SAE AMS 4375M-2017 Sheet and Plate Magnesium Alloy 3 0Al - 1 0Zn - 0 20Mn (AZ31B-O) Annealed and Recrystallized (UNS M11311).pdf
《SAE AMS 4375M-2017 Sheet and Plate Magnesium Alloy 3 0Al - 1 0Zn - 0 20Mn (AZ31B-O) Annealed and Recrystallized (UNS M11311).pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4375M-2017 Sheet and Plate Magnesium Alloy 3 0Al - 1 0Zn - 0 20Mn (AZ31B-O) Annealed and Recrystallized (UNS M11311).pdf(5页珍藏版)》请在麦多课文档分享上搜索。
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/AMS4375M AEROSPACE MATERIAL SPECIFICATION AMS4375 REV. M Issued 1947-07 Reaffirmed 1995-05 Rev
5、ised 2017-06 Superseding AMS4375L Sheet and Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-O) Annealed and Recrystallized (Composition similar to UNS M11311) RATIONALE AMS4375M revises the Title to correct the temper designation, revises Composition (Table 1), Condition (3.2), Properties (3.3.
6、3), Reports (4.4.1) and Identification, and is a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers a magnesium alloy in the form of sheet and plate from 0.016 to 3.000 inches (0.41 to 76.20 mm), inclusive, in thickness (see 8.4). 1.2 Application This prod
7、uct has been used typically for low-strength parts requiring rigidity with low density, 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 h
8、erein. The supplier may 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. 2.1 SAE Publications Available fro
9、m 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), and Rolled, Fo
10、rged, or Flash Welded Rings ARP1917 Clarification of Terms Used in Aerospace Metals Specifications SAE INTERNATIONAL AMS4375M Page 2 of 5 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.
11、ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identification Marking of Aluminum and Magnesium Products ASTM E9 Compression Testing of Metallic Materials at Room Temperature 2.3 ANSI Accredited Publications Copies of these documents are available online at http:/webs
12、tore.ansi.org/. ANSI H 35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H 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, determined in accordance with AMS2355. Table 1
13、- Composition Element Min Max Aluminum 2.5 3.5 Zinc 0.7 1.3 Manganese 0.20 1.0 Silicon - 0.05 Copper - 0.05 Calcium - 0.04 Iron - 0.005 Nickel - 0.005 Other Elements, each (3.1.1) - 0.10 Other Elements, total (3.1.1) - 0.30 Magnesium remainder 3.1.1 Determination not required for routine acceptance.
14、 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Annealed and recrystallized. SAE INTERNATIONAL AMS4375M Page 3 of 5 3.3 Properties The product shall conform to the following requirements: 3.3.1 Tensile Properties Shall be as specified in Table 2 and 3.3.1.1, determined
15、 in accordance with AMS2355 on the mill produced size. Table 2 Table 2A - Tensile properties Nominal Thickness Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi, Min Elongation in 2 inches or 4D %, Min 0.016 to 0.060, incl 32.0-40.0 18.0 12 Over 0.060 to 0.500, incl 32.0-40.0 15.0 12 Ove
16、r 0.500 to 2.000, incl 32.0-40.0 15.0 10 Over 2.000 to 3.000, incl 32.0-40.0 15.0 9 Table 2B - Tensile properties (SI) Nominal Thickness Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa, Min Elongation in 50.8 mm or 4D %, Min 0.41 to 1.52, incl 221-276 124 12 Over 1.52 to 12.70, in
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS4375M2017SHEETANDPLATEMAGNESIUMALLOY30AL10ZN020MNAZ31BOANNEALEDANDRECRYSTALLIZEDUNSM11311PDF

链接地址:http://www.mydoc123.com/p-1021582.html