《BS EN 2817-2009 航空航天系列.FE-PM1802 (X5CrNiCu15-5)型钢.自耗电极熔融.溶解处理和沉淀处理.机械用棒材.a-D≤200mm.Rm≥.pdf》由会员分享，可在线阅读，更多相关《BS EN 2817-2009 航空航天系列.FE-PM1802 (X5CrNiCu15-5)型钢.自耗电极熔融.溶解处理和沉淀处理.机械用棒材.a-D≤200mm.Rm≥.pdf（10页珍藏版）》请在三一文库上搜索。
1、- - This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 January 2010 - - EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2817 November 2009 ICS 49.025.10 English Version Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable elect
2、rode remelted - Solution treated and 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 - Stah
3、l FE-PM1802 (X5CrNiCu15-5) - Mit selbstverzehrender Elektrode umgeschmolzen - Lsungsgeglht und ausgelagert - 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 R
4、egulations which stipulate the conditions for giving this 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. T
5、his European Standard exists in three official versions (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 ar
6、e the national standards bodies of Austria, Belgium, Bulgaria, 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, Switze
7、rland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION 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. E
8、N 2817:2009: E - - EN 2817:2009 (E) 2 Foreword This document (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
9、 the approval of the National Associations and the Official 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
10、 conflicting national standards shall be withdrawn at the latest 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. Accordin
11、g to the CEN/CENELEC Internal Regulations, the national standards 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,
12、Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. - - EN 2817:2009 (E) 3 Introduction This European Standard is part of the series of EN metallic material standards for aerospace applications. The gene
13、ral organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-5. - - 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 preci
14、pitation treated Bar for machining 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
15、 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 4258, Aerospace series Metallic materials General organization of standardization Links be
16、tween types of EN standards and their use EN 4436, Aerospace series Steel Test methods Determination of ferrite content 1) EN 4500-5, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 5: Specific rules for steels 1) EN 4700-002, Aerospace series Steel
17、 and heat resisting alloys Wrought products Technical specification Part 002: Bar and section 1) 1) Published as ASD-STAN Prestandard at the date of publication of this standard. - - EN 2817:2009 (E) 5 1 Material designation Steel FE-PM1802 (X5CrNiCu15-5) 2 Chemical composition % Element C Si Mn P S
18、 Cr Mo Ni Cu Nb Ta Fe min. 14,0 3,5 2,5 5 C Base max. 0,07 1,00 1,00 0,030 0,015 15,5 0,50 5,5 4,5 0,45 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 6.1 Delivery condition Solution tre
19、ated Solution treated and precipitation treated 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 U 7 Use condition Solution treated and precipitation treated Delivery cond
20、ition Heat treatment 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 %
21、 11 Direction of test piece L L T 12 T 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 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 Be
22、nding k 20 Impact 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 C Temperature C 22 Time h 23 Stress a MPa 24 Elongation a % 25 Rupture stress R MPa 26 Elongation at rupture A % 27 Notes (see line 98) - - EN 2817:2009 (E) 6 30 M
23、icrostructure 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 4700-2.
24、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 - - EN 2817:2009 (E) 7 100 Product qualification See EN 2043. Qualification programme to be agreed between manufacturer and purchaser. - - - -