SAE AMS 4474A-2015 Aluminum Alloy Sheet and Plate 4 0Cu - 1 0Li - 0 40Mg - 0 35Ag - 0 13Zr (2195-T8) Solution Heat Treated Cold Worked and Artificially Aged (UNS A92195).pdf
《SAE AMS 4474A-2015 Aluminum Alloy Sheet and Plate 4 0Cu - 1 0Li - 0 40Mg - 0 35Ag - 0 13Zr (2195-T8) Solution Heat Treated Cold Worked and Artificially Aged (UNS A92195).pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4474A-2015 Aluminum Alloy Sheet and Plate 4 0Cu - 1 0Li - 0 40Mg - 0 35Ag - 0 13Zr (2195-T8) Solution Heat Treated Cold Worked and Artificially Aged (UNS A92195).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 is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref
2、rom, 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 2015 SAE InternationalAll rights reserved. No part of this publi
3、cation 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: +1 724-776-4970 (out
4、side USA)Fax: 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/AMS4474AAEROSPACEMATERIAL SPECIFICATIONAMS4474 REV. AIssued 2012-10Revised 2015-08Superseding
5、 AMS4474Aluminum Alloy, Sheet and Plate4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T8)Solution Heat Treated, Cold Worked, and Artificially Aged(Composition similar to UNS A92195)RATIONALEAMS4474A revises Properties (3.4.1.1, Table 2), and Reports (4.4.1) as a result of increasing the product thic
6、kness range.1. SCOPE1.1 FormThis specification covers an aluminum alloy in the form of sheet and plate with a thickness of 0.125 to 0.499 inch (3.20 to 12.67 mm), inclusive (See 8.4).1.2 ApplicationThis product has been used for aircraft applications where it offers a combination of high strength an
7、d low density, but usage is not limited to such applications.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
8、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 PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel:
9、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, Forged, or Flash Welded RingsAMS2772 Heat Treatment of Aluminum Alloy Raw Mate
10、rialsAS1990 Aluminum Alloy TempersSAE INTERNATIONAL AMS4474A 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 B660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B
11、666/B666M Identification Marking of Aluminum and Magnesium Products2.3 ANSI PublicationsAvailable from American National Standards Institute, 25 West 43rd Street, 4th Floor, New York, NY 10036, Tel: 212-642-4900, www.ansi.org.ANSI H35.2 Dimensional Tolerances for Aluminum Mill ProductsANSI H35.2M Di
12、mensional Tolerances for Aluminum Mill Products (Metric)3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355.Table 1 - CompositionElement min maxSilicon - 0.12Iron - 0.15Copper 3.7 4.3Manganese - 0.25Magnesium 0.25
13、 0.8Zinc - 0.25Titanium - 0.10Zirconium 0.08 0.16Silver 0.25 0.6Lithium 0.8 1.2Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder3.2 ConditionProduct shall be supplied in the following condition:3.2.1 Solution heat treated, cold worked and artificially aged to T8 temper (See A
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