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

    SAE AMS 4049M-2016 Aluminum Alloy Sheet and Plate Alclad 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075 -T6 Sheet - T651 Plate) Solution and Precipitation Heat Treated (UNS A97075).pdf

    • 资源ID:1021334       资源大小:86.51KB        全文页数:6页
    • 资源格式: PDF        下载积分:10000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10000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。

    SAE AMS 4049M-2016 Aluminum Alloy Sheet and Plate Alclad 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075 -T6 Sheet - T651 Plate) Solution and Precipitation Heat Treated (UNS A97075).pdf

    1、_ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSX EOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDODQGHQJL neering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the VROHUHVS

    2、RQVLELOLWRIWKHXVHU SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2016 SAE International All rights reserved. No part of this publication may be reproduced

    3、, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776

    4、-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4049M AEROSPACE MATERIAL SPECIFICATION AMS4049 REV. M Issued 1951-10 Reaffirmed 2008-05 Revised 2016-06 Su

    5、perseding AMS4049L Aluminum Alloy, Sheet and Plate, Alclad 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075; -T6 Sheet - T651 Plate) Solution and Precipitation Heat Treated (Composition similar to UNS A97075) RATIONALE AMS4049M revises Condition (3.2.1, 3.2.2), Properties (3.3.5), deleted the weight limi

    6、t previously applicable to ultrasonic inspection (3.4), revised Reports (4.4.1), and is a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of sheet and plate with thickness from 0.008 to 4.000 inch, incl (0.20 to 101.6 mm, i

    7、ncl), clad on two sides (see 8.4). 1.2 Application These products have been used typically for structural use, including machined parts subject to excessive warpage during machining, but usage is not limited to such applications. 1.2.1 Certain design and processing procedures may cause these product

    8、s to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may

    9、work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. SAE INTERNATIONAL AMS4049M Page 2 of 6 2.1 SAE Publication

    10、s Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2355 Quality Assurance, Sampling and Testing, Aluminum Alloys and Magnesium Alloy, Wrought Products (Except Forging Stock

    11、), and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials ARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 2.2 ASTM Publications Available fro

    12、m ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B594 Ultrasonic Inspection of Aluminum Alloy Products for Aerospace Applications ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identifi

    13、cation Marking of Aluminum and Magnesium Alloy Products 2.3 ANSI Accredited Publications Copies of these documents are available online at http:/webstore.ansi.org/. ANSI H35.1/H35.1M Alloy and Temper Designation Systems for Aluminum ANSI H35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H

    14、35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1 and Table 2, determined in accordance with AMS2355. Table 1 - Composition, core (7075) Element min max Silicon - 0.40 Iron - 0.50 Cop

    15、per 1.2 2.0 Manganese - 0.30 Magnesium 2.1 2.9 Chromium 0.18 0.28 Zinc 5.1 6.1 Titanium - 0.20 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder SAE INTERNATIONAL AMS4049M Page 3 of 6 Table 2 - Composition, cladding (7072) Element min max Silicon + Iron - 0.7 Copper - 0.10

    16、Manganese - 0.10 Magnesium - 0.10 Zinc 0.8 1.3 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder 3.2 Product shall be supplied in the following condition; heat treatment shall be performed in accordance with AMS2772. 3.2.1 Sheet Solution and precipitation heat treated to th

    17、e T6 temper (see ANSI H35.1/H35.1M). 3.2.2 Plate Solution heat treated, stretched to produce a nominal permanent set of 2%, but not less than 1-1/2%, nor more than 3%, and precipitation heat treated to the T651 temper (see ANSI H35.1/H35.1M). 3.2.2.1 Plate shall receive no further straightening oper

    18、ations after stretching. 3.3 Properties 3.3.1 The product shall conform to the following requirements, determined in accordance with AMS2355. 3.3.2 Tensile Properties Shall be as shown in Table 3. Table 3A - Minimum tensile properties, inch/pound units Nominal Thickness Inches Tensile Strength ksi Y

    19、ield Strength at 0.2% Offset ksi Elongation in 2 inches or 4D % 0.008 to 0.011, incl 68.0 58.0 5 Over 0.011 to 0.039, incl 71.0 61.0 8 Over 0.039 to 0.062, incl 72.0 62.0 9 Over 0.062 to 0.187, incl 74.0 64.0 9 Over 0.187 to 0.249, incl 76.0 65.0 9 Over 0.249 to 0.499, incl 75.0 65.0 9 Over 0.499 to

    20、 1.000, incl 78.0 68.0 7 Over 1.000 to 2.000, incl 77.0 67.0 6 Over 2.000 to 2.500, incl 76.0 64.0 5 Over 2.500 to 3.000, incl 72.0 61.0 5 Over 3.000 to 3.500, incl 71.0 58.0 5 Over 3.500 to 4.000, incl 67.0 54.0 3 SAE INTERNATIONAL AMS4049M Page 4 of 6 Table 3B - Minimum tensile properties, SI unit

    21、s Nominal Thickness Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation % in 50 mm 0.20 to 0.28, incl 469 400 5 Over 0.28 to 0.99, incl 490 420 8 Over 0.99 to 1.57, incl 496 427 9 Over 1.57 to 4.75, incl 510 441 9 Over 4.75 to 6.32, incl 524 448 9 Over 6.32 to 12.67, incl 5

    22、17 448 9 Over 12.67 to 25.40, incl 538 469 - Over 25.40 to 50.80, incl 531 462 - Over 50.80 to 63.50, incl 524 441 - Over 63.50 to 76.20, incl 496 420 - Over 76.20 to 88.90, incl 490 400 - Over 88.90 to 101.60, incl 462 372 - 3.3.3 Bending Product shall withstand, without cracking, bending at room t

    23、emperature through an angle of 180 degrees around a diameter equal to the bend factor shown in Table 4 times the nominal thickness of the product with axis of bend parallel to the direction of rolling. Table 4 - Bending parameters Nominal Thickness Inches Nominal Thickness Millimeters Bend Factor 0.

    24、008 to 0.020, incl 0.20 to 0.51, incl 6 Over 0.020 to 0.063, incl Over 0.51 to 1.60, incl 7 Over 0.063 to 0.091, incl Over 1.60 to 2.31, incl 8 Over 0.091 to 0.125, incl Over 2.31 to 3.18, incl 9 Over 0.125 to 0.249, incl Over 3.18 to 6.32, incl 10 Over 0.249 to 0.499, incl Over 6.32 to 12.67, incl

    25、12 3.3.4 Cladding Thickness After rolling, the average cladding thickness per side shall be as shown in Table 5. Table 5 - Minimum average cladding thickness Total Thickness of Composite Product Inches Total Thickness of Composite Product Millimeters Average Cladding Thickness Per Side % of Thicknes

    26、s minimum Average Cladding Thickness Per Side % of Thickness maximum 0.008 to 0.062, incl 0.20 to 1.57, incl 3.2 - Over 0.062 to 0.187, incl Over 1.57 to 4.75, incl 2.0 - Over 0.187 to 0.499, incl Over 4.75 to 12.67, incl 1.2 - Over 0.499 to 4.000, incl Over 12.67 to 101.60, incl 1.2 3.0 SAE INTERNA

    27、TIONAL AMS4049M Page 5 of 6 3.3.5 Mechanical property requirements for product outside the range covered by Table 3 shall be agreed upon between purchaser and producer. 3.4 Quality The product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign material

    28、s and from imperfections detrimental to usage of the plate. 3.4.1 When specified, each plate 0.500 inch (12.70 mm) and over in nominal thickness shall be ultrasonically inspected in accordance with ASTM B594 and shall meet the requirements of Table 6 as applicable. Table 6 - Ultrasonic class Nominal

    29、 Thickness Inches Nominal Thickness Millimeters Ultrasonic Class Over 0.500 to 1.500, excl Over 12.70 to 38.10, excl B Over 1.500 to 3.000, incl Over 38.10 to 76.20, incl A Over 3.000 to 4.000, incl Over 76.20 to 101.60, incl B 3.5 Tolerances Shall conform to all applicable requirements of ANSI H35.

    30、2 or ANSI H35.2M. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection 7KHSURGXFHURIWKHSURGXFWVKDOOVXSSODOOVDPSOHVIRUSURGXFHUVWHVWVDQGVKDOOEH UHVSRQVLEOHIRUWKH performance of all required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necess

    31、ary to ensure that the product conforms to specified requirements. 4.2 Classification of Tests 4.2.1 Acceptance Tests Composition (3.1), tensile properties (3.3.1), and tolerances (3.5) and when specified UT inspection (3.4.1) are acceptance tests and, except for core composition, shall be performed

    32、 on each inspection lot. 4.2.2 Periodic Tests Bending (3.3.2) and cladding thickness (3.3.3) are periodic tests and shall be performed at a frequency selected by the producer unless frequency of testing is specified by purchaser. 4.3 Sampling and Testing Shall be in accordance with AMS2355. 4.4 Repo

    33、rts The producer of the product shall furnish with each shipment a report stating that the product conforms to the composition requirements and tolerances and showing the numerical results of tests on each inspection lot to determine conformance to the other acceptance test requirements. This report

    34、 shall include the purchase order number, inspection lot number, AMS4049M, size, and quantity. The report shall include the identity of the producer and the size of the mill product. 4.4.1 When the product size is outside the range covered by 1.1, the report shall contain a statement to that effect.

    35、 SAE INTERNATIONAL AMS4049M Page 6 of 6 4.5 Resampling and Retesting Shall be in accordance with AMS2355. 5. PREPARATION FOR DELIVERY 5.1 Identification Shall be in accordance with ASTM B666/B666M. 5.2 Packaging 5.2.1 Product shall be protected from damage during storage and shipment by a method det

    36、ermined by producer unless specified by purchaser. Examples of typical protective methods include but are not limited to interleaving with paper or oiling of the surface. 5.2.2 The product shall be prepared for shipment in accordance with ASTM B660 and in compliance with applicable rules and regulat

    37、ions pertaining to the handling, packaging, and transportation of the product to ensure carrier acceptance and safe delivery. 6. ACKNOWLEDGMENT A producer shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. 7. REJECTIONS Material

    38、not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection. 8. NOTES 8.1 Revision Indicator A change bar (l) located in the left margin is for the convenience of the user in locating areas where technical revisions, not editorial changes, have bee

    39、n made to the previous issue of this document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revisions. Change bars and (R) are not used in original publications, nor in documents that contain editorial changes only. 8.2 Terms used

    40、 in AMS are clarified in ARP1917. 8.3 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions and properties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information. 8.

    41、4 Purchase documents should specify not less than the following: AMS4049M Product form and size of product desired Property and acceptance requirements from the cognizant engineering organization applicable to sizes outside the range shown in 1.1. Quantity of product desired. PREPARED BY AMS COMM,77(


    注意事项

    本文(SAE AMS 4049M-2016 Aluminum Alloy Sheet and Plate Alclad 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075 -T6 Sheet - T651 Plate) Solution and Precipitation Heat Treated (UNS A97075).pdf)为本站会员(visitstep340)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