SAE AMS 4478-2013 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (Alclad 2024 -T81 Sheet -T851 Plate) Solution Heat Treated Cold Worked and Artificially Aged (UNS A82.pdf
《SAE AMS 4478-2013 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (Alclad 2024 -T81 Sheet -T851 Plate) Solution Heat Treated Cold Worked and Artificially Aged (UNS A82.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4478-2013 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (Alclad 2024 -T81 Sheet -T851 Plate) Solution Heat Treated Cold Worked and Artificially Aged (UNS A82.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 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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.Copyright 2013 SAE InternationalAll rights reserved. No part of this publication may b
3、e 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/AMS4478AEROSPACEMATERIALSPECIFICATIONAMS4478Issued 2013-07Aluminum Alloy, Sheet and Plate, Alclad4.4Cu -
5、1.5Mg - 0.60Mn (Alclad 2024, -T81 Sheet, -T851 Plate)Solution Heat Treated, Cold Worked and Artificially Aged(Composition similar to UNS A82024)RATIONALEAMS4478 is a new specification for Alclad 2024-T81/-T851 sheet and plate to facilitate stabilization of AMS-QQ-A-250/5.1. SCOPE1.1 FormThis specifi
6、cation covers an aluminum alloy in the form of Alclad sheet and plate supplied in the T81/-T851 temper.1.2 ApplicationThese products have been used typically for high strength parts requiring higher yield strength than is afforded by naturallyaged tempers of this alloy and maximum corrosion resistan
7、ce and whose fabrication does not involve welding, 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 supplied herein. The supplier may work to a subseq
8、uent 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 PublicationsAvailable from SAE International, 400 Commonwealth Driv
9、e, 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 and Testing, Aluminum Alloys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded RingsAMS2772 Heat Trea
10、tment of Aluminum Alloy Raw MaterialsAS1990 Aluminum Alloy TempersSAE AMS4478 Page 2 of 52.2 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 594 Ultrasonic Inspection of Aluminum-Alloy
11、Products for Aerospace ApplicationsASTM B 660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B 666/B 666M Identification of Aluminum and Magnesium Alloy Products2.3 ANSI PublicationsAvailable from American National Standards Institute, 25 West 43rd Street, New York, NY 10036, Tel: 212-642-
12、4900, www.ansi.org.ANSI H 35.2 Dimensional Tolerances for Aluminum Mill ProductsANSI H 35.2M Dimensional Tolerances for Aluminum Mill Products (Metric)3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight as shown in Tables 1 and 2, determined in accordance with AMS2355.
13、TABLE 1 COMPOSITION, CORE (2024)Element min maxSilicon - 0.50Iron - 0.50Copper 3.8 4.9Manganese .30 0.9Magnesium 1.2 1.8Chromium - 0.10Zinc - 0.25Titanium - 0.15Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainderTABLE 2 COMPOSITION, CLADDING (1230)Element min maxIron + Silicon
14、- 0.70Copper - 0.10Manganese - 0.05Magnesium - 0.05Zinc - 0.10Titanium - 0.03Other Elements, each - 0.03Aluminum 99.30 -3.2 ConditionThe product shall be supplied in the following condition:SAE AMS4478 Page 3 of 53.2.1 SheetSolution heat treated, cold worked and artificially aged to the T81 temper i
15、n accordance with AMS2772. (See AS1990).3.2.2 PlateSolution heat treated, stretched to produce a nominal permanent set of 2% but not less than 1-1/2% nor more than 3%, and artificially aged to the T851 temper in accordance with AMS2772 (See AS1990).3.2.2.1 Plate shall receive no further straightenin
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