SAE AMS 4598A-2012 Copper Nickel Tin Alloy Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和旋接线硬化(TX 00)77Cu 15Ni 8Sn铜镍矿锡合金机械管》.pdf
《SAE AMS 4598A-2012 Copper Nickel Tin Alloy Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和旋接线硬化(TX 00)77Cu 15Ni 8Sn铜镍矿锡合金机械管》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4598A-2012 Copper Nickel Tin Alloy Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和旋接线硬化(TX 00)77Cu 15Ni 8Sn铜镍矿锡合金机械管》.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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2012 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/AMS4598A AEROSPACE MATERIAL SPECIFICATION AMS4598 REV. A Issued 2010-12 Revised 2012-09 Super
5、seding AMS4598 Copper Nickel Tin Alloy, Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX 00) (Composition similar to UNS C72900) RATIONALE AMS4598A corrects an error in the converted metric value for tensile yield strength in forward extruded product (Table 2). 1. SCOPE
6、1.1 Form This specification covers a copper-nickel-tin alloy in the form of mechanical tube (See 8.8). 1.2 Application These products have been used typically for parts requiring high strength, wear resistance, and corrosion resistance at moderate temperatures, but usage is not limited to such appli
7、cations. 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 document unless a specific document issue is specified. When the re
8、ferenced 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, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4
9、970 (outside USA), www.sae.org. AMS2750 Pyrometry SAE AMS4598A Page 2 of 6 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. ASTM B 251 General Requirements for Wrought Seamless Copper and
10、 Copper-Alloy Tube ASTM B 251M General Requirements for Wrought Seamless Copper and Copper-Alloy Tube (Metric) ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 18 Rockwell Hardness of Metallic Materials ASTM E 478 Chemical Analysis of Copper Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition
11、 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 Element (3.1.1) min max Nickel (+ Cobalt) 14.5 15.5 Tin 7.5 8.
12、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. Limits may be established and analysis required for unnamed ele
13、ments 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 the elements in the table are analyzed, the sum shall be
14、99.5% minimum, but such determination is not required for routine acceptance of each lot. 3.2 Condition The product shall be supplied in the following condition: Vertically continuously cast, extruded, and, if necessary, cold finished; solution annealed and spinodal hardened to the TX 00 temper (See
15、 8.2). SAE AMS4598A Page 3 of 6 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 room temperature water. 3.3
16、.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, See 8.2). 3.4 Properties The product sha
17、ll 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 Nominal Outside Diameter* (tube) Ultimate Tensile Strength Yield Strength (at 0.2% offset) Elongation in 4D
18、1.100 (28 mm) to 7.250 inches (184 mm), incl (A) 131 ksi (903 MPa) 104 ksi (717 MPa) 8% 7.250 (184 mm) to 13.6 inches (330 mm) (B) 130 ksi (896 MPa) 108 ksi (745 MPa) 5% *Wall thickness is dependent on outside diameter and averages approximately 15% of OD in extrusions (A) Forward extruded, (B) Back
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