SAE AMS 4029L-2012 Aluminum Alloy Sheet and Plate (2014 -T6 Sheet -T651 Plate) Solution and Precipitation Heat Treated (UNS A92014)《溶液沉淀热处理的铝合金薄板材和厚板材(2014 T6型薄板材和T651型厚板材)》.pdf
《SAE AMS 4029L-2012 Aluminum Alloy Sheet and Plate (2014 -T6 Sheet -T651 Plate) Solution and Precipitation Heat Treated (UNS A92014)《溶液沉淀热处理的铝合金薄板材和厚板材(2014 T6型薄板材和T651型厚板材)》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4029L-2012 Aluminum Alloy Sheet and Plate (2014 -T6 Sheet -T651 Plate) Solution and Precipitation Heat Treated (UNS A92014)《溶液沉淀热处理的铝合金薄板材和厚板材(2014 T6型薄板材和T651型厚板材)》.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 2017 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:/standards.sae.org/AMS4029L AEROSPACE MATERIAL SPECIFICATION AMS4029 REV. L Issued 1958-08 Revised 2012-01 Reaffir
5、med 2017-09 Superseding AMS4029K Aluminum Alloy Sheet and Plate (2014; -T6 Sheet, -T651 Plate) Solution and Precipitation Heat Treated (Composition similar to UNS A92014) RATIONALE AMS4029L has been reaffirmed to comply with the SAE Five-Year Review policy. 1. SCOPE 1.1 Form This specification cover
6、s an aluminum alloy in the form of sheet and plate. 1.2 Application These products have been used typically for structural parts of good strength, but usage is not limited to such applications. 1.2.1 Certain design and processing procedures may cause these products to become susceptible to stress-co
7、rrosion cracking; ARP823 recommends practices to minimize such conditions. 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 of a d
8、ocument 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, Warrendale, PA
9、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 Rings AMS2772 Heat Treatment of Aluminu
10、m Alloy Raw Materials ARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products AS1990 Aluminum Alloy Tempers SAE INTERNATIONAL AMS4029L Page 2 of 5 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, P
11、A 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum Products 2.3 ANSI Publications Available from American National Standards Institute, 25 West 43rd Street, New York, NY 10036-8002, Tel:
12、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 AMS2355
13、. TABLE 1 - COMPOSITION Element min maxSilicon 0.50 1.2 Iron - 0.7 Copper 3.9 5.0 Manganese 0.40 1.2 Magnesium 0.20 0.8 Chromium - 0.10Zinc - 0.25Titanium - 0.15Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder 3.2 Condition The product shall be supplied in the following cond
14、ition: 3.2.1 Sheet Solution and precipitation heat treated in accordance with AMS2772 to the T6 temper (See AS1990). 3.2.2 Plate Solution heat treated, stretched to produce a nominal permanent set of 2% but not less than 1-1/2% nor more than 3%, and precipitation heat treated to T651 (See AS1990). B
15、oth solution heat treatment and precipitation heat treatment shall be in accordance with AMS2772. 3.2.2.1 Plate shall receive no further straightening operations after stretching. SAE INTERNATIONAL AMS4029L Page 3 of 5 3.3 Properties The product shall conform to the following requirements, determine
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