SAE AMS 4376H-2011 Plate Magnesium Alloy 3 0Al - 1 0Zn - 0 20Mn (AZ31B-H26) Cold Rolled and Partially Annealed (UNS M11311)《含3 0Al-1 0Zn-0 20Mn(AZ31B-H26)冷轧和局部退火的镁合金板材》.pdf
《SAE AMS 4376H-2011 Plate Magnesium Alloy 3 0Al - 1 0Zn - 0 20Mn (AZ31B-H26) Cold Rolled and Partially Annealed (UNS M11311)《含3 0Al-1 0Zn-0 20Mn(AZ31B-H26)冷轧和局部退火的镁合金板材》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4376H-2011 Plate Magnesium Alloy 3 0Al - 1 0Zn - 0 20Mn (AZ31B-H26) Cold Rolled and Partially Annealed (UNS M11311)《含3 0Al-1 0Zn-0 20Mn(AZ31B-H26)冷轧和局部退火的镁合金板材》.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 2011 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/AMS4376H AEROSPACE MATERIAL SPECIFICATION AMS4376 REV. H Issued 1950-06 Revised 2011-09Supers
5、eding AMS4376G Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-H26) Cold Rolled and Partially Annealed (Composition similar to UNS M11311) RATIONALE AMS4376H revises Composition (3.1, Table 1) and results from a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specifica
6、tion covers a magnesium alloy in the form of plate. 1.2 Application This product has been used typically for moderate-strength parts requiring rigidity with low density, but usage is not restricted to such applications. 2. APPLICABLE DOCUMENTS 2.1 The issue of the following documents in effect on th
7、e 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 specified,
8、the last published issue of that document shall apply. 2.2 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, Sampling and Testing, Alum
9、inum Alloys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings SAE AMS4376H Page 2 of 5 2.3 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.or
10、g. ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products ASTM E 9 Compression Testing of Metallic Materials at Room Temperature 2.4 ANSI Publications Available from American National Standards Institute, 25 West 43
11、rd Street, New York, NY 10036-8002, Tel: 212-642-4900, www.ansi.org. ANSI H 35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H 35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Tab
12、le 1, determined in accordance with AMS2355. TABLE 1 - COMPOSITION Element min max Aluminum 2.5 3.5 Zinc 0.7 1.3 Manganese 0.20 1.0 Silicon - 0.05 Copper - 0.05Calcium - 0.04 Iron 0.005Nickel 0.005Other Elements, each (3.1.1) - 0.10 Other Elements, total (3.1.1) - 0.30 Magnesium remainder 3.1.1 Dete
13、rmination not required for routine acceptance. 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Plate 0.500 Inch (12.70 mm) and Under in Nominal Thickness Cold rolled, partially annealed, and pickled. 3.2.2 Plate Over 0.500 Inch (12.70 mm) in Nominal Thickness Cold rolle
14、d and partially annealed. SAE AMS4376H Page 3 of 5 3.3 Properties The plate shall conform to the following requirements: 3.3.1 Tensile Properties Shall be as specified in Table 2, determined in accordance with AMS2355 on the mill produced size. TABLE 2A - TENSILE PROPERTIES Nominal Thickness Inches
15、Tensile Strength ksi, min Yield Strength at 0.2% Offset ksi, min Elongation in 2 inches or 4D %, min 0.250 to 0.375, incl 39.0 27.0 6 Over 0.375 to 0.500, incl 38.0 26.0 6 Over 0.500 to 0.750, incl 37.0 25.0 6 Over 0.750 to 1.000, incl 37.0 23.0 6 Over 1.000 to 1.500, incl 35.0 22.0 6 Over 1.500 to
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