SAE AMS 4115J-2015 Aluminum Alloy Rolled or Cold-Finished Bars Rods Wire and Flash Welded Rings Annealed 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061-0) (UNS A96061).pdf
《SAE AMS 4115J-2015 Aluminum Alloy Rolled or Cold-Finished Bars Rods Wire and Flash Welded Rings Annealed 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061-0) (UNS A96061).pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4115J-2015 Aluminum Alloy Rolled or Cold-Finished Bars Rods Wire and Flash Welded Rings Annealed 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061-0) (UNS A96061).pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACE MATERIAL SPECIFICATION AMS4115 REV. J Issued 1960-01 Reaffirmed 2007-04 Revised 2015-03 Superseding AMS4115H Aluminum Alloy, Rolled or Cold-Finished, Bars, Rods, Wire, and Flash Welded Rings Annealed 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O) (Composition similar to UNS A96061) RATIONALE AM
2、S4115J revises Composition (Table 1), Properties (3.3.2.1, 3.3.2.4), Classification of Tests (4.2.1 and 4.2.2), and Reports (4.4.1), and is a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of rolled or cold-finished bars,
3、rods, and wire, of flash welded rings, and of stock for flash welded rings. 1.1.1 This specification covers products 8 inches (203 mm) and under in nominal diameter or least distance between parallel sides and for flash welded rings 8 inches (203 mm) and under in radial thickness, and stock of any s
4、ize (See 8.5). 1.2 Application These products have been used typically for parts requiring moderate strength, especially where such parts require brazing or welding during fabrication, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documents in effe
5、ct 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 document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been spe
6、cified, the last published issue of that document shall apply. _ 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
7、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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyrigh
8、t 2015 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. TO PLACE A DOCUMENT ORDER
9、: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (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/AMS4115J SAE INTER
10、NATIONAL AMS4115J Page 2 of 6 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, 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 Magnes
11、ium Alloy, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AMS7488 Rings, Flash Welded, Aluminum and Aluminum Alloys AS1990 Aluminum Alloy Tempers 2.2 ASTM Publications Available from ASTM International, 100 Bar
12、r Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Publications Available from American National Standards
13、Institute, 25 West 43rd Street, New York, NY 10036-8002, 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
14、weight shown in Table 1, determined in accordance with AMS2355. 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Bars, Rods, and Wire Rolled or cold-finished, as ordered, and annealed in accordance with AMS2772 to the O temper (See AS1990). 3.2.2 Flash Welded Rings Shall
15、 be manufactured in accordance with AMS7488 and annealed in accordance with AMS2772 to the O temper. SAE INTERNATIONAL AMS4115J Page 3 of 6 Table 1 - Composition Element min max Silicon 0.40 0.8 Iron - 0.7 Copper 0.15 0.40 Manganese - 0.15 Magnesium 0.8 1.2 Chromium 0.04 0.35 Zinc - 0.25 Titanium -
16、0.15 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder 3.2.3 Stock for Flash Welded Rings As ordered by the flash welded ring manufacturer. 3.3 Properties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced siz
17、e. 3.3.1 Bars, Rods, Wire, and Flash Welded Rings 3.3.1.1 As Annealed (-O) Condition Tensile Properties Shall be as shown in Table 2 for bars, rods, and wire 8 inches (203 mm) and under in nominal diameter or least distance between parallel sides and for flash welded rings 8 inches (203 mm) and unde
18、r in radial thickness. Table 2 O temper tensile properties Property Value Tensile Strength, maximum Yield Strength at 0.2% Offset, minimum 22.0 ksi (152 MPa) 6.0 ksi (41 MPa) Elongation in 4D, minimum 18% 3.3.2 Response to Heat Treatment 3.3.2.1 Response to Heat Treatment (O to T42 Temper) When spec
19、ified, product in the O temper (without the subsequent imposition of cold working or forming operations), after solution heat treatment and natural aging to the T42 temper (See AS1990) in accordance with AMS2772, shall have the properties of Table 3. 3.3.2.1.1 Natural Aging before Testing Specimens
20、in the T42 tempers will not be required to be tested within 4 days after completion of the solution heat treatment. If, within this period, the manufacturer elects to test specimens, which thereupon fail to meet the requirements, they can discard these original test results and test additional speci
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