SAE AMS 4248C-2012 Aluminum Alloy Hand Forgings and Rolled Rings 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061-T652) Solution Heat Treated Stress Relief Compressed and Precipitation Heat .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 2012 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/AMS4248C AEROSPACE MATERIAL SPECIFICATION AMS4248 REV. C Issued 1987-01 Reaffirme
5、d 2000-10 Revised 2012-01 Superseding AMS4248B Aluminum Alloy Hand Forgings and Rolled Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T652) Solution Heat Treated, Stress Relief Compressed, and Precipitation Heat Treated (Composition similar to UNS A96061)RATIONALE AMS4248C revises ordering data (8.5)
6、and results from a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of hand forgings and rolled rings. 1.2 Application These products have been used typically for complex shaped parts requiring moderate strength and good for
7、geability of the alloy and where stability is required during machining, but usage is not limited to such applications. Corrosion resistance of this alloy is superior to that of aluminum alloys having copper as the principal alloying element. 2. APPLICABLE DOCUMENTS The issue of the following docume
8、nts 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 document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document h
9、as been specified, the last published issue of that document shall apply. 2.1 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. AMS2355 Quality Assurance, Samplin
10、g and Testing, Aluminum Alloys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2808 Identification, Forgings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers SAE AMS4248C Page 2 of 6 2.2 ASTM Publications
11、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 B 594 Ultrasonic Inspection of Aluminum-Alloy Products for Aerospace Applications ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM E 14
12、17 Liquid Penetrant Testing 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355. 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.
13、35 Zinc - 0.25 Titanium - 0.15 Other Elements - 0.05 Other Elements - 0.15 Aluminum remainder 3.2 Condition Solution heat treated, stress relieved by compression to produce 1 to 5% permanent set, and precipitation heat treated. Heat treatments shall be performed in accordance with AMS2772 to the T65
14、2 temper (See AS1990). 3.2.1 Forge stock as ordered by the forging manufacturer. 3.3 Properties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced size: 3.3.1 Tensile Properties Shall be as follows: 3.3.1.1 Hand Forgings Specimens, mac
15、hined from forgings having an essentially square or rectangular cross-section heat treated in the indicated thickness, shall have the properties shown in Table 2A or 2B provided the as-forged thickness does not exceed 8 inches (203 mm) and the cross-sectional area is not over 256 square inches (1652
16、 cm2). SAE AMS4248C Page 3 of 6 TABLE 2A - MINIMUM TENSILE PROPERTIES, HAND FORGINGS, INCH/POUNDS UNITS Nominal Thickness at Time of Heat Treatment Inches Specimen Orientation Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in or 4D % Up to 2, incl Longitudinal 38.0 35.0 10 Long.-T
17、rans. 8 Over 2 to 4, incl Longitudinal 38.0 35.0 10 Long.-Trans. 38.0 35.0 8 Short-Trans. 37.0 33.0 5 Over 4 to 8, incl Longitudinal 37.0 34.0 8 Long.-Trans. 6 Short-Trans. 35.0 32.0 4 TABLE 2B - MINIMUM TENSILE PROPERTIES, HAND FORGINGS, SI UNITS Nominal Thickness at Time of Heat Treatment Millimet
18、ers Specimen Orientation Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in or 4D % Up to 51, incl Longitudinal 262 241 10 Long.-Trans. 8 Over 51 to 102, incl Longitudinal 262 241 10 Long.-Trans. 262 241 8 Short-Trans. 255 228 5 Over 102 to 203, incl Longitudinal 255 234 8 Long.-Tr
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