1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 2213 Edition P 1 November 2010 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8131 - www.asd-stan.orgICS: Descriptors: ENGL
2、ISH VERSION Aerospace series Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bars De 16 mm 980 MPa Rm 1 180 MPa Srie arospatiale Acier FE-PL1505 (15CrMoV6) labor lair Tremp et revenu Barres De 16 mm 980 MPa Rm 1 180 MPa Luft- und Raumfahrt Stahl FE-PL1505 (15CrMoV6) Lufterschmolzen Gehrt
3、et und angelassen Stangen De 16 mm 980 MPa Rm 1 180 MPa 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
4、been technically approved 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 sta
5、ndard. After examination and 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 t
6、he EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 1stNovember 2010 Comments should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain
7、 Copyright 2010 by ASD-STAN prEN 2213:2010 (E) 2 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 standard has been prepared in accordance with EN 4500-5. 1 Scope This
8、standard specifies the requirements relating to: Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bars De 16 mm 980 MPa Rm 1 180 MPa for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated refe
9、rences, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2043, Aerospace series Metallic materials General requirements for semi-finished product qualification (excluding forgings and castings) 1)EN 2951, Aer
10、ospace series Metallic materials Test method Micrographic determination of content of non-metallic inclusions 1)EN 4050-4, Aerospace series Test method for metallic materials Ultrasonic inspection of bars, plates, forging stock and forgings Part 4: Acceptance criteria EN 4258, Aerospace series Metal
11、lic materials General organization of standardization Links between types of EN standards and their use EN 4500-5, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 5: Specific rules for steels 1)EN 4700-002, Aerospace series Steel and heat resisting
12、alloys Wrought products Technical specification Part 002: Bar and section 1)EN ISO 642, Steel Hardenability test by end quenching (Jominy test) 1) Published as ASD-STAN Standard at the date of publication of this standard by Aerospace and Defence Industries Association of Europe-Standardization (ASD
13、-STAN), (www.asd-stan.org). prEN 2213:2010 (E) 3 1 Material designation Steel FE-PL1505 (15CrMoV6) Element C Si Mn P S Cr Mo V Fe min. 0,12 0,80 1,25 0,80 0,20 2 Chemical composition % max. 0,18 0,20 1,10 0,020 0,015 1,50 1,00 0,30 Base 3 Method of melting Air melted 4.1 Form Bars 4.2 Method of prod
14、uction 4.3 Limit dimension(s) mm De 16 5 Technical specification EN 4700-002 Delivery condition Annealed Hardened and tempered 6.1 Heat treatment 955 C 995 C / AC 615 C 655 C a6.2 Delivery condition code A U Use condition Hardened and tempered Delivery condition 7 Heat treatment Delivery condition 9
15、55 C 995 C / AC 615 C 655 C a Characteristics 8.1 Test sample(s) See EN 4700-002. 8.2 Test piece(s) See EN 4700-002. 8.3 Heat treatment Annealed Hardened and tempered 9 Dimensions concerned mm De 16 10 Thickness of cladding on each face % 11 Direction of test piece L 12 Temperature C Ambient 13 Proo
16、f stress Rp0,2 MPa 780 14 Strength Rm MPa 980 Rm 1 180 15 Elongation A % 12 b16 T Reduction of area Z % 17 Hardness HB 197 291 HB 350 18 Shear strength Rc MPa 19 Bending k 20 Impact strength KV J 30 21 Temperature C 22 Time h 23 Stress a MPa 24 Elongation a % 25 Rupture stress R MPa 26 C Elongation
17、at rupture A % 27 Notes (see line 98) a, bprEN 2213:2010 (E) 4 31 Hardenabilty (Jominy test) See EN 4700-002. 1 EN ISO 642 7 The “capability clause“ applies Distance in mm 1,5 5 9 15 25 40 HRC min. 38 37 35 32 31 29 34 Grain size See EN 4700-002. 7 G 5 44 External defects See EN 4700-002. 1 Visual 5
18、0 Cleanliness/inclusion content See EN 4700-002. (Micro cleanness) 1 EN 2951 7 Category 1 51 Macrostructure (Grain flow) See EN 4700-002. 61 Internal defects See EN 4700-002. 7 Class 3, see EN 4050-4. 95 Marking inspection See EN 4700-002. 96 Dimensional inspection See EN 4700-002. 98 Notes a The ra
19、nge of temperature of tempering shall be adjusted on the wire rod if the bar is made from cold working b In case of cold working transformation, elongation could be 10 % minimum. 99 Typical use prEN 2213:2010 (E) 5 100 Product qualification See EN 2043. Qualification programme to be agreed between manufacturer and purchaser.
