1、STD-AECMA PREN 3511-ENGL 1797 10L23LL 001b21 282 Edition approved for publication 1999-03-31 AECMA STANDARD NORME AECMA AECMA NORM Comments should be sent within six months after the date of publication to AECMA Gulledelle 94 8-1200 BRUXELLES prEN 3511 Edition P 2 March 1999 ! ICs: I Descriptors: PU
2、BLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 Supersedes edition PI March 1988 ENGLISH VERSION Aerospace series Steel FE-PLI 801 (1 00Cr6) Vacuum induction melted and consumable electrode remelte
3、d Softened Bar for the manufacture of machined bearings aor DI 130 mm Srie arospatiale Acier FE-PLI801 (100Cr6) labor sous vide par induction et refondu llectrode consommable Adouci Barres pour usinage destines la fabrication de roulements a ou D 5 130 mm Luft- und Raumfahrt Stahl FE-PLI801 (100Cr6)
4、 Vakuuminduktionserschmolzen und mit selbstverzehrender Elektrode umgeschmolzen Geg I ht Stangen zur spanenden Bearbeitung zur Fertigung von Wlzlagern a oder 130 mm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industri
5、es). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an exte
6、nt that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draff European St
7、andard to CEN (European Cornmittee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N A.E. Technopolis 54 - 199. rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX C5 Chairman Mr Evetts aecma 1999 Page 3 prEN 3511: 1999 O Introduction This standard is part of t
8、he 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. I Scope This standard specifies the requirements relating to: Steel FE-PL1801 (1 00Cr6) Vacuum induct
9、ion melted and consumable electrode remelted Softened Bar for the manufacture of machined bearings a or D I 130 mm for aerospace applications. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are c
10、ited 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 Standard only when incorporated in it by amendment or revision. For undated references the latest edit
11、ion of the publication referred to applies. EN 2043 Aerospace series - EN metallic materials - Wrought products - General requirements for product qualification 1) FE-PL 1801 (lOOCr6) 2) EN 3664-5 Aerospace series - Micrographic structure of steels for bearings - Part 5: Steel EN 4235-3 Aerospace se
12、ries - Steel - Wrought products - Technical specification - Pari 3: Bar and section 1) EN 4258 Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use Aerospace series - Metallic materials - Rules for drafting and presentati
13、on of material standards - Part 5: Specific rules for steel 1) EN 4500-5 1) Published as AECMA Prestandard at the date of publication of this standard 2) In preparation at the date of publication of this standard Previous page is blank STD-AECMA PREN 3511-ENGL 1799 LOL23Ll 001b123 055 Page 4 prEN 35
14、1 1: 1999 Delivery condition - 8.1 8.2 8.3 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 - - - - - - - - - _. - - - - - - - - - - - - Softened Delivery condition code Use condition Heat treatment I U Hardened and tempered Heat treatment Delivery condition + 820 “C c 0s 870 “CI OQ + 150 “C
15、5 Oc 190 “C i AC Characteristics Heat treatment Dimensions concerned rnm Thickness of cladding on yo each face Direction of test piece See EN 4235-3 See EN 4235-3 Test sample(s) Test piece(s) Delivery condition See line 29 a or D 5 130 De i 25 - - - Temperature Proof stress o “C - Ambient Rp0,2 MPa
16、- T Shear strength I Rc I MPa I - Strength R, MPa - - Elongation A Yo - Reduction of area Z YO - - Ha rd ness I Temperature I B I “C I - H- 229 HB 2 740 HV or 2 61 HRC Bending k- - Impact strength - Time h - C Stress oa MPa - Elongation a% Rupture stress rupture Elongation at MPa A Yo - Notes (see l
17、ine 98) *) 1) Reference heat treatment Microstructure Grain size External defects Cleanlinesslinclusion content (micro-cleanness) Macrostructure Decarburization Internal defects Marking inspection Dimensional inspection Notes Typical use - Hardened and tempered 820 “C I 0s 870 “C It 2 30 min / OQ +
18、150 “C 5 c 190 “C / t 2 2 h /AC 1 EN 3664-5 2 One per batch 7 Acceptance level shall be determined by agreement between manufacturer and purchaser See EN 4235-3 -I 50 mrn a or D 130 mm I 41 a or c 50 mm 71 G27 I G$6 - See EN 4235-3 - See EN 4235-3 Category 5 71 - See EN 4235-3 7 Class Condition Seve
19、rity I 1 I Freckles I A 2 White spots A 3 Radial segregation B I 4 I Ring pattern I C - See EN 4235-3 - See EN 4235-3 77 Class 5 - - See EN 4235-3 - See EN 4235-3 - *) p.p.m. 1) Hardened without temper the hardness indicated on line 17: HRC 2 63. The “capability clause“ applies. - Highly stressed bearing Page 6 prEN 351 1 : 1999 roduct qualification See EN 2043 Qualification programme to be agreed between manufacturer and purchaser
