SAE AMS 4339A-2004 Aluminum Alloy Rolled or Cold Finished Bars and Rods 4 4Cu - 1 5Mg - 0 60Mn (2024-T851) Solution Heat Treated Cold Worked and Artificially Aged (UNS A92024)《经4 4.pdf
《SAE AMS 4339A-2004 Aluminum Alloy Rolled or Cold Finished Bars and Rods 4 4Cu - 1 5Mg - 0 60Mn (2024-T851) Solution Heat Treated Cold Worked and Artificially Aged (UNS A92024)《经4 4.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4339A-2004 Aluminum Alloy Rolled or Cold Finished Bars and Rods 4 4Cu - 1 5Mg - 0 60Mn (2024-T851) Solution Heat Treated Cold Worked and Artificially Aged (UNS A92024)《经4 4.pdf(5页珍藏版)》请在麦多课文档分享上搜索。
1、 AEROSPACE MATERIAL SPECIFICATION Aluminum Alloy, Rolled or Cold Finished Bars and Rods 4.4Cu - 1.5Mg - 0.60Mn (2024-T851) Solution Heat Treated, Cold Worked, and Artificially Aged (Composition similar to UNS A92024) TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4
2、970 (outside USA) Fax: 724-776-0790 Email: custsvcsae.org SAE WEB ADDRESS: http:/www.sae.org AMS 4339AIssued MAR 1994 Revised OCT 2004 Superseding AMS 4339 1. SCOPE: 1.1 Form: This specification covers an aluminum alloy in the form of rolled or cold finished bars and rods. 1.2 Application: These pro
3、ducts have been used typically for parts requiring higher yield strength than is afforded by naturally aged tempers of this alloy and whose fabrication does not involve welding, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS: The issue of the following documents in effect on
4、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 a specific document issue is specified. When the referenced document has been canceled and no superseding document has been specified,
5、 the last published issue of that document shall apply. 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org. AMS 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolle
6、d, Forged, or Flash Welded Rings AMS 2772 Heat Treatment of Aluminum Alloy Raw Materials 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
7、and suitability for any particular use, including any patent infringement arising therefrom, 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 suggestio
8、ns. Copyright 2004 SAE International All rights reserved. No part of this publication 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. SAE - 2 - AMS
9、 4339A AMS 4339A2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM E 594 Ultrasonic Inspection of Aluminum-Alloy Products for Aerospace Applications ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products A
10、STM B 666/B 666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Publications: Available from ANSI, 25 West 43rd Street, New York, NY 10036 or www.ansi.org. ANSI H35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (
11、Metric) 3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS 2355. TABLE 1 - Composition Element min max Silicon Iron Copper Manganese Magnesium Chromium Zinc Titanium Other Impurities, Each Other Impurities, Total
12、 Aluminum - - 3.8 0.30 1.2 - - - - - remainder 0.50 0.50 4.9 0.9 1.8 0.10 0.25 0.15 0.05 0.15 3.2 Condition: The product shall be solution heat treated, cold worked, and artificially aged and shall be stress-relieved by stretching or other means after heat treatment to produce a nominal permanent se
13、t of 1.5% but not less than 1% nor more than 3%. The heat treatment and aging shall be performed in accordance with AMS 2772. SAE - 3 - AMS 4339A AMS 4339A3.2.1 Bars and rods stress-relieved by stretching shall receive no further straightening operations after stretching unless specifically authoriz
14、ed by purchaser. 3.3 Properties: The product shall conform to the following requirements, determined in accordance with AMS 2355 or on the mill product: 3.3.1 Tensile Properties: Shall be as shown in Table 2 except as specified in 3.3.1.1. TABLE 2 - Minimum Tensile Properties Tensile Strength Yield
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