欢迎来到麦多课文档分享! | 帮助中心 海量文档,免费浏览,给你所需,享你所想!
麦多课文档分享
全部分类
  • 标准规范>
  • 教学课件>
  • 考试资料>
  • 办公文档>
  • 学术论文>
  • 行业资料>
  • 易语言源码>
  • ImageVerifierCode 换一换
    首页 麦多课文档分享 > 资源分类 > PDF文档下载
    分享到微信 分享到微博 分享到QQ空间

    AECMA PREN 3678-1999 Aerospace Series Steel FE-PM3801 (X5CrNiCu17-4) Air Melted Solution Treated and Precipitation Treated Forgings a or D Less Than or Equal to 200 mm Rm Greater T.pdf

    • 资源ID:420573       资源大小:195.13KB        全文页数:5页
    • 资源格式: PDF        下载积分:2000积分
    快捷下载 游客一键下载
    账号登录下载
    微信登录下载
    二维码
    微信扫一扫登录
    下载资源需要2000积分(如需开发票,请勿充值!)
    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)。
    如需开发票,请勿充值!如填写123,账号就是123,密码也是123。
    支付方式: 支付宝扫码支付    微信扫码支付   
    验证码:   换一换

    加入VIP,交流精品资源
     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。
    5、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。

    AECMA PREN 3678-1999 Aerospace Series Steel FE-PM3801 (X5CrNiCu17-4) Air Melted Solution Treated and Precipitation Treated Forgings a or D Less Than or Equal to 200 mm Rm Greater T.pdf

    1、STD.AECMA PREN 3678-ENGL L999 1012311 0016463 484 #l# Edition approved for publication Comments should be sent within six months after the date of publication to AECMA Gulledelle 94 1999-09-30 B-1200 BRUXELLES AECMA STANDARD NORME AECMA AECMA NORM C5 Chairman Mr Evetts prEN 3678 Edition P 1 Septembe

    2、r 1999 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledeiie 94 - 6-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 ICs: Descriptors: ENGLISH VERSION Aerospace series Steel FE-PM380 1 (X5CrN iC u I 7-4) Air melted Solution treated and precipitation treated

    3、 Forgings a or 5 200 mm Rm 2 930 MPa Srie arospatiale Acier FE-PM3801 (XSCrNiCu17-4) labor lair Mis en solution et vieilli Pices forges et pices matrices a or D I 200 mm Rm 2 930 MPa Luft- und Raumfahrt Stahl FE-PM3801 (XSCrNiCu17-4) Luftersc hmolzen Lsungsgeglht und ausgehrtet Schmiedestcke a or D

    4、I 200 mm Rm 2 930 MPa This Herospace 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 C

    5、ommittee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an exfenf fhaf inferchangeabihty is affected, physically or functiona/y, without re-iden fification of the standard. Affer examination and signature of

    6、 the AECMA Standard Checking Centre (NPS) and formal agreement of the Oficial Services of the Member countries it will be submitfed as a draff European Standard to CEN (uropean Committee for Standardization) for formal vote. Copyright Association Europeene des Constructeurs de Materiel Aerospatial P

    7、rovided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3678: 1999 O Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is descri

    8、bed 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-PM3801 (X5CrNiCu17-4) Air melted Solution treated and precipitation treated Forgings a or D I 200 mm R, 2 930 MPa for aerospace applications. 2 Norma t

    9、ive 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 amendments to or revisions of an

    10、y 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 2157-3 Aerospace series - Steel forging stock and forgings - Technical specification - Part 3: Pre- prod

    11、uction and production forgings EN 3163 Aerospace series - Steel FE-PM3801 (XSCrNiCu17-4) - Air melted - Softened - Forging stock - a or D I 300 mm 1) EN 4258 Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use EN 4500-5

    12、Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 5: Specific rules for steel 1) 1) Published as AECMA Prestandard at the date of publication of this standard Previous page is blank Copyright Association Europeene des Constructeurs de Materiel A

    13、erospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 3b78-ENGL 1999 W LO12311 0036465 257 5 Page 4 prEN 3678: 1999 Method of production Limit dimension(s) mm Technical specification 1 4 4.3 Forged from fo

    14、rging stock EN 3163 a or D : 200 EN 2157-3 I 025 “C5 Oc 1 055 “Clt 2 30 min /AC or OQ + COOI to es 30 OC -very condition 1 025C : Oc. 1 055 “Clt 230 min1 AC or OQ + COOI to es 30 oc + 610 “C I e 630 “CI t 2 4 h IAC I Solution treated I Solution treated and precipitation treated 6.2 7 Heat treatment

    15、Delivery condition code W U Use condition Solution treated and precipitation treated Delivery condition 8.1 1 Test sample(s) See EN 21 57-3 Heat treatment 8.2 8.3 I Delivery condition - + 610 “C I 630 “C It 2 4 h I AC I Test piece(s) See EN 2157-3 Heat treatment Solution treated Use condition Charac

    16、teristics 9 10 11 Dimensions concerned mm a or D c 200 a or DC 75 75 a or Ds 200 each face Thickness of cladding on % - - Direction of test piece - L L T - Proof stress Elongation Reduction of area e “C - Ambient Ambient Ambient - 2 725 2 725 2 725 Rp0,2 MPa R, MPa - 2 930 2 930 2 930 A% - 2 14 2 12

    17、 2 10 Z % - 2 50 2 50 2 35 19 20 21 22 23 24 25 - - - - 17 I Hardness Bending k- - - - Impact strength - W 2 40 J ; Notch direction T KV 2 20 J ; Notch direction T Temperature e OC - Time h - Stress aa MPa - C Elongation a Oh - Rupturestress aR MPa - 5 363 HB I 277cHB5352 I 277 5 HB 352 18 I Shear s

    18、trength I Rc I MPa I - 27 I 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-,-,-STD-AECMA PREN 367B-ENGL L999 W 1012311 OOLbYbb 193

    19、 - - - Page 5 prEN 3678: 1999 See EN 21 57-3 - - Grain size External defects Batch uniformity Marking inspection 3imencional inspection Votes rypical use See EN 21 57-3 Gr4 See EN 2 157-3 See EN 2157-3 See EN 2157-3 -I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provide

    20、d by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 3b78-ENGL h999 LOL23LL 00Lb4b7 02T Page 6 prEN 3678: 1999 Product qualification Qualification programme to be agreed between manufacturer and purchaser. 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-,-,-


    注意事项

    本文(AECMA PREN 3678-1999 Aerospace Series Steel FE-PM3801 (X5CrNiCu17-4) Air Melted Solution Treated and Precipitation Treated Forgings a or D Less Than or Equal to 200 mm Rm Greater T.pdf)为本站会员(postpastor181)主动上传,麦多课文档分享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档分享(点击联系客服),我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们

    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 

    收起
    展开