ImageVerifierCode 换一换
格式:PDF , 页数:5 ,大小:136.06KB ,
资源ID:421234      下载积分:2000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
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   
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-421234.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 4289-1998 Aerospace Series Aluminium Alloy AL-P7175- Forging Stock Edition P 1《航空系列 铝合金AL-P7175锻造.P1版》.pdf)为本站会员(jobexamine331)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 4289-1998 Aerospace Series Aluminium Alloy AL-P7175- Forging Stock Edition P 1《航空系列 铝合金AL-P7175锻造.P1版》.pdf

1、STD*AECMA PREN Li289-ENGL 1998 10LZ311 0014559 05T Edition approved for publication AECMA STANDARD NORME AECMA AECMA NORM Comments should be sent within six months after the date of Dublication to C5 Chairman prEN 4289 Edition P 1 April 1998 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTR

2、IES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. +32) 2 775 81 11 ICs: Descriptors: ENGLISH VERSION Aerospace series Aluminium alloy AL-P7 1 75- Forging stock Srie arospatiale Alliage daluminium AL-P7175- Produits destins la forge Luft- und Raumfahrt Aluminiumlegierung AL

3、-P7175- Schmiedevormaterial This “Aerospace 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 Tech

4、nical Committee following comment by 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 sign

5、ature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Cornmittee for Standardization) for formal vote. 1998-04-30 AECMA Gulledelle 94 Mr Evetts I B-1200 BRUXELLES I ae

6、cma 1998 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 4289: 1998 O Introduction This standard is part of the series of EN metallic mater

7、ial standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-2. 1 Scope This standard specifies the requirements relating to: Aluminium alloy AL-P7175- Forging stock for aerospace applications. 2

8、 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 references, subsequent amendments to or revision

9、s 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 2043 EN 2070-3 EN 2070-7 EN 2082-2 EN 4258 EN 4500-2 Aerospace series - Metallic materials - Gene

10、ral requirements for semi-finished product qualification (excluding forgings and castings) 1) Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification - Part 3: Bar and section Aerospace series - Aluminium and aluminium alloy wrought products - Technical specificat

11、ion - Part 7: Wrought forging stock Aerospace series - Aluminium alloy forging stock and forgings - Technical specification - Part 2: Forging stock Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use 1) Aerospace series

12、- Metallic materials - Rules for drafting and presentation of material standards - Part 2: Specific rules for aluminium, aluminium alloys and magnesium alloys 1) 1) Published as AECMA Prestandard at the date of publication of this standard Previouc page is blank Copyright Association Europeene des C

13、onstructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Material designation 6.1 Aluminium alloy AL-P7175 Delivery condition 03 F Heat treatment - - Form Ingot or billet Rod, bar or section Method

14、 of production Cast Extruded Limit dimension(s) mm al I O00 a I 400 Technical specification EN 2082-2 EN 2070-7 6.2 7 Delivery condition code U U Use condition 03 F Heat treatment Delivery condition Delivery condition 8.1 8.2 8.3 9 Characteristics Test sample(s) See EN 2082-2 See EN 2070-7 Test piec

15、e(s) See EN 2082-2 See EN 2070-7 Heat treatment T73 (see line 29) T73 (see line 29) Dimensions concerned mm See EN 2082-3 a or D s 400 Thickness of cladding on lo I each face - % - 1 I 12 13 14 15 16 - - - - I 17 I Hardness I - Direction of test piece L L Temperature e OC Ambient Ambient Proof stres

16、s %,2 MPa 2385 2385 l) T Strength R, MPa 2455 1) 2455 1) Elongation A% 27 1) 27 1) Reductionofarea Z % - I18 I Shearstrength I R, IMPal - Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking perm

17、itted without license from IHS-,-,-eference heat treatment - - xternal defects See EN 2070-7 or EN 2082-2 See EN 2070-7 or EN 2082-2 lacrostructure iternal defects Marking inspection Dimensional inspection Notes Typical use Page 5 prEN 4289: 1998 Forged test pieces (cast stock) or delivery condition

18、 (extruded section) + 460 “C 5 8s 480 “C / WQ Os 80 “C 2, + 100 “C c Oc 120 “C I6 h 5 t 5 24 h + 170 “C c Oc 182 “C I6 h 5 t 5 18 h See EN 2070-7 or EN 2082-2 See EN 2070-7 51 Extruded forging stock Back end defects : see EN 2070-7 Peripheral coarse grain : level A (as per EN 2070-3) See EN 2070-7 o

19、r EN 2082-2 1) The “capability clause“ applies. 2) The use of quench additives or higher quenchant temperature shall be subject to agreement between manufacturer and purchaser. - -I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot

20、for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 prEN 4289: 1998 Product qualification See EN 2043 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-,-,-

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