SAE AMS 4640H-2011 Aluminum Bronze Bars Rods Shapes Tubes and Forgings 81 5Cu - 10 0Al - 4 8Ni - 3 0Fe Drawn and Stress Relieved (HR50) or Temper Annealed (TQ50) (UNS C63000)《拉伸和消除.pdf
《SAE AMS 4640H-2011 Aluminum Bronze Bars Rods Shapes Tubes and Forgings 81 5Cu - 10 0Al - 4 8Ni - 3 0Fe Drawn and Stress Relieved (HR50) or Temper Annealed (TQ50) (UNS C63000)《拉伸和消除.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4640H-2011 Aluminum Bronze Bars Rods Shapes Tubes and Forgings 81 5Cu - 10 0Al - 4 8Ni - 3 0Fe Drawn and Stress Relieved (HR50) or Temper Annealed (TQ50) (UNS C63000)《拉伸和消除.pdf(8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/AMS4640H AEROSPACE MATERIAL SPECIFICATION AMS4640 REV. H Issued 1940-06 Revised 2011-05Supers
5、eding AMS4640G Aluminum Bronze, Bars, Rods, Shapes, Tubes, and Forgings 81.5Cu - 10.0Al - 4.8Ni - 3.0Fe Drawn and Stress Relieved (HR50) or Temper Annealed (TQ50) (Composition similar to UNS C63000) RATIONALE AMS4640H revises 3.3.3 to correct the proper designation of ASTM B 858, and results from a
6、Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum bronze alloy in the form of bars, rods, shapes, tubes, forgings, and forging stock. 1.2 Application These products have been used typically for parts requiring strength and wear resistance at m
7、oderate 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 documen
8、t 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, PA 15096-
9、0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2221 Tolerances, Copper and Copper Alloy Bars and Rods AMS2223 Tolerances, Copper and Copper Alloy Seamless Tubing AMS2808 Identification, Forgings SAE AMS4640H Page 2 of 8 2.2 ASTM Publications Available
10、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 154 Mercurous Nitrate Test for Copper and Copper Alloys ASTM B 249/B 249M General Requirements for Wrought Copper and Copper-Alloy Rod, Bar, Shapes, and Forgings A
11、STM B 251 General Requirements for Wrought Seamless Copper and Copper-Alloy Tube ASTM B 251M General Requirements for Wrought Seamless Copper and Copper-Alloy Tube (Metric) ASTM B 858 Ammonia Vapor Test for Determining Susceptibility to Stress Corrosion Cracking in Copper Alloys ASTM E 8/E 8M Tensio
12、n Testing of Metallic Materials 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 me
13、thods acceptable to purchaser. TABLE 1 - COMPOSITION Element (3.1.1) min max Aluminum 9.0 11.0 Nickel 4.0 5.5 Iron 2.0 4.0 Manganese - 1.5 Zinc 0.30Tin 0.20Silicon - 0.25 Copper + Silver (3.1.2) remainder Copper + Silver + Sum of Named Elements (3.1.3) 99.5 - 3.1.1 These composition limits do not pr
14、eclude 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 Copper and silver may be reported as “remainder“, or as the difference between the sum of results for all elements and 10
15、0%, or as the result of direct analysis. 3.1.3 When all named elements in Table 1 are analyzed, the sum shall be 99.5 percent minimum, but such determination is not required for routine acceptance of each lot. SAE AMS4640H Page 3 of 8 3.2 Condition The product shall be supplied in the following cond
16、ition: 3.2.1 Bars, Rods, Shapes, and Tubes Hot rolled or extruded, drawn or otherwise cold finished if necessary, and annealed by heating within the range 1100 to 1300 F (593 to 704 C) and cooling in air (HR50 temper - See 8.2). 3.2.2 Forgings Quenched in room temperature water from 1625 F 25 (885 C
17、 14), annealed by heating within the range 1100 to 1300 F (593 to 704 C), and cooling in air (TQ50 temper - See 8.2). 3.2.3 Forging Stock As ordered by the forging manufacturer. 3.3 Properties The product shall conform to the following requirements: 3.3.1 Tensile Properties Shall be as follows, dete
18、rmined in accordance with ASTM E 8/E 8M. 3.3.1.1 Rounds, Hexagons, and Octagons (Bars, Rods and Shapes) Shall be as shown in Table 2. TABLE 2A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS Nominal Diameter or Distance Between Parallel Sides Inches Tensile Strength ksi Yield Strength at 0.5% Extensi
19、on Under Load ksi Elongation in 4D % Up to 1.00, incl Over 1.00 to 2.00, incl Over 2.00 to 3.00, incl Over 3.00 to 5.00, incl 110 110 105 100 68.0 60.0 55.0 50.0 10 10 10 10 TABLE 2B - MINIMUM TENSILE PROPERTIES, SI UNITS Nominal Diameter or Distance Between Parallel Sides Millimeters Tensile Streng
20、th MPa Yield Strength at 0.5% Extension Under Load MPa Elongation in 4D % Up to 25.4, incl Over 25.4 to 50.8, incl Over 50.8 to 76.2, incl Over 76.2 to 127.0, incl 758 758 724 689 469 414 379 345 10 10 10 10 SAE AMS4640H Page 4 of 8 3.3.1.2 Flats, Squares, Shapes (Bars), and Tubes Shall be as shown
21、in Table 3. TABLE 3A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness or OD Inches Tensile Strength ksi Yield Strength at 0.5% Extension Under Load ksi Elongation in 4D % Up to 1.00, incl Over 1.00 to 3.00, incl Over 3.00 100 95.0 90.0 52.0 50.0 48.0 10 10 10 TABLE 3B - MINIMUM TENSI
22、LE PROPERTIES, SI UNITS Nominal Thickness or OD Millimeters Tensile Strength MPa Yield Strength at 0.5% Extension Under Load MPa Elongation in 4D % Up to 25.4, incl Over 25.4 to 76.2, incl Over 76.2 689 655 621 359 345 330 10 10 10 3.3.1.3 Forgings As specified by producer. 3.3.2 Hardness Shall be a
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