AECMA PREN 3361-2000 Aerospace Series Steel FE-PM1802 (X5CrNiCu15-5) Consumable Electrode Remelted Solution Treated and Precipitation Treated Sheet and Strip a Less Than or Equal th.pdf

1、STD-AECIA PREN 33bL-ENGL 2000 H 10123LL 00L835b LUA Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ICSY-LEC-MOULINEAUX CEDEX I I AECMA STANDARD NORME AECMA AECMA NORM prEN 3361 Edition P 3 May 2000 PUBLISHED BY THE EUROPEAN ASSOCIATION OF A

2、EROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 6-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 Supersedes edition P 2 December 1997 ICs: Descriptors: ENGLISH VERSION Aerospace series Steel FE-PMI802 (X5CrNiCul5-5) Consumable electrode remelted Solution treated and precipitation treat

3、ed Sheet and strip a16mm 1 070 MPa I Rm 5 I 220 MPa Srie arospatiale Luft- und Raumfahrt Acier FE-PMI 802 (XSCrNiCul5-5) Refondu a llectrode consommable Mis en solution et vieilli Tles et bandes Stahl FE-PMI802 (X5CrNiCul5-5) Mit selbstverzehrender Elektrode umgeschmolzen Lsungsgeglht und ausgelager

4、t Bleche und Bnder as6mm armm I 070 MPa 5 Rm 1 220 MPa I 070 MPa 5 Rm 5 I 220 MPa This Herospace Series“ Prestandard has been drawn up under the responsibilify of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA- Members. If has been tec

5、hnically approved by the experts of the concerned Technical Committee following comment by fhe Member countries. Subsequent to the publication of this Prestandard, the fechnical content shall not be changed to an exfent that interchangeabilify is affected, physically or functionally, without re-iden

6、fification of the standard. Affer examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of fhe Official Services of the Member countries if will be submitted as a dran European Standard to CEN (European Cornmittee for Standardization) for formal vote. Edition app

7、roved for publication 1 Comments should be sent within six months after the date of publication to C5 Chairman 2000-05-31 AECMA Gulledelle 94 6-1200 BRUXELLES Mr Evetts COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD.AECMA PREN 3361

8、-ENGL 2000 1111 LOL23LL 0038357 064 1111 Page 3 prEN 3361: 2000 O 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

9、-5. 1 Scope This standard specifies the requirements relating to: Steel FE-PM1802 (XSCrNiCul5-5) Consumable electrode remelted Solution treated and precipitation treated Sheet and strip almm 1 070 MPa I R, I 1 220 MPa for aerospace applications. 2 Normative references This European Standard incorpor

10、ates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European

11、 Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 2043 Aerospace series - Metallic materials - General requirements for semi-finished product qualification (excluding forgings and castings) 1) EN 2951

12、 Aerospace series - Metallic materials - Test method - Micrographic determination of content of non-metallic inclusions 1) EN 4235-2 Aerospace series - Steel - Wrought products - Technical specification - Part 2: Plate, sheet and strip 1) EN 4258 Aerospace series - Metallic materials - General organ

13、ization of standardization - Links between types of EN standards and their use EN 4500-5 Aerospace series - Metallic materials - Rules for the drafting and presentation of material standards - Part 5: Specific rules for steel 1) 1) Published as AECMA Prestandard at the date of publication of this st

14、andard Previous page is blank COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling Services STD.AECMA PREN 33bL-ENGL 2000 M L0323LL 0038358 TLO Page 4 prEN 3361: 2000 4.2 Method of production 4.3 Limit dimension(s) mm 5 Technical specification Cold

15、rolled a16 EN 4235-2 6.1 Delivery condition Solution treated Heat treatment 1 025C 5 0s 1 055 “C I30 5 t 5 40 min IAC or OQ + COOI to es 30 oc 16.2 I Delivery condition code I W I U I Solution treated and precipitation treated 1 025C s s 055 “C I30 st I 40 min IAC or OQ + 535C 81 565 “CI t 24 h /AC

16、+ COOI to es 30 OC 7 Use condition Solution treated and precipitation treated Heat treatment Delivery condition + 535 “CI 6% 565 “CI t 2 4 h /AC Characteristics Delivery condition - 8.1 8.2 8.3 9 I I I I I - - o Thickness of cladding on each face % Test sample(s) See EN 4235-2 Test piece) See EN 423

17、5-2 Heat treatment Solution treated Use condition Dimensions concerned mrn a I 2,8 2,8a56 a 16 I 17 I Hardness I 363HBori383HV 1 s363HBors383HV I 34s HRC I39 ; 335 i HVi 385 18 19 Shear strength Rc MPa - - - Bending k- 18 ; a = 180 1) - 20 21 il Impact strength - Temperature I e1.c - I22 I ITime 23

18、Stress ua MPa - 24 Elongation a% - 25 Rupturetress oR MPa - 26 Elongation at A% - 27 Notes (see line 98) 1) -c - -. rupture lhl COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD.AECMA PREN 33bL-ENGL 2000 LOL23LL 0018359 953 Page 5 prE

19、N 3361: 2000 7 - licrostructure The 6 ferrite content shall not exceed 2 % See EN 4235-2 xternal defects 1 - 1 7 :leanliness/inclusion content nicro-cleanness) Visual See EN 4235-2 EN 2951 Category 4 Marking - - Dimensional inspection I) To be agreed between manufacturer and purchaser. Notes Typical

20、 use -I See EN 4235-2 See EN 4235-2 -I -I See EN 4235-2 I - -I COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTDOAECMA PREN 33bL-ENGL 2000 LOL2311 0018360 b79 Page 6 prEN 3361: 2000 Product qualification See EN 2043 - Qualification programme to be agreed between manufacturer and purchaser. COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling Services