,07 1,00 1,00 0,030 0,015 15,5 0,50 5,5 4,5 0,45 Base 3 Method of melting Consumable electrode remelted 4.1 Form Bar 4.2 Method of production 4.3 Limit dimension(s) mm a or D 200 5 Technical specification EN 4700-2 Delivery condition Solution treated Solution treat

26、ed and precipitation treated 6.1 Heat treatment 1 025 C 1 055 C / t 30 min / AC or OQ+ cool to 30 C 1 025 C 1 055 C / t 30 min / AC or OQ + cool to 30 C + 535 C 565 C / t 4 h / AC 6.2 Delivery condition code W UUse condition Solution treated and precipitation treated Delivery condition 7 Heat treatm

27、ent Delivery condition + 535 C 565 C / t 4 h / AC Characteristics 8.1 Test sample(s) See EN 4700-2. 8.2 Test piece(s) See EN 4700-2. 8.3 Heat treatment Solution treated Use condition 9 Dimensions concerned mm a or D 200 a or D 75 75 a or D 200 10 Thickness of cladding on each face % 11 Direction of

28、test piece L L T 12 Temperature C Ambient Ambient Ambient 13 Proof stress Rp0,2 MPa 1 000 1 000 1 000 14 Strength Rm MPa 1 070 1 070 1 070 15 Elongation A % 11 10 7 16 T Reduction of area Z % 45 40 27 17 Hardness 363 HB 331 HB 401 331 HB 401 331 HB 401 18 Shear strength Rc MPa 19 Bending k 20 Impact

29、 strength KV J 80; Notch direction T + 35, at 30 C 80; Notch direction T + 35, at 30 C 55; Notch direction L + 25, at 30 C 21 Temperature C 22 Time h 23 Stress a MPa 24 Elongation a % 25 Rupture stress R MPa 26 C Elongation at rupture A % 27 Notes (see line 98) DIN EN 2817:2010-04 EN 2817:2009 (E) 6

30、 30 Microstructure EN 4436 2 One per cast 3 Corresponding to ingot top 7 The ferrite content shall not exceed 2 % 34 Grain size See EN 4700-2. 7 G 5 44 External defects See EN 4700-2. 1 Visual 50 Cleanliness/inclusion content See EN 4700-2. (micro-cleanness) 7 Category 4 51 Macrostructure See EN 470

31、0-2. 7 Class Condition Severity 1 Freckles A 2 White spots A 3 Radial segregation A 4 Ring pattern B 61 Internal defects See EN 4700-2. 6 a or D 100 mm may be tested either on the product or at an earlier stage of manufacturing. 7 Class 3 95 Marking inspection See EN 4700-2. 96 Dimensional inspection See EN 4700-2. 98 Notes 99 Typical use DIN EN 2817:2010-04 EN 2817:2009 (E) 7 100 Product qualification See EN 2043. Qualification programme to be agreed between manufacturer and purchaser. DIN EN 2817:2010-04