SAE AMS 4596B-2010 Copper Nickel Tin Alloy Bars and Rods 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶煅烧和调幅硬化(TX00)的77Cu15Ni8Sn铜镍锡合金条材 棒材和管材》.pdf
《SAE AMS 4596B-2010 Copper Nickel Tin Alloy Bars and Rods 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶煅烧和调幅硬化(TX00)的77Cu15Ni8Sn铜镍锡合金条材 棒材和管材》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4596B-2010 Copper Nickel Tin Alloy Bars and Rods 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶煅烧和调幅硬化(TX00)的77Cu15Ni8Sn铜镍锡合金条材 棒材和管材》.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 20 SAE International All rights reserved. No part of this publication may
3、 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 USA
4、) 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/AMS4596B AEROSPACE MATERIAL SPECIFICATION AMS4596 REV. B Issued 2002-11 Reaffirmed 2007-11 Revi
5、sed 2010-12 Superseding AMS4596A Copper Nickel Tin Alloy, Bars and Rods 77Cu 15Ni 8Sn Solution Annealed and Spinodal Hardened (TX 00) (Composition similar to UNS C72900) RATIONALE AMS4596B revises condition (3.2) and quality (3.5.1, 4.3.1.4), and removes tubes as an applicable product form. This all
6、oy in the form of mechanical tubing is specified by AMS4598. 1. SCOPE 1.1 Form This specification covers a copper-nickel-tin alloy in the form of bars and rods. When tube is ordered to AMS4596, it shall be supplied to AMS4598. 1.2 Application These products have been used typically for parts requiri
7、ng 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 to the extent specified her
8、ein. 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 Publications Available from
9、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 10SAE AMS4596B Page 2 of 5 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West
10、 Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 249/B 249M General Requirements for Wrought Copper and Copper-Alloy Rod, Bar, Shapes, and Forgings ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 18 Rockwell Hardness of Metallic Materials ASTM E 478 Chemical Analysis
11、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 purchaser. TABLE 1 - COMPOSITION Elem
12、ent (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 presence of other elements. Limit
13、s 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 direct analysis. 3.1.3 When all
14、 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 Input material is vertically continous cast, hot worked by extrusion or forging and, if necessary, cold finished. Thermal treatments inclu
15、de solution annealing followed by spinodal hardening to the TX00 temper (See 8.2). SAE AMS4596B 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 a
16、t heat for 45 to 360 minutes and water quench in 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, the
17、n air cool or quench (TX 00 temper, see 8.2). 3.4 Properties The 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 (BARS, RODS) Nominal Thickness B
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