AECMA PREN 4629-2006 Aerospace series Steel FE-PM 3504 (X4CrNiMo16-5-1) Air melted Hardened and tempered Forgings Stock De or = to 300 mm Edition P 1《航空航天系列.钢FE-PM 3504(X4CrNiMo16-.pdf

《AECMA PREN 4629-2006 Aerospace series Steel FE-PM 3504 (X4CrNiMo16-5-1) Air melted Hardened and tempered Forgings Stock De or = to 300 mm Edition P 1《航空航天系列.钢FE-PM 3504(X4CrNiMo16-.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 4629-2006 Aerospace series Steel FE-PM 3504 (X4CrNiMo16-5-1) Air melted Hardened and tempered Forgings Stock De or = to 300 mm Edition P 1《航空航天系列.钢FE-PM 3504(X4CrNiMo16-.pdf（6页珍藏版）》请在麦多课文档分享上搜索。

1、ASD STANDARD NORME ASD ASD NORM prEN 4629 Edition P 1 September 2006 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONGulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION Aerospace se

2、ries Steel FE-PM 3504 (X4CrNiMo16-5-1) Air melted Hardened and tempered Forging stock De 300 mm Srie arospatiale Acier FE-PM 3504 (X4CrNiMo16-5-1) labor lair Tremp et revenu Demi-produits pour forgeage De 300 mm Luft- und Raumfahrt Stahl FE-PM 3504 (X4CrNiMo16-5-1) Lufterschmolzen Gehrtet- und angel

3、assen Schmiedestcke De 300 mm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved

4、by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination a

5、nd review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level by

6、 giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 30 September 2006 Comments should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2006 by ASD-ST

7、AN Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4629:20062 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STAN

8、s Metallic Material Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under

9、 license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4629:20063 Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This

10、standard has been prepared in accordance with EN 4500-5. 1 Scope This standard specifies the requirements relating to: Steel FE-PM 3504 (X4CrNiMo16-5-1) Air melted Hardened and tempered Forging stock De 300 mm for aerospace applications. 2 Normative references The following referenced documents are

11、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 (including any amendments) applies. EN 2951, Aerospace series Metallic materials Test method Micrographic determination of c

12、ontent of non-metallic inclusions. 1)EN 2957, Aerospace series Method of preparation of forged samples. 1)EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use. EN 4050-2, Aerospace series Test method for metallic mater

13、ials Ultrasonic inspection of bars, plates, forging stock and forgings Part 2: Performance of test.1)EN 4500-5, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 5: Specific rules for steels. 1)EN 4700-5, Aerospace series Steel and heat resisting allo

14、ys Wrought products Technical specification Part 5: Specific rules for steel. 2)1) Published as ASD Prestandard at the date of publication of this standard.2) In preparation at the date of publication of this standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provide

15、d by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4629:20064 1 Material designation Steel FE-PM 3504 (X4CrNiMo16-5-1) Element C Si Mn P aS aN Cr Mo Ni Fe min. 15,00 0,80 4,00 2 Chemical composition % max. 0,06 0,70 1,50 0,030 0,

16、005 0,020 17,00 1,50 6,00 Base 3 Method of melting Air melted 4.1 Form Forging stock 4.2 Method of production 4.3 Limit dimension(s) mm De 300 mm 5 Technical specification EN 4700-5 Delivery condition Softened 6.1 Heat treatment 6.2 Delivery condition code U Use condition Delivery condition 7 Heat t

17、reatment Characteristics 8.1 Test sample(s) See EN 4700-5. Reforged sample in accordance to EN 2957 or cut from forging stock 8.2 Test piece(s) See EN 4700-5. 8.3 Heat treatment Delivery condition See line 29. 9 Dimensions concerned mm De 300 mm De 300 mm 10 Thickness of cladding on each face % 11 D

18、irection of test piece L TL 12 Temperature C Ambient Ambient Ambient 13 Proof stress Rp0,2MPa 700 700 14 Strength RmMPa 900 / 1 050 900 / 1 050 15 Elongation A % 16 12 16 T Reduction of area Z % 17 Hardness HB 293 269 HB 331 269 HB 331 18 Shear strength RcMPa 19 Bending k 20 Impact strength 120 J at

19、 20 C Notch direction T 70 J at 40 C Notch direction T 60 J at 20 C Notch direction L 35 J at 40 C Notch direction L 21 Temperature C 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 C Elongation at rupture A % 27 Notes (see line 98) aCopyright Association Europeene des Construct

20、eurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4629:20065 29 Reference heat treatment Hardened and tempered 1 010 C 1 060 C / OQ or WQ + 580 C 610 C 30 Microstructure See EN 4700-5. 7 The f

21、errite content shall not exceed 5 %.34 Grain size See EN 4700-5. 7 G = 5 or finer 44 External defects See EN 4700-5. 50 Cleanliness/inclusion content 1 See EN 4700-5. (micro cleanness) 7 EN 2951 category 2 51 Macrostructure See EN 4700-5. 61 Internal defects See EN 4700-5. 7 EN 4050-2 class 2 95 Mar

22、king inspection See EN 4700-5. 96 Dimensional inspection See EN 4700-5. 98 Notes aFor specific welding applications (e.g. high power beam), and after agreement between manufacturer and purchaser, S+P should be inferior or equal to 0,023% 99 Typical use Copyright Association Europeene des Constructeu

23、rs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4629:20066 100 Product qualification See EN 2043. Qualification programme to be agreed between manufacturer and purchaser. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-