SAE AMS 4485-2012 Magnesium Alloy Extrusions 4 0Y - 2 25Nd - 0 5Zr (WE43C - T5) Precipitation Heat Treated (UNS M18434)《沉淀热处理的挤压制4 0Y 2 25Nd 0 5Zr(WE43C-T5)镁合金》.pdf
《SAE AMS 4485-2012 Magnesium Alloy Extrusions 4 0Y - 2 25Nd - 0 5Zr (WE43C - T5) Precipitation Heat Treated (UNS M18434)《沉淀热处理的挤压制4 0Y 2 25Nd 0 5Zr(WE43C-T5)镁合金》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4485-2012 Magnesium Alloy Extrusions 4 0Y - 2 25Nd - 0 5Zr (WE43C - T5) Precipitation Heat Treated (UNS M18434)《沉淀热处理的挤压制4 0Y 2 25Nd 0 5Zr(WE43C-T5)镁合金》.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 theref
2、rom, 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 InternationalAll rights reserved. No part of this publication may b
3、e 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 USA)Fax
4、: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS4485AEROSPACEMATERIALSPECIFICATIONAMS4485Issued 2012-12Magnesium Alloy, Extrusions4.0Y - 2.25Nd - 0.5Z
5、r (WE43C - T5)Precipitation Heat Treated(Composition similar to UNS M18434)RATIONALEAMS4485 is a new specification for magnesium alloy WE43C in the form of extrusions. 1. SCOPE1.1 FormThis specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles.1.2 Appli
6、cationThese extrusions have been used typically for parts requiring a combination of light weight, high yield strength up to 480 F (250 C), relatively high corrosion resistance, and good flammability resistance for magnesium alloys,but usage is not limited to such applications.2. APPLICABLE DOCUMENT
7、SThe 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 unless a specific document issue is specified. When the referenced document has been cance
8、lled and no superseding document has been specified, the last published issue of that document shall apply.2.1 SAE PublicationsAvailable 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.AMS
9、2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded RingsAMS2750 PyrometryCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted
10、 without license from IHS-,-,-SAE AMS4485 Page 2 of 52.2 ASTM PublicationsAvailable 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 117 Operating Salt Spray (Fog) ApparatusASTM B 557/B 557M Tension Testing Wrought
11、 and Cast Aluminium- and Magnesium- Alloy ProductsASTM B 660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B 666/B 666M Identification Marking of Aluminum and Magnesium ProductsASTM B 953 Sampling Magnesium and Magnesium Alloys for Spectrochemical AnalysisASTM B 954 Analysis of Magnesium
12、and Magnesium Alloys by Atomic Emission Spectrometry3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by spectrochemical methods in accordance withASTM B 954, or by other analytical methods acceptible to purchaser.TABLE 1 - COMPOSITIONEle
13、ment min maxYttriumNeodymiumZinc3.72.0-4.32.50.06ZirconiumOther Rare Earths (3.1.1)ManganeseCopperIronNickel0.20.3-1.01.00.030.020.0050.0020Other Elements, each - 0.01Magnesium remainder3.1.1 Other Rare Earths are heavy rare earths, such as Gadolinium, Dysprosium, Erbium, Samarium, and Ytterbium. Th
14、e total of Gadolinium + Dysprosium + Erbium shall be 0.3-1.0%. Samarium shall not exceed 0.04% and Ytterbium shall not exceed 0.02%3.2 ConditionPrecipitation heat treated.3.2.1 Extrusions shall be supplied with an as-extruded surface finish; light polishing to remove minor surface imperfections is p
15、ermissible provided such imperfections can be removed within specified dimensional tolerances.3.3 Heat TreatmentExtrusions shall be precipitation heat treated by heating to a temperature between 392 to 482 F (200 to 250 C), andholding at the selected temperature 10 F (6 C) for the proper time for pr
16、ecipitation heat treatment to meet the requirements of 3.4, and air cooling. Pyrometry shall be in accordance with AMS2750.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4485 Page 3 of 53.4 P
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