SAE AMS 4128D-2007 Aluminum Alloy Bars Rolled or Cold Finished 1 0Mg - 0 60Si - 0 30Cu - 0 20Cr (6061-T451) Solution Heat Treated and Stress Relieved by Stretching (UNS A96061)《1 0.pdf
《SAE AMS 4128D-2007 Aluminum Alloy Bars Rolled or Cold Finished 1 0Mg - 0 60Si - 0 30Cu - 0 20Cr (6061-T451) Solution Heat Treated and Stress Relieved by Stretching (UNS A96061)《1 0.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4128D-2007 Aluminum Alloy Bars Rolled or Cold Finished 1 0Mg - 0 60Si - 0 30Cu - 0 20Cr (6061-T451) Solution Heat Treated and Stress Relieved by Stretching (UNS A96061)《1 0.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 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 2013 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/AMS4128D AEROSPACE MATERIAL SPECIFICATION AMS4128 REV. D Issued 1969-11 Revised 2
5、007-10 Reaffirmed 2013-09 Superseding AMS4128C Aluminum Alloy Bars, Rolled or Cold Finished 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T451) Solution Heat Treated and Stress Relieved by Stretching (Composition similar to UNS A96061) RATIONALE AMS4128D has been reaffirmed to comply with the SAE five-year
6、 review policy. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of bars and rods 0.500 inch (12.50 mm) and over in nominal diameter or least difference between parallel sides. 1.2 Application These bars have been used typically for parts where moderate ductility, formabilit
7、y, and response to precipitation heat treatment are required and where distortion during machining must be minimized, 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 specifica
8、tion 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 has been specified, the last published issue of that document shall apply. 2.1
9、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. AMS 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except
10、Forging Stock, and Rolled, Forged, or Flash Welded Rings AMS 2772 Heat Treatment of Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers SAE INTERNATIONAL AMS4128D Page 2 of 5 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 1
11、9428-2959, Tel: 610-832-9585, www.astm.org. ASTM B660 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 10036,
12、Tel: 212-642-4900, www.ansi.org. ANSI H35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H35.2M 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 with AM
13、S 2355. TABLE 1 - COMPOSITION Element min maxSilicon 0.40 0.8 Iron - 0.7 Copper 0.15 0.40Manganese - 0.15Magnesium 0.8 1.2 Chromium 0.04 0.35Zinc - 0.25Titanium - 0.15Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder 3.2 Condition Rolled or cold finished, as ordered, solution
14、 heat treated in accordance with AMS 2772, and stress-relieved by stretching to produce a nominal permanent set of 1-1/2% but not less than 1% nor more than 3% to produce the -T451 temper (See AS1990). 3.2.1 Product shall receive no further straightening operations after stretching, unless specifica
15、lly authorized by purchaser. 3.3 Properties Product 0.500 inch (12.50 mm) to 8.000 inch (203.2 mm) in nominal diameter or least distance between parallel sides shall conform to the following requirements, determined in accordance with AMS 2355 on the mill produced size. SAE INTERNATIONAL AMS4128D Pa
16、ge 3 of 5 3.3.1 As Solution Heat Treated and Stress-Relieved by Stretching 3.3.1.1 Tensile Properties Shall be as shown in Table 2: TABLE 2A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness Inches Tensile Strength ksi Yield Strength at 0.2% Offset Elongation % in 2 Inches or 4D 0.500
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