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 5532H-2017 Iron Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 30Fe - 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0Cb(Nb) - 0 15N Solution Heat Treated (UNS R30155).pdf

    • 资源ID:1021970       资源大小:251.59KB        全文页数:5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 5532H-2017 Iron Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 30Fe - 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0Cb(Nb) - 0 15N Solution Heat Treated (UNS R30155).pdf

    1、 _ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising ther

    2、efrom, is the sole responsibility of the user.” 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 2017 SAE International All rights reserved. No part of this

    3、publication may be reproduced, 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: +1 724-776-49

    4、70 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AMS5532H AEROSPACE MATERIAL SPECIFICATION AMS5532 REV. H Issued 1947-09 Reaffirmed 2012-07 Rev

    5、ised 2017-12 Superseding AMS5532G Iron Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 30Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb(Nb) - 0.15N Solution Heat Treated (Composition similar to UNS R30155) RATIONALE AMS5532H revises Reports (4.4) and Identification (5.1.1), and results

    6、from a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant iron alloy in the form of sheet, strip, and plate. 1.2 Application These products have been used typically for parts requiring high strength up to 1500 F (816 C) and o

    7、xidation resistance up to 1800 F (982 C), but usage is not limited to such applications. 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 work to a subsequent r

    8、evision 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. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, W

    9、arrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2242 Tolerances Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and Plate AMS2248 Chemical Check Analysis Limits Corrosion and Heat-Resista

    10、nt Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron Alloys SAE INTERNATIONAL AMS5532H Page 2 of 5 AMS2371 Quality Assurance Sampling and Testing Corrosion and Heat-Resistant Steels and Alloys Wrought Products and Forging Stock AMS2807 Identification Carbon and Low-Alloy Steels,

    11、Corrosion and Heat-Resistant Steels and Alloys Sheet, Strip, Plate, and Aircraft Tubing ARP1917 Clarification of Terms Used in Aerospace Metals Specifications AS4194 Sheet and Strip Surface Finish Nomenclature 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C

    12、700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM A480/A480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and Strip ASTM E8/E8M Tension Testing of Metallic Materials ASTM E139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials A

    13、STM E290 Bend Testing of Material for Ductility ASTM E354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical m

    14、ethods in accordance with ASTM E354, by spectrochemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element Min Max Carbon Manganese Silicon Phosphorus Sulfur Chromium Nickel Cobalt Molybdenum Tungsten Columbium (Niobium) Nitrogen Tantalum Copper Iron 0.08

    15、1.00 - - - 20.00 19.00 18.50 2.50 2.00 0.75 0.10 - - remainder 0.16 2.00 1.00 0.040 0.030 22.50 21.00 21.00 3.50 3.00 1.25 0.20 0.05 0.50 SAE INTERNATIONAL AMS5532H Page 3 of 5 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2248. 3.2 Condition The product sh

    16、all be supplied in the following condition: 3.2.1 Sheet and Strip Hot or cold rolled, solution heat treated, and, unless solution heat treatment is performed in an atmosphere yielding a bright finish, descaled, having a surface appearance in accordance with ASTM A480/A480M and AS4194 comparable to 3

    17、.2.1.1 or 3.2.1.2 as applicable. 3.2.1.1 Sheet No. 2D finish. 3.2.1.2 Strip No. 1 strip finish. 3.2.2 Plate Hot rolled, solution heat treated, and descaled. 3.3 Properties The product shall conform to the following requirements: 3.3.1 Tensile Properties Shall be as shown in Table 2, determined in ac

    18、cordance with ASTM E8/E8M. Table 2 - Room temperature tensile properties Property Value Tensile Strength Elongation in 2 inches (50.8 mm) or 4D, min 100 to 140 ksi (689 to 965 MPa) 40% 3.3.2 Bending Product 0.1874 inch (4.760 mm) and under in nominal thickness shall be tested in accordance with ASTM

    19、 E290 using a sample prepared nominally 0.75 inch (19.0 mm) in width with its axis of bending parallel to the direction of rolling and shall withstand, without cracking, when bending at room temperature through an angle of 180 around a diameter equal to the bend factor shown in Table 3 times the nom

    20、inal thickness of the product. In case of dispute, the results of tests using the guided bend test of ASTM E290 shall govern. Table 3 - Bending parameters Nominal Thickness Inch Nominal Thickness Millimeters Bend Factor Up to 0.050, incl Up to 1.27, incl 1 Over 0.050 to 0.125, incl Over 1.27 to 3.18

    21、, incl 2 Over 0.125 to 0.1874, incl Over 3.18 to 4.760, incl 3 SAE INTERNATIONAL AMS5532H Page 4 of 5 3.3.3 Stress-Rupture Properties at 1500 F (816 C) A tensile specimen, maintained at 1500 F 3 F (816 C 2 C) while a load sufficient to produce an initial axial stress of 18.0 ksi (124 MPa) or higher

    22、is applied continuously, shall not rupture in less than 24 hours. The test shall be continued to rupture without change of load. Elongation after rupture, measured at room temperature, shall be not less than 10% in 2 inches (50.8 mm) or 4D. Tests shall be conducted in accordance with ASTM E139. 3.3.

    23、3.1 The test of 3.3.3 may be conducted using incremental loading. In such case, the load required to produce an initial axial stress of 18.0 ksi (124 MPa) or higher shall be maintained to rupture or for 24 hours, whichever occurs first. After the 24 hours and at intervals of 8 hours minimum, thereaf

    24、ter, the stress shall be increased in increments of 2.0 ksi (14 MPa). Time to rupture and elongation requirements shall be as specified in 3.3.3. 3.4 Quality The product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfection

    25、s detrimental to usage of the product. 3.5 Tolerances Shall conform to all applicable requirements of AMS2242. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The producer of the product shall supply all samples for producers tests and shall be responsible for the performance of al

    26、l required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that the product conforms to specified requirements. 4.2 Classification of Tests All technical requirements are acceptance tests and shall be performed on each heat or lot as a

    27、pplicable. 4.3 Sampling and Testing Shall be in accordance with AMS2371. 4.4 Reports The producer of the product shall furnish with each shipment a report showing the producers name and the country where the metal was melted (e.g., final melt in the case of metal processed by multiple melting operat

    28、ions) and stating the product conforms to the composition, tolerances, and ultrasonic tests, and showing the numerical results of tests on each inspection lot to determine conformance to the other acceptance test requirements. This report shall include the purchase order number, inspection lot numbe

    29、rs, AMS5532H, size and quantity. The report shall also identify the producer, the product form, and the size of the mill product. 4.4.1 When material produced to this specification has exceptions taken to the technical requirements listed in Section 3 (see 5.1.1), the report shall contain a statemen

    30、t “This material is certified as AMS5532H(EXC) because of the following exceptions.” and the specific exceptions shall be listed. 4.5 Resampling and Retesting Shall be in accordance with AMS2371. SAE INTERNATIONAL AMS5532H Page 5 of 5 5. PREPARATION FOR DELIVERY 5.1 Identification Shall be in accord

    31、ance with AMS2807. 5.1.1 When technical exceptions are taken (see 4.4.1), the material shall be marked with AMS5532H(EXC). 5.2 Packaging The product shall be prepared for shipment in accordance with commercial practice and in compliance with applicable rules and regulations pertaining to the handlin

    32、g, 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 Product not conforming to this specific

    33、ation, or to modifications authorized by purchaser, will be subject to rejection. 8. NOTES 8.1 Revision Indicator A change bar (I) located in the left margin is for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of

    34、 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 in AMS are clarified in ARP191

    35、7. 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. 8.4 Unless otherwise specified, t

    36、he material producer shall work to the revision of AMS5532 in effect on the date of order placement. Unless otherwise specific, material manufactured and certified to the immediately previous revision of AMS5532 may be procured and used until inventory is depleted. 8.5 Purchase documents should specify not less than the following: AMS5532H Form and size of product desired Property and acceptance requirements from the cognizant engineering organization applicable to sizes outside the range listed in 1.1 Quantity of product desired PREPARED BY AMS COMMITTEE “F”


    注意事项

    本文(SAE AMS 5532H-2017 Iron Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 30Fe - 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0Cb(Nb) - 0 15N Solution Heat Treated (UNS R30155).pdf)为本站会员(livefirmly316)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