SAE AMS 4409-2007 Aluminum Alloy Plate 4 0Zn - 2 0Mg - 0 32Mn (7019-T651) Solution Heat Treated Stress Relieved and Artificially Aged (UNS A97019)《4 0Zn 2 0Mg 0 32Mn (7019-T651)溶解热.pdf
《SAE AMS 4409-2007 Aluminum Alloy Plate 4 0Zn - 2 0Mg - 0 32Mn (7019-T651) Solution Heat Treated Stress Relieved and Artificially Aged (UNS A97019)《4 0Zn 2 0Mg 0 32Mn (7019-T651)溶解热.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4409-2007 Aluminum Alloy Plate 4 0Zn - 2 0Mg - 0 32Mn (7019-T651) Solution Heat Treated Stress Relieved and Artificially Aged (UNS A97019)《4 0Zn 2 0Mg 0 32Mn (7019-T651)溶解热.pdf(4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 isentirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefr
2、om, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.Copyright 2013 SAE InternationalAll rights reserved. No part of this publication may be
3、 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: +1 724-776-4970 (outside USA)Fax:
4、 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS4409AEROSPACEMATERIALSPECIFICATIONAMS4409Issued 2007-10Reaffirmed 2013-05Aluminum Alloy, Plate4.0Zn - 2
5、.0Mg - 0.32Mn (7019-T651)Solution Heat Treated, Stress Relieved and Artificially Aged(Composition similar to UNS A97019)RATIONALEAMS4409 has been reaffirmed to comply with the SAE five-year review policy.1. SCOPE1.1 FormThis specification covers an aluminum alloy in the form of plate.1.2 Application
6、This product has been used as a moderate strength engineered plate used also for selected structural applications, but usage is not limited to such applications. Armor plate applications are possible, but specific sampling and testing procedures regarding material properties required for this applic
7、ation shall be mutually agreed by producer and user.2. APPLICABLE DOCUMENTSThe 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 revision of a document unless a specifi
8、c 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 PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7
9、323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded RingsAMS 2772 Heat Treatment of Aluminum Alloy Raw MaterialsAS1990
10、 Aluminum Alloy TempersSAE AMS4409 Page 2 of 42.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM B 660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B 666/B666M Identification
11、 of Aluminum and Magnesium Alloy Products2.3 ANSI PublicationsAvailable from American National Standards Institute, Inc., 25 West 43rd Street, New York, NY 10036, Tel: 212-642-4900, www.ansi.org.ANSI H 35.2 Dimensional Tolerances for Aluminum Mill ProductsANSI H 35.2M Dimensional Tolerances for Alum
12、inum Mill Products (Metric)3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined in accordance with AMS 2355.TABLE 1 - COMPOSITIONElement min maxSilicon - 0.35Iron - 0.45Copper - 0.20Manganese 0.15 0.50Magnesium 1.5 2.5Zinc 3.5 4.5Titanium -
13、0.15Zirconium 0.10 0.25Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder3.2 ConditionThe product shall be supplied in the following condition:3.2.1 Solution and heat treated, stress-relieved by stretching to produce a nominal permanent set of 1.5%, but not less than 1% nor mo
14、re than 3%, and artificially aged to the -T651 temper (See AS1990).3.3 Heat TreatmentShall be performed in accordance with AMS 2772 and as follows:Solution Heat Treatment Temperature: 855 - 875 F (458 - 468 C)Aging Heat Treatment: Aging shall be performed at a specific temperature and time as requir
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