ImageVerifierCode 换一换
格式:PDF , 页数:14 ,大小:658.83KB ,
资源ID:419955      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-419955.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 3114-4-1997 Aerospace Series Test Method Microstructure of (a + b) Titanium Alloy Wrought Products Part 4 Microstructure of Sheet for Superplastic Forming Edition P 1《航空.pdf)为本站会员(lawfemale396)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 3114-4-1997 Aerospace Series Test Method Microstructure of (a + b) Titanium Alloy Wrought Products Part 4 Microstructure of Sheet for Superplastic Forming Edition P 1《航空.pdf

1、 STD-AECMA PREN 3LL4-4-ENGL 1777 E 1012311 0013137 778 E AECMA STANDARD prEN 31 14-4 NORME AECMA Edition P 1 AECMA NORM July 1997 Edition approved for publication PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (

2、+32) 2 775 81 11 Comments should be sent within six months after the date of Dubiication to C5 Chairman ICs : Descriptors : ENGLISH VERSION Aerospace series Test method Microstructure of (a + l titanium alloy wrought products Part 4 : Microstructure of sheet for superplastic forming Srie arospatiale

3、 Mthode dessai Microstructure des produits corroys en alliage de titane (a + ) Partie 4 : Microstructure des tles pour formage superplastique Luft- und Raumfahrt Prf verfahren Mikrogefge von Titanlegierung (CL + ) Teil 4 : Mikrogefge Kneterzeugnisse von Blechen fr superplastisches Umformen This “Aer

4、ospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). 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

5、the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking

6、Centre INPSI and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. NOTE : Images of higher quality for the prints in this standard are available from BNAE. 1997-07-31 AE

7、CMA Gulledelle 94 B-1200 BRUXELLES Mr Odorico aecrna 1997 COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling Services1 Scope This standard contains pictures of the microstructure of (a + ) titanium alloy sheet for superplastic forming. It shall be

8、 used in conjunction with EN 31 14-1. 2 Normative 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 reference

9、s, 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 edition of the publication referred to applies. EN 31 14-1 Aerospace series - Microstructure of (a + ) titani

10、um alloy wrought products - Part 1 : General requirements 1) 3 Micrographs 4L1 A to 4L12A (a + ) structure, longitudinal section, annealed. 4L1B to 4L12B (a + ) structure, longitudinal section, 930C/t = 30 min/WQ. 1) Published as AECMA Prestandard at the date of publication of this standard Previous

11、 page is blank COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD*AECMA PREN 3114-4-ENGL 1777 W LOL23LL OOL3137 740 H Page 4 prEN 31 14-4 : 1997 (a + ) structure, longitudinal section Annealed 200 : 1 4L1 A 200: 1 930 OC / t = 30 min /

12、 WQ 4L1 B COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD-AECMA PREN 3114-Li-ENGL 1797 D LOL23LL 00131LiO Lib2 D Page 5 prEN 31 14-4 : 1997 (a + I structure, longitudinal section Annealed 200 : 1 4L2A 200 : 1 930 OC / t = 30 min / W

13、Q 4L2B COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD*AECMA PREN 3LL4-4-ENGL 1777 1012311 OOL3L41 3T7 Page 6 prEN 31 14-4 : 1997 (a + i structure, longitudinal section Annealed 200: 1 4L3A 200 : 1 930 OC / t = 30 min / WQ 4L3B COPY

14、RIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD-AECMA PREN 3LlLI-4-ENGL 1777 D LO123L1 OOL31LI2 235 Page 7 prEN 31 14-4 : 1997 (01 + I structure, longitudinal section Annealed 200: 1 4L4A 200: 1 930 OC / t = 30 min /WO 4L4B COPYRIGHT As

15、sociation Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD-AECMA PREN 3LL4-4-ENGL 2777 W LOL23Ll 0013LLi3 171 D Page 8 prEN 31 14-4 : 1997 (01 + ) structure, longitudinal section Annealed 200 : 1 4L5A 200: 1 93OOC / t = 30 min / WQ 4L5B COPYRIGHT Associat

16、ion Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD*AECMA PREN 3114-4-ENGL 1777 W 1012311 0013144 008 W Page 9 piEN 31 14-4 : 1997 (a + l structure, longitudinal section Annealed 200 : 1 4L6A 4L6B COPYRIGHT Association Europeene Des Constructeurs de Mate

17、riel AerospaceLicensed by Information Handling ServicesSTD*AECMA PREN 3114-4-ENGL 1777 m LOL23LL 0013145 Ti-14 m Page 10 prEN 31 14-4 : 1997 (a + ) structure, longitudinal section Annealed 200 : 1 4L7A 200: 1 930 OC / t = 30 min / WQ 4L7B COPYRIGHT Association Europeene Des Constructeurs de Materiel

18、 AerospaceLicensed by Information Handling ServicesPage 11 prEN 31 14-4 : 1997 (a + ) structure, longitudinal section 930 OC / t = 30 min /WO 4L8B 200 : 1 COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD-AECMA PREN 3LL4-4-ENGL 1997 1

19、0123L1 00131lr7 817 W Page 12 prEN 31 14-4 : 1997 (a + ) structure, longitudinal section 200 : 1 Annealed 4L9A 200: 1 930 OC / t = 30 min / WQ 4L9B COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD-AECMA PREN 311LI-4-ENGL 1997 9 30123

20、11 0033348 753 Page 13 prEN 31 14-4 : 1997 (a + l structure, longitudinal section Annealed 200: 1 4L1 OA 200 : 1 930 OC / t = 30 min / WQ 4L1 OB COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTDSAECMA PREN 311q-g-ENGL 1997 9 1012311 0

21、013149 b9T m Page 14 prEN 31 14-4 : 1997 (CL + i structure, longitudinal section Annealed 200: 1 4L11A 200: 1 930 OC / t = 30 min / WQ 4LllB COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesSTD-AECMA PREN 3114-4-ENGL 1777 D 1012311 0013L50 301 9 Page 15 prEN 31 14-4 : 1997 (a + ) structure, longitudinal section 200 : 1 Annealed 4L12A 200: 1 930 OC / t = 30 min / WQ 4L12B COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling Services

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