ImageVerifierCode 换一换
格式:PDF , 页数:5 ,大小:192.54KB ,
资源ID:709922      下载积分:10000 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-709922.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(EN 2326-1992 en Aluminium Alloy AL-P6082-T6 Extruded Bars and Sections a or D Less Than or Equal to 200 mm《航空航天系列 AL-P6082-T6铝合金 a D≤200mm挤压棒和型材》.pdf)为本站会员(刘芸)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!

EN 2326-1992 en Aluminium Alloy AL-P6082-T6 Extruded Bars and Sections a or D Less Than or Equal to 200 mm《航空航天系列 AL-P6082-T6铝合金 a D≤200mm挤压棒和型材》.pdf

1、CEN EN*232b 92 m 3404589 0033487 89b a EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2326 September 1992 UDC: 669.715-42 629.7 Key words: Aircraft industry, metal bars, metal sections, aluminium alloys, specifications, chemical composition, dimensions, characteristics English version Aerospac

2、e series Aluminium alloy AL-P6082-T6 Extruded bars and sections a or D 5 200 mm Srie arospatiale Luft- und Raumfahrt Alliage d?aluminium AL-P6082-T6 Aluminiumlegierung AL-P6082-T6 Barres et profils fils a ou D I 200 mm StranggepreBte Stangen und Profile a oder D I 200 mm This European Standard was a

3、pproved by CEN on 1992-03-09. CEN members are bound to comply with the CENKENELEC Internal Regulations 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 s

4、tandards may be obtained on application to the Central Secretariat or to any CEN member. This 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

5、 to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. C

6、EN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels O 1992 Copyright reserved to CEN members Ref. Nr. EN 2326 : 1992 E CEN ENr232b 92 D 3404589 0033488 722 b Page 2 1 EN 2326 : 1992 Foreword

7、This European Standard has been prepared by the European Association of Aerospace Manufacturers ( AECMA) . After inquiries and votes carried out in accordance with the rules of this Association, this Standard has successively received the approval of the National Associations and the Official Servic

8、es of the member countries of AECMA, 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 March 1993, and conflicting national standards shall be withdrawn at the late

9、st by March 1993. In accordance with the Common CENICENELEC Rules the foliowing countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and Uni

10、ted Kingdom. CEN ENx2326 92 3404589 0033489 669 = Page 3 EN 2326 : 1992 O Introduction For the use of this standard, see EN 2500-2. 1 Scope This standard specifies the requirements relating to extruded bars and sections in aluminium alloy AL-P6082-, for use in the T6 condition, a or D 5 200 mm, for

11、aerospace applications. 2 References This European Standard incorporates 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 amendment

12、s 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 edition of the publication referred to applies. EN 2047 EN 2048 EN 2049 EN 2050 EN 2070-3 EN 2134 EN 2341 EN 2500-2 EN 2600 Beaded L

13、-section aluminium alloy extrusions - Dimensions - Aerospace series L-section aluminium alloy extrusions - Dimensions - Aerospace series I) Channel section aluminium alloy extrusions - Dimensions - Aerospace series 1 T-section aluminium alloy extrusions - Dimensions - Aerospace series Aerospace seri

14、es - Aluminium and aluminium alloy wrought products - Technical specification - Part 3 - Bars and sections Round aluminium alloy bars - Dimensions - Aerospace series Aluminium and aluminium alloy square and rectangular extruded bars - Dimensions - Aerospace series Aerospace series - Instructions for

15、 the drafting and use of metallic material standards - Pan 2 - Specific requirements for aluminium, aluminium alloys and magnesium alloys 2, Aerospace series - Designation of metallic semi-finished products - Rules 21, 11 Published as AECMA standard at the date of publication of this standard. 21 Pu

16、blished as AECMA pre-standard at the date of publication of this standard. CEN EN+232b 92 = 3404589 0033490 380 = Maienal dciipniiion Page 4 EN 2326 : 1992 Aluminium ailoy AL-WO82- r; 2 II Eiemni si Fe Cu Mn Mg Cr Zn Ti Well Chemical comporition Each Toul Al 0.40 0,6 BiU 46 min. 0.7 lMX. 1.3 0.50 0.

17、10 1.0 1,2 0.2 0.20 0.10 0.05 0.15 4 S Form Bin and Uctiona Method of production Ennidcd Limit dimcniiona (mm) S.1 Technical apecificaiion EN 2070-3 5.2 Dimcnaionri riandadi rorD 5 200 EN 2047. W 2048. EN 2049, EN 2050. EN 2134, EN U41 6.1 Deiivery condition and hei: truiment 6.2 Delivery condition

18、code Ur condition and hut ru:ment T6 525C 585540CIWQ0S40C + 160*C 5 8 5 180T16h it S30h U T6 Delivery condition Sample Teat piece Hut trmlinent Ur condition: T6 20 a or D 5 150 150 aorD 5200 9 DmcMonsconcemd mm 8 Of D 5 20 10 Thicknerr of cladding on 96 uch face 11 Direction of lest piccc L 12 empem

19、tu e *C Ambient tampenturn - 13 Proofstrnu 9.2 MPa 2 255 2 270 2 240 20 impact mrrngth 21 Tcmpeniurc 8 Oc - 22 Time h u StfCS8 Ja MPa 24 c Elongation a R. 25 Ruptunnrru JR MPa 26 Elongation ai A I - - - _I NptUm 27 Notes (ice line 98) 1) CEN EN*232b 92 9 3404589 0033491 217 9 7 1 7 nnul defecu _ Bac

20、k end defects : see EN 2070-3 Se EN 2070-3 Se EN 2070-3 Electrical conductivity y = 27 MSh (typical value) kkh uniformity 7 Hardness DsUgnrtion 95 HB (typical value) 6 S 20 HB per product A 4 30 HB per batch Noies Typical UIC Page 5 EN 2326 : 1992 -1 - See EN 2070-3 For extruded bars, see EN 2600. For extruded sections, see relevant drawing. i) or A, mm 2 7 96 for a 5 10 mm

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