SAE AMS 4465A-2015 Aluminum Alloy Clad One Side Sheet 0 6Mg - 0 35Si - 0 28Cu (No 23 Brazing Sheet) As Fabricated (UNS A86951).pdf
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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 2015 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/AMS4465A AEROSPACE MATERIAL SPECIFICATION AMS4465 REV. A Issued 2009-09 Revised 2
5、015-06 Superseding AMS4465 Aluminum Alloy, Clad One Side Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 23 Brazing Sheet) As Fabricated (Composition similar to UNS A86951) RATIONALE AMS4465A revises Properties (3.3.1.1.1), Reports (4.4.1) and is a Five Year Review and update of this specification. 1. SCOPE 1.1
6、Form This specification covers an aluminum alloy in the form of sheet, clad on one side. 1.1.1 This specification covers product from 0.010 to 0.249 inches (0.25 to 6.32 mm) inclusive, in thickness (See 8.5). 1.2 Application This sheet has been used typically for brazed assemblies that are subjected
7、 to heat treatment after joining, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The 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
8、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 Publications Available from SAE International, 400 Commonwealth Drive, Warrendal
9、e, PA 15096-0001, Tel: 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 Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment o
10、f Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers SAE INTERNATIONAL AMS4465A Page 2 of 5 2.2 ASTM Publications Available 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 Aluminu
11、m and Magnesium Products ASTM B666/B666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Publications Available 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 Tolerance for Alu
12、minum Mill Products ANSI H35.2M Dimensional Tolerance for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1 and Table 2, determined in accordance with AMS2355. Table 1 - Composition, core (6951) Element Min Max Silic
13、on 0.20 0.50 Iron - 0.8 Copper 0.15 0.40 Manganese - 0.10 Magnesium 0.40 0.8 Zinc - 0.20 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder Table 2 - Composition, cladding (4045) Element Min Max Silicon 9.0 11.0 Iron - 0.8 Copper - 0.30 Manganese - 0.05 Magnesium - 0.05 Zinc
14、 - 0.10 Titanium - 0.20 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder 3.2 Condition As fabricated (F) (See AS1990). SAE INTERNATIONAL AMS4465A Page 3 of 5 3.3 Properties The sheet shall conform to the following applicable requirements, determined in accordance with AMS2
15、355 on the mill product: 3.3.1 After Solution and Precipitation Heat Treatment Sheet shall have the following properties after solution and precipitation heat treatment to the -T62 temper in accordance with AMS2772 for 6951 alloy. 3.3.1.1 Tensile Properties Shall be shown in Table 3. 3.3.1.1.1 Mecha
16、nical property requirements for product outside the range covered by 1.1.1 shall be agreed upon between purchaser and producer. Table 3A - Minimum tensile properties, inch/pound units (see 8.2) Nominal Thickness Inch Tensile Strength ksi Yield Strength at 2% Offset ksi Elongation in 2 Inches or 4D %
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