SAE AMS 5894D-2016 Cobalt Alloys Bars Sheet and Plate 60Co - 28Cr - 4 5W - 1 15C Solution Heat Treated.pdf
《SAE AMS 5894D-2016 Cobalt Alloys Bars Sheet and Plate 60Co - 28Cr - 4 5W - 1 15C Solution Heat Treated.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5894D-2016 Cobalt Alloys Bars Sheet and Plate 60Co - 28Cr - 4 5W - 1 15C Solution Heat Treated.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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2016 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/AMS5894D AEROSPACE MATERIAL SPECIFICATION AMS5894 REV. D Issued 1993-01 Revised 2
5、016-02 Superseding AMS5894C Cobalt Alloys, Bars, Sheet, and Plate 60Co 28Cr 4.5W 1.15C Solution Heat Treated RATIONALE AMS5894D revises Condition (3.2.2.1), Properties (3.4.1.1) and Reports (4.4), and is a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers
6、 a cobalt alloy in the form of sheet and plate up to 1 inch (25 mm) in nominal thickness or round bars up to 3 1/2 inches (89 mm) in nominal diameter (see 8.4). 1.2 Application These products have been used typically for parts requiring wear resistance and minimum galling or seizing tendencies at ro
7、om and elevated temperatures, 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 of a
8、 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, Warrendale, P
9、A 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2261 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire AMS2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys and Cobalt Alloys AMS2371 Quality Assurance Sampling an
10、d Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock AMS2750 Pyrometry SAE INTERNATIONAL AMS5894D Page 2 of 5 AMS2806 Identification Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS2
11、807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys, Sheet, Strip, Plate, and Aircraft Tubing 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.
12、ASTM A480/A480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and Strip ASTM E8/E8M Tension Testing of Metallic Materials ASTM E18 Rockwell Hardness of Metallic Materials ASTM E354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel and Cobalt A
13、lloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E354, by spectrochemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element min max Carb
14、on 0.90 1.40 Manganese 0.5 2.0 Silicon 0.2 2.0 Phosphorus - 0.04 Sulfur - 0.03 Chromium 28.00 32.00 Tungsten 3.50 5.50 Nickel - 3.0 Molybdenum - 1.50 Iron - 3.0 Cobalt remainder 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. 3.2 Condition The product s
15、hall be supplied in the following condition: 3.2.1 Sheet and Plate Hot rolled, solution heat treated and descaled with a No. 1 finish appearance as described in ASTM A480/A480M. SAE INTERNATIONAL AMS5894D Page 3 of 5 3.2.2 Bar Solution heat treated with a turned or ground finish. 3.2.2.1 Bars shall
- 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:
- SAEAMS5894D2016COBALTALLOYSBARSSHEETANDPLATE60CO28CR45W115CSOLUTIONHEATTREATEDPDF

链接地址:http://www.mydoc123.com/p-1022271.html