SAE AMS 4347D-2014 Aluminum Alloy Sheet 1 0Mg - 0 8Si - 0 8Cu - 0 5Mn (6013-T4) Solution Heat Treated and Naturally Aged (UNS A96013).pdf
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1、AEROSPACE MATERIAL SPECIFICATION AMS4347 REV. D Issued 1987-10 Revised 2014-12 Superseding AMS4347C Aluminum Alloy Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.5Mn (6013-T4) Solution Heat Treated and Naturally Aged (Composition similar to UNS A96013) RATIONALE AMS4347D revises Properties (3.3.1), and Reports (4.
2、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 from 0.020 to 0.249 inch (0.51 to 6.32 mm), inclusive, in thickness (See 8.5). 1.2 Application This product has been used typically for formed structur
3、al parts where good stretch formability is required and where, after precipitation heat treatment, good strength, toughness, and fatigue properties and maximum corrosion resistance are inherent, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documen
4、ts 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 cancelled and no superseding document ha
5、s been specified, the last published issue of that document shall apply. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2355 Quality Assurance, Sampling
6、 and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers _ SAE Technical Standards Board Rules provide that: “This report is published by
7、 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 therefrom, is the sole responsibility of the user.” SAE reviews each technical report
8、 at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2014 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in an
9、y 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: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS:
10、 http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4347D SAE INTERNATIONAL AMS4347D Page 2 of 4 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken,
11、 PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Publications Available from American National Standards Institute, 25 West 43rd Street, New York, NY 1
12、0036, Tel: 212-642-4900, www.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
13、 with AMS2355. TABLE 1 - Composition Element min max Silicon 0.6 1.0 Iron - 0.50 Copper 0.6 1.1 Manganese 0.20 0.8 Magnesium 0.8 1.2 Chromium - 0.10 Zinc - 0.25 Titanium - 0.10 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder 3.2 Condition Solution heat treated and natural
14、ly aged to the T4 temper (AS1990) in accordance with AMS2772. 3.3 Tensile Properties Sheet, 0.020 to 0.249 inch (0.51 to 6.32 mm), inclusive, in nominal thickness, shall conform to the requirements of Table 2 and Table 3, determined in the long-transverse direction in accordance with AMS2355 on the
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