ImageVerifierCode 换一换
格式:PDF , 页数:12 ,大小:245.10KB ,
资源ID:419332      下载积分:5000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
注意:如需开发票,请勿充值!
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【http://www.mydoc123.com/d-419332.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: 微信登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(AECMA PREN 2540-1997 Aerospace Series Steel FE-PM3902 (X7CrNiAl17-7) Air Melted Solution Treated and Precipitation Hardened Sheet and Strip a Less Than or Equal to 6 mm 1 240 MPa L4.pdf)为本站会员(孙刚)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

AECMA PREN 2540-1997 Aerospace Series Steel FE-PM3902 (X7CrNiAl17-7) Air Melted Solution Treated and Precipitation Hardened Sheet and Strip a Less Than or Equal to 6 mm 1 240 MPa L4.pdf

1、Document ProjectNo. Committee ref IDCI 97/719216 97 5286 ACE115 Draft for Public Comment Latest date for receipt of comments 3nshRIc I4py Q c? I I Date I 16 NOVEMBER 1997 DRAFT EUROPEAN (AECMA) AEROSPACE STANDARD STEEL FE-PM3902 (X7CrNiA117-7) AIR MELTED SOLUTION TREATED AND PRECIPITATION HARDENED S

2、HEET AND STRIP a no acknowledgment will normally be sent. MR P RYDON Requests for purchase of further copies of thus draft shoula be sent to Customer Services, at the head office address below. Telephone 0181 996 7000, fax 0181 996 7QOI. THIS IS A DRAFT AND MUST NOT BE REGARDED OR USED AS A BRITISH

3、STANDARD Head office 389 Chiswick High Road London W4 4AL Telephone O181 996 9000 Fax 0181 996 7400 036-9108 AI JnFomJI Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without lice

4、nse from IHS-,-,-Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-BSI COMMITTEES TO WHOSE MEMBERS THIS DRAFT HAS ALSO BEEN SENT CONSTITUTION ORGANIZATIO

5、NS REPRESENTED - -_-_- BRITISH INVESTMENT CASTING TRADE ASSOCIATION CASTINGS DEVELOPMENT CENTRE CIVIL AVIATION AUTHORITY (AIRWORTHINESS DIVISION) CONFEDERATION OF BRITISH FORGERS INSTITUTE OF SPRING TECHNOLOGY MINISTRY OF DEFENCE SOCIETY OF BRITISH AEROSPACE COMPANIES LIMITED STAINLESS STEEL WIRE IN

6、DUSTRY ASSOCIATION U K STEEL ASSOCIATION - A2 - 97/719216 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Copyright Association Europeene des Construct

7、eurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-pr EN 2540 DRAFT EUROPEAN (AECMA) AEROSPACE STANDARD This DPC refers to a draft text currently at the PPN ballot stage within a technical committee

8、of AECMA (The European Association of Aerospace Industries) l. The voting period within the AECMA technical committee is exceptionally only one month from the date of dispatch of the originating document from BNAE, hence this will be completed well before the expiry of the DPC comment date. Any comm

9、ents received as a result of the DPC, after the expiry of the PPN ballot, will be reviewed by the relevant BSI committee and taken into account when they consider the UK view and vote on a possible BS EN publication. ) AECMA consists of the national aerospace trade associations from nine European co

10、untries, the UK member being SBAC ( Society of British Aerospace Companies). AECMA has been given a mandate by CEN to prepare all European Aerospace Standards on its behalf. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for Resa

11、leNo reproduction or networking permitted without license from IHS-,-,-5 7 f 7 1 92 i 6 OC Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-DRAFT prEN 2

12、540 Date : 10-97 Edition : P1 STUDY : C5 DRAWN“: 3 STAGE : 20 Ref.: EFA Superseding Ref.: ENGUSH VERSION Aerospace series Steel FE-PM3902 (X7CrNiAi17-7) Air meited Solution treated and precipitation hardened Sheet and strip as6mm 1 240 MPa s Rm s 1 450 MPa Srie arospatiale Acier FE-PM3902 (XCrNiAI17

13、-7) Elabore a Vair Mis en solution et durci par prcipitation Tles et bandes asmm 1 240 MPa s Rm 5 1 450 MPa Luft- und Raumfahrt Stahl FE-PM3902 (X7CrNiAll7-7) Lufterschmolzen Lsungsgeglht und ausgelagert Bleche und Bnder asmm 1 240 MPa s Rm s 1 450 MPa en CIfr CI de Master document : Sponsor : Mr. B

14、OlTOMLEY 1171 7 192 160c THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STXVDARDIZATION Gulledeie PI, B - 1200 Bruxelies Tel, : (32) 2 775 8110 Fax.: (32) 2 775 8111 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo

15、 reproduction or networking permitted without license from IHS-,-,-rage 2 prEN 2540 : 1997 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN

16、2540 : 1997 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 4500-5. 1 Scope This standard specifies the requirements

17、 relating to : Steel FE-PM3902 (X7CrNiAI17-7) Air melted Solution treated and precipitation hardened Sheet and strip asmm 1 240 MPa s R, s 1 450 MPa for aerospace applications. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications

18、. 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 Standard only when incorporated in it by amendment or revision. For

19、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) l) EN 4235-2 Aerospace series - Steel wrought products - Technical specificatio

20、n - Part 2 : Plate, sheet and strip EN 4258 Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use l) EN 4500-5 Aerospace series - MetaUic materials - Rules for drafting and presentation of material standards - Part 5 : Spe

21、cific rules for steel 1) Published as AECMA Prestandard at the date of publication of this standard B Mi2 I I i OI97K6 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without licen

22、se from IHS-,-,-1 2 Material designation Steel FE-PM3902 (X7CrNiAll7-7) Chemical composition % Element C si Mn P S cr Cu Ni Al Fe - - - - min. - - 16.0 6.50 0,751 max. 0,09 1.00 1.00 0.040 0,030 18.0 0,50 7,75 1.50 . Base 3 4.1 5 I Technical specification I Method of melting Air melted Form Sheet an

23、d strip EN4235-2 4.2 4.3 Method of production Cold rolled Limit dimension(s) mm as6 I Heat treatment 0.1 1 025 “C s BO 1 055 CIt r 30 min1 AC or OQ I Delivery condition Solution treated 5.2 7 - Use condition Heat treatment Soluon treated and precipitation hardened Delivery condrton 740 “C s 6s 780 “

24、Clt a 90 min + cool to 8s 20 “C 1 within 1 h 1 hold for 30 min + 550 “CO BO 580 C/t r 90 min1AC Characteristics 3.1 3.2 Test sample(s) See EN 4235-2 Test piece(s) See EN 4235-2 3.3 9 - Heat treatment Ddiq condition Use condiuon Dimensions concerned mm as5 I 5cas6 as6 - - 11 I Direction of test piece

25、 I I I See EN 4235-2 I lo I - Thickness of cladding on % - - - I Ambient Proof stress MPa - Rm MPa - - Elongation A% 1 - a1 o35 - 1240iRms1450 r5 - -II I 16 17 Reductionofarea Z % - - - Hardness s229HV S229HV r 38 HRC 41 I i 8 19 Shear strength Re MPa - - - Bending k- 0,5 a = 180 o 1.5 a = 180 - 20

26、I impact strength I I A% I 27 1 Notes (see line 98) I I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 2540 : 1997 External defects larkin

27、g inspection hnensionai inspection lotes ypical use See EN 4235-2 I - -I See EN 4235-2 -I - I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 xE

28、N 2540 : 1997 Product qualification BMl2 Il l97K6 See EN 2043 Qualification programme to be agreed between manufacturer and purchaser. 4717 192 16oC Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
备案/许可证编号:苏ICP备17064731号-1