SAE AMS 4352J-2017 Magnesium Alloy Extrusions 5 5Zn - 0 45Zr (ZK60A-T5) Precipitation Heat Treated (UNS M16600).pdf
《SAE AMS 4352J-2017 Magnesium Alloy Extrusions 5 5Zn - 0 45Zr (ZK60A-T5) Precipitation Heat Treated (UNS M16600).pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4352J-2017 Magnesium Alloy Extrusions 5 5Zn - 0 45Zr (ZK60A-T5) Precipitation Heat Treated (UNS M16600).pdf(6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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2017 SAE InternationalAll rights reserved. No part of this publi
3、cation 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: +1 724-776-4970 (out
4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on thisTechnical Report, please visithttp:/standards.sae.org/AMS4352JAEROSPACEMATERIAL SPECIFICATIONAMS4352 REV. JIssued 1951-10Reaffirmed 2008-11Revised 2017-06Superse
5、ding AMS4352HMagnesium Alloy, Extrusions5.5Zn - 0.45Zr (ZK60A-T5)Precipitation Heat TreatedUNS M16600RATIONALEAMS4352J revises Composition (Table 1), Properties (3.4), Reports (4.4), Identification (5.1.1) and Packaging (5.2.1), and is a Five-Year Review and update of this specification.1. SCOPE1.1
6、FormThis specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles up to 40 in2(258 cm2) in cross-sectional area (solids) and up to 8.5 inches (216 mm) OD by 1.188 inches (30.18 mm) wall thickness (tubing) (see 8.4).1.2 ApplicationThese extrusions have bee
7、n used typically for parts requiring toughness and moderate abrasion resistance, but usage is not limited to such applications.2. APPLICABLE DOCUMENTSThe 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. Th
8、e 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.2.1 SAE PublicationsAvailable from SAE Inter
9、national, 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 Wrought Products (Except Forging Stock), and Rolled, Forged, or Fla
10、sh Welded RingsAMS2750 PyrometryARP1917 Clarification of Terms Used in Aerospace Metals SpecificationsSAE INTERNATIONAL AMS4352J Page 2 of 62.2 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.
11、ASTM B666/B666M Identification Marking of Aluminum and Magnesium ProductsASTM E9 Compression Testing of Metallic Materials at Room Temperature2.3 ANSI Accredited PublicationsCopies of these documents are available online at http:/webstore.ansi.org/.ANSI H35.2 Dimensional Tolerances for Aluminum Mill
12、 ProductsANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric)3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355.Table 1 - CompositionElement Min MaxZinc 4.8 6.2Zirconium 0.45 1.0Impurities, each
13、 (3.1.1) - 0.10Impurities, total (3.1.1) - 0.30Magnesium remainder3.1.1 Determination not required for routine acceptance.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 permissibl
14、e provided such imperfections can be removed within specified dimensional tolerances.3.3 Heat TreatmentExtrusions shall be precipitation heat treated by heating to 300 F 15 F (149 C 8 C), holding at heat for not less than 24 hours, and cooling in air. Pyrometry shall be in accordance with AMS2750.3.
15、4 PropertiesExtrusions shall conform to the requirements of 3.4.1 and 3.4.2. Mechanical property requirements for product outside of the ranges covered by 1.1 shall be agreed upon between purchaser and producer.3.4.1 Tensile PropertiesShall be as specified in 3.4.1.1 and 3.4.1.2, and 3.4.1.3, determ
16、ined in accordance with AMS2355.3.4.1.1 Bars, Rods, Wire, and Solid ProfilesSAE INTERNATIONAL AMS4352J Page 3 of 6Table 2Table 2A - Minimum tensile properties, inch/pound unitsNominalCross-Sectional AreaSquare InchesTensileStrengthksiYield Strengthat 0.2% OffsetksiElongationin 4D%Up to 5, excl 45.0
17、36.0 45 to 25, excl 45.0 34.0 625 to 40, excl 43.0 31.0 6Table 2B - Minimum tensile properties, SI unitsNominalCross-Sectional AreaSquare CentimetersTensileStrengthMPaYield Strengthat 0.2% OffsetMPaElongationin 4D%Up to 32, excl 310 248 432 to 161, excl 310 234 6161 to 258, excl 296 214 63.4.1.2 Tub
18、ingTable 3Table 3A - Minimum tensile properties, inch/pound unitsNominalODInchesNominalWall ThicknessInchesTensileStrengthksiYield Strengthat 0.2% OffsetksiElongation in2 Inches or 4D%Up to 3.0, incl 0.028 to 0.250, incl 46.0 38.0 4Over 3.0 to 8.5, incl 0.094 to 1.188, incl 44.0 33.0 4Table 3B - Min
19、imum tensile properties, SI unitsNominalODMillimetersNominalWall ThicknessMillimetersTensileStrengthMPaYield Strengthat 0.2% OffsetMPaElongationin 50.8 mm or 4D%Up to 76, incl 0.71 to 6.35, incl 317 262 4Over 76 to 216, incl 2.39 to 30.18, incl 303 228 43.4.1.3 Hollow ProfilesTable 4 - Minimum tensi
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS4352J2017MAGNESIUMALLOYEXTRUSIONS55ZN045ZRZK60AT5PRECIPITATIONHEATTREATEDUNSM16600PDF

链接地址:http://www.mydoc123.com/p-1021566.html