SAE AMS 4016M-2013 Aluminum Alloy Sheet and Plate 2 5Mg - 0 25Cr (5052-H32) Strain Hardened Quarter-Hard and Stabilized (UNS A95052)《应变硬化四分之一硬度和稳定的镁合金薄板和板材 2 5Mg 0 25Cr (5052-H32)》.pdf
《SAE AMS 4016M-2013 Aluminum Alloy Sheet and Plate 2 5Mg - 0 25Cr (5052-H32) Strain Hardened Quarter-Hard and Stabilized (UNS A95052)《应变硬化四分之一硬度和稳定的镁合金薄板和板材 2 5Mg 0 25Cr (5052-H32)》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4016M-2013 Aluminum Alloy Sheet and Plate 2 5Mg - 0 25Cr (5052-H32) Strain Hardened Quarter-Hard and Stabilized (UNS A95052)《应变硬化四分之一硬度和稳定的镁合金薄板和板材 2 5Mg 0 25Cr (5052-H32)》.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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2012 SAE International All rights reserved. No part of this publication m
3、ay 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: +1 724-776-4970 (outside U
4、SA) 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/AMS4016M AEROSPACE MATERIAL SPECIFICATION AMS4016 REV. M Issued 1939-12 Revised 2013-01 Super
5、seding AMS4016L Aluminum Alloy, Sheet and Plate 2.5Mg - 0.25Cr (5052-H32) Strain Hardened, Quarter-Hard, and Stabilized (Composition similar to UNS A95052) RATIONALE AMS4016M results from a Limited Scope Ballot to revise the headers on Tables 2A and 2B to indicate that yield strength and elongation
6、values are minima. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of sheet and plate. 1.2 Application These products have been used typically for parts requiring moderate strength, good formability, good welding and resistance spot welding characteristics, and good resista
7、nce to corrosion, 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 specification to the extent specified herein. The supplier may work to a subsequent revision of a document un
8、less 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 15096-0001
9、, 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 SAE AMS4016M Page 2 of 5 2.2 ASTM Publicati
10、ons 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 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Publica
11、tions Available from American National Standards 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
12、 Composition Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355. TABLE 1 - COMPOSITION Element min max Silicon Iron Copper Manganese Magnesium Chromium Zinc Other Elements, each Other Elements, total Aluminum - - - - 2.2 0.15 - - - remainder 0.25 0.40
13、0.10 0.10 2.8 0.35 0.10 0.05 0.15 3.2 Condition Strain hardened, quarter-hard, and stabilized (See 8.2). 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 specified in Table 2.
14、 SAE AMS4016M Page 3 of 5 TABLE 2A - TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi, min Elongation in 2 Inches or 4D %, min 0.017 to 0.019, incl Over 0.019 to 0.050, incl Over 0.050 to 0.113, incl Over 0.113 to 0.249, incl Over 0
15、.249 to 0.499, incl Over 0.499 to 2.000, incl 31.0 to 38.0 31.0 to 38.0 31.0 to 38.0 31.0 to 38.0 31.0 to 38.0 31.0 to 38.0 23.0 23.0 23.0 23.0 23.0 23.0 4 5 7 9 11 12 TABLE 2B - TENSILE PROPERTIES, SI UNITS Nominal Thickness Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa, min El
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