SAE AMS 4017L-2018 Aluminum Alloy Sheet and Plate 2 5Mg - 0 25Cr (5052-H34) Strain-Hardened Half-Hard and Stabilized (UNS A95052).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 ther
2、efrom, 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 2018 SAE International All rights reserved. No part of this
3、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: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-49
4、70 (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/AMS4017L AEROSPACE MATERIAL SPECIFICATION AMS4017 REV. L Issued 1942-01 Reaffirmed 2017-11 Rev
5、ised 2018-01 Superseding AMS4017K Aluminum Alloy Sheet and Plate 2.5Mg - 0.25Cr (5052-H34) Strain-Hardened, Half-Hard, and Stabilized (Composition similar to UNS A95052) RATIONALE AMS4017L revises Condition (3.2), Properties (3.3.1.1), Reports (4.4.1) and Identification (5.1.1), and results from a F
6、ive-Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of sheet and plate 0.009 to 1.000 inch (0.23 to 25.40 mm), inclusive, in nominal thickness (see 8.5). 1.2 Application These products have been used typically for parts requirin
7、g moderate forming and where good welding characteristics and resistance to corrosion are important, 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 exten
8、t 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 specified, the last published issue of that document shall apply. SAE INTERNATIONAL AMS
9、4017L Page 2 of 5 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 Magnesium Alloy Wro
10、ught Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, w
11、ww.astm.org. ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Accredited Publications Copies of these documents are available online at http:/webstore.ansi.org/. ANSI H35.1/ H35.1M Standard Alloy and Tem
12、per Designation System For Aluminum ANSI H35.2 Dimensional Tolerance 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 A
13、MS2355. Table 1 - Composition Element Min Max Silicon - 0.25 Iron - 0.40 Copper - 0.10 Manganese - 0.10 Magnesium 2.2 2.8 Chromium 0.15 0.35 Zinc - 0.10 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder 3.2 Condition Strain hardened, half-hard, and stabilized to the H34 tem
14、per (see ANSI H35.1/H35/1M). SAE INTERNATIONAL AMS4017L Page 3 of 5 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. 3.3.1.1 Tensile property requirement
15、s for sheet and plate outside the thickness range of 1.1 shall be as agreed upon by purchaser and producer. Table 2 Table 2A - Tensile properties, inch/pound units Nominal Thickness Inch Tensile Strength ksi Yield Strength at 0.2% Offset ksi, Min Elongation in 2 Inches or 4D %, Min 0.009 to 0.019, i
16、ncl 34.0 - 41.0 26.0 3 Over 0.019 to 0.050, incl 34.0 - 41.0 26.0 4 Over 0.050 to 0.113, incl 34.0 - 41.0 26.0 6 Over 0.113 to 0.249, incl 34.0 - 41.0 26.0 7 Over 0.249 to 1.000, incl 34.0 - 41.0 26.0 10 Table 2B - Tensile properties, SI units Nominal Thickness Millimeters Tensile Strength MPa Yield
17、 Strength at 0.2% Offset MPa, Min Elongation in 50.8 mm or 4D %, Min 0.23 to 0.48, incl 234 - 283 179 3 Over 0.48 to 1.27, incl 234 - 283 179 4 Over 1.27 to 2.87, incl 234 - 283 179 6 Over 2.87 to 6.32, incl 234 - 283 179 7 Over 6.32 to 25.40, incl 234 - 283 179 10 3.3.2 Bending Product 0.249 inch (
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