SAE AMS 4216B-2003 Aluminum Alloy Sheet 1 0Mg - 0 8Si - 0 8Cu - 0 50Mn (6013-T6) Solution Heat Treated and Artificially Aged (UNS A96013)《固溶热处理的含1 0Mg-0 8Si-0 8Cu-0 50Mn(6013-T6)的人.pdf
《SAE AMS 4216B-2003 Aluminum Alloy Sheet 1 0Mg - 0 8Si - 0 8Cu - 0 50Mn (6013-T6) Solution Heat Treated and Artificially Aged (UNS A96013)《固溶热处理的含1 0Mg-0 8Si-0 8Cu-0 50Mn(6013-T6)的人.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4216B-2003 Aluminum Alloy Sheet 1 0Mg - 0 8Si - 0 8Cu - 0 50Mn (6013-T6) Solution Heat Treated and Artificially Aged (UNS A96013)《固溶热处理的含1 0Mg-0 8Si-0 8Cu-0 50Mn(6013-T6)的人.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 there
2、from, 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 2013 SAE International All rights reserved. No part of this p
3、ublication 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: +1 724-776-497
4、0 (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:/www.sae.org/technical/standards/AMS4216B AEROSPACE MATERIAL SPECIFICATION AMS4216 REV. B Issued 1989-07 Revised 2
5、003-07 Reaffirmed 2013-12 Superseding AMS4216A Aluminum Alloy, Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged (Composition similar to A96013) RATIONALE AMS4216B has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE:1.1 Form: This spe
6、cification covers an aluminum alloy in the form of sheet.1.2 Application: This sheet has been used typically for structural parts requiring good strength, toughness, and fatigue properties and maximum corrosion resistance, but usage is not limited to such applications.2. APPLICABLE DOCUMENTS: The is
7、sue 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 revision of a document unless a specific document issue is specified. When the referenced document has been canceled and
8、 no superseding document has been specified, the last published issue of that document shall apply.2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.AMS 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought
9、 Products, Except Forging Stock, and Rolled, Forged, or Flash Welded RingsAMS 2772 Heat Treatment of Aluminum Alloy Wrought MaterialsAS1990 Aluminum Alloy TempersSAE INTERNATIONAL AMS4216B Page 2 of 5 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959
10、 or www.astm.org.ASTM B 660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products2.3 ANSI Publications: Available from ANSI, 25 West 43rd Street, New York, NY 10036 or www.ansi.org.ANSI H35.2 Dimensional Tolerances for Aluminu
11、m Mill ProductsANSI H35.2M 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 AMS 2355:3.2 Condition: Solution heat treated and artificially aged to the T6 te
12、mper in accordance with AMS 2772 (see AS1990).TABLE 1 - CompositionElement min maxSilicon 0.6 1.0Iron - 0.50Copper 0.6 1.1Manganese 0.20 0.8Magnesium 0.8 1.2Chromium - 0.10Zinc - 0.25Titanium - 0.10Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainderSAE INTERNATIONAL AMS4216B Pa
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