SAE AMS 4595-2011 Copper Nickel Tin Alloy Plate 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和亚稳态硬化工艺制备的77Cu-15Ni-8Sn铜镍锡合金板(TX 00)》.pdf
《SAE AMS 4595-2011 Copper Nickel Tin Alloy Plate 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和亚稳态硬化工艺制备的77Cu-15Ni-8Sn铜镍锡合金板(TX 00)》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4595-2011 Copper Nickel Tin Alloy Plate 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和亚稳态硬化工艺制备的77Cu-15Ni-8Sn铜镍锡合金板(TX 00)》.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/AMS4595 AEROSPACE MATERIAL SPECIFICATION AMS4595 Issued 2011-07 Copper Nickel Tin Alloy Plate
5、 77Cu 15Ni 8Sn Solution Annealed and Spinodal Hardened (TX 00) (Composition similar to UNS C72900) RATIONALE AMS4595 is a new specification for copper-nickel-tin alloy plate. 1. SCOPE 1.1 Form This specification covers a copper-nickel-tin alloy in the form of plate . 1.2 Application Plate products a
6、re for use in parts requiring high strength, wear resistance, and corrosion resistance at moderate 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
7、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, the last published issue of that document shall apply. 2.1 SAE P
8、ublications 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. AMS2750 Pyrometry SAE AMS4595 Page 2 of 5 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Dr
9、ive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 248/B 248M General Requirements for Wrought Copper and Copper-Alloy Plate, Sheet, Strip, and Rolled Bar ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 18 Rockwell Hardness of Metallic Materials
10、ASTM E 478 Chemical Analysis of Copper Alloys 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 E 478, by spectrochemical methods, or by other analytical methods acceptable to the purchase
11、r. TABLE 1 - COMPOSITION Element (3.1.1) min max Nickel (+ Cobalt) 14.5 15.5 Tin 7.5 8.5 Iron - 0.50 Zinc - 0.50 Manganese - 0.30 Columbium - 0.10 Magnesium - 0.15 Lead - 0.02 Copper (3.1.2) remainder Copper + sum of Named Elements (3.1.3) 99.5 3.1.1 These composition limits do not preclude the pres
12、ence of other elements. Limits may be established and analysis required for unnamed elements by agreement between the manufacturer or supplier and purchaser. 3.1.2 Copper may be reported as “remainder”, or as the difference between the sum of results for all elements and 100%, or as the result of di
13、rect analysis. 3.1.3 When all the elements in the table are analyzed, the sum shall be 99.5% minimum, but such determination is not required for routine acceptance of each lot. 3.2 Condition Vertically continuous cast, hot worked and, if necessary, cold finished, solution annealed and spinodal harde
14、ned to the TX 00 temper (See 8.2). SAE AMS4595 Page 3 of 5 3.3 Heat Treatment Product shall be heat treated as follows; pyrometry shall be in accordance with AMS2750. 3.3.1 Solution Annealing Heat within the range 1450 to 1600 F (788 to 870 C), hold at heat for 45 to 360 minutes and water quench in
15、room temperature water. 3.3.2 Spinodal Hardening Heat to 600 to 800 F (315 to 425 C), hold at heat for a total time at temperature greater than 1 hour and less than 10 hours, depending on section thickness to meet the property requirements of 3.4, then air cool or quench (TX 00 temper). 3.4 Properti
16、es Product shall conform to the following requirements: 3.4.1 Tensile Properties Shall be as shown in Table 2, determined in accordance with ASTM E 8/E 8M. TABLE 2 - MINIMUM LONGITUDINAL TENSILE PROPERTIES (PLATE) Nominal Thickness Ultimate Tensile Strength Yield Strength (at 0.2% offset) Elongation
- 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:
- SAEAMS45952011COPPERNICKELTINALLOYPLATE77CUC15NIC8SNSOLUTIONANNEALEDANDSPINODALHARDENEDTX00UNSC72900

链接地址:http://www.mydoc123.com/p-1021687.html