SAE AMS 4371B-2015 Magnesium Alloy Plate 4 0Y - 2 25Nd - 0 5Zr (WE43C - T5) Precipitation Heat Treated (UNS M18434).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 2015 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/AMS4371B AEROSPACE MATERIAL SPECIFICATION AMS4371 REV. B Issued 2013-03 Revised 2
5、015-06 Superseding AMS4371A Magnesium Alloy, Plate 4.0Y - 2.25Nd - 0.5Zr (WE43C - T5) Precipitation Heat Treated (Composition similar to UNS M18434) RATIONALE AMS4371B revises Properties (3.4.1.1, Table 2) and Reports (4.4.1). 1. SCOPE 1.1 Form This specification covers a magnesium alloy in the form
6、 of rolled plate from 0.500 up to 6.0 inches (12.7 to152.4 mm) inches inclusive (See 8.4). 1.2 Application This product has been used typically for parts requiring a combination of light weight, high yield strength up to 480nullF (250nullC), relatively high corrosion resistance, and good flammabilit
7、y resistance for magnesium alloys, 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
8、 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. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrenda
9、le, 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, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2750 Pyrometry SAE I
10、NTERNATIONAL AMS4371B Page 2 of 5 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, www.astm.org. ASTM B117 Standard Practice for Operating Salt Spray (Fog) Apparatus ASTM B557 Tension Testing Wrought a
11、nd Cast Aluminum- and Magnesium- Alloy Products ASTM B557M Tension Testing Wrought and Cast Aluminum- and Magnesium- Alloy Products (Metric) ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identification Marking of Aluminum and Magnesium Products ASTM B953 Sampling Mag
12、nesium and Magnesium Alloys for Spectrochemical Analysis ASTM B954 Analysis of Magnesium and Magnesium Alloys by Atomic Emission Spectrometry 2.3 ANSI Publications Available from American National Standards Institute, 25 West 43rd Street, 4th Floor, New York, NY 10036, Tel: 212-642-4900, www.ansi.or
13、g. 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 weight shown in Table 1, determined by spectrochemical methods in accordance with ASTM
14、B954, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element min max Yttrium Neodymium Zinc 3.7 2.0 - 4.3 2.5 0.06 Zirconium Other Rare Earths (3.1.1) Manganese Copper Iron Nickel 0.2 0.3 - - - - 1.0 1.0 0.03 0.02 0.005 0.0020 Other Elements, each (3.1.2) - 0.01 Magnes
15、ium remainder SAE INTERNATIONAL AMS4371B Page 3 of 5 3.1.1 Other Rare Earths are heavy rare earths, such as Gadolinium, Dysprosium, Erbium, Samarium, and Ytterbium. The total of Gadolinium + Dysprosium + Erbium shall be 0.3-1.0%. Samarium shall not exceed 0.04% and Ytterbium shall not exceed 0.02% 3
16、.1.2 Determination not required for routine acceptance. 3.2 Condition Precipitation heat treated. 3.2.1 Rolled plate shall be supplied with an as-rolled surface finish; light polishing to remove minor surface imperfections is permissible provided such imperfections can be removed within specified di
17、mensional tolerances. 3.3 Heat Treatment Plate shall be precipitation heat treated by heating to a temperature between 392 to 482 F (200 to 250 C), and holding at heat for the proper time for precipitation heat treatment to meet the requirements of 3.4, and air cooling. Pyrometry shall be in accorda
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