SAE AMS 4612J-2004 Brass Naval Bars and Rods 60 5Cu - 38 5Zn - 0 75Sn Hard Temper (H04)《60 5Cu 38 5Zn 0 75Sn硬化回火(H04)黄铜棒材和杆材》.pdf
《SAE AMS 4612J-2004 Brass Naval Bars and Rods 60 5Cu - 38 5Zn - 0 75Sn Hard Temper (H04)《60 5Cu 38 5Zn 0 75Sn硬化回火(H04)黄铜棒材和杆材》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4612J-2004 Brass Naval Bars and Rods 60 5Cu - 38 5Zn - 0 75Sn Hard Temper (H04)《60 5Cu 38 5Zn 0 75Sn硬化回火(H04)黄铜棒材和杆材》.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 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 2012 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/AMS4612J AEROSPACE MATERIAL SPECIFICATION AMS4612 REV. J Issued 1941-09 Revised 2
5、004-04 Reaffirmed 2012-02 Superseding AMS4612H Brass, Naval, Bars and Rods 60.5Cu - 38.5Zn - 0.75Sn Hard Temper (H04) (Composition similar to UNS C46400) RATIONALE AMS4612J has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE:1.1 Form: This specification covers a copper alloy
6、 (naval brass) in the form of bars and rods.1.2 Application: These products have been used typically for automatic screw machine parts, but usage is not limited to such applications. This material has slightly higher strength and lower ductility than AMS 4611. It also has better corrosion resistance
7、 than AMS 4610 but is less readily machinable.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 supplied herein. The supplier may work to a subsequent revision of a document unless a specific doc
8、ument 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, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.AMS 2221 Toleranc
9、es, Copper and Copper Alloy Bars and RodsAMS 4610 Brass, Free-Cutting Bars and Rods, 61.5Cu - 35Zn - 3.1Pb, Half Hard (H02)AMS 4611 Brass, Naval, Bars and Rods, 60.5Cu - 38.7Zn - 0.8Sn, Half Hard (H02)Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or
10、networking permitted without license from IHS-,-,-SAE AMS4612J Page 2 of 6 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959 or www.astm.org.ASTM B 154 Mercurous Nitrate Test for Copper and Copper AlloysASTM B 249 General Requirements
11、for Wrought Copper and Copper-Alloy Rod, Bar, Shapes and ForgingsASTM B 249M General Requirements for Wrought Copper and Copper-Alloy Rod, Bar, Shapes and Forgings (Metric)ASTM B 858 Ammonia Vapor Test for Determining Susceptibility to Stress Corrosion Cracking in Copper AlloysASTM E 8 Tension Testi
12、ng of Metallic MaterialsASTM E 8M Tension Testing of Metallic Materials (Metric)ASTM E 478 Chemical Analysis of Copper Alloys3. 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 s
13、pectrochemical methods, or by other analytical methods acceptable to purchaser.3.1.1 These composition limits do not preclude the presence 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 Zin
14、c may be reported as “remainder”, 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 named elements in Table 1 are analyzed, the sum shall be 99.6 percent minimum, but such determination is not required for routine acceptance of
15、 each lot.TABLE 1 - CompositionElement (3.1.1) min maxCopper 59.0 62.0Tin 0.50 1.00Lead - 0.20Iron - 0.10Zinc (3.1.2) remainder -Sum of Named Elements (3.1.3) 99.6 -Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license
16、 from IHS-,-,-SAE AMS4612J Page 3 of 6 3.2 Condition: Cold finished, hard (H04) temper (See 8.3).3.3 Properties: The product shall conform to the following requirements:3.3.1 Tensile Properties: Shall be as shown in Table 2, determined in accordance with ASTM E 8 or ASTM E 8M.3.3.2 Embrittlement: Sp
17、ecimens as in 4.3.2 shall withstand, without cracking, the mercurous nitrate test performed in accordance with ASTM B 154, Procedure A, or the Ammonia Vapor Test in accordance with AMS B 858.3.4 Quality: The product, as received by purchaser, shall be uniform in quality and condition, sound, and fre
18、e from foreign materials and from imperfections detrimental to usage of the product.3.5 Tolerances: Shall conform to AMS 2221 as applicable to nonrefractory alloys.TABLE 2A - Minimum Tensile Properties, Inch/Pound UnitsNominal Diameter or DistanceBetween Parallel SidesInchesTensileStrengthksiYield S
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