SAE AMS 4650M-2013 Copper-Beryllium Alloy Bars Rods Shapes and Forgings 98Cu - 1 9Be Solution Heat Treated TB00 (A) (UNS C17200)《溶解热处理TB00(A)铜铍合金棒材 棒条体 板材和铸件98Cu 1 9Be》.pdf
《SAE AMS 4650M-2013 Copper-Beryllium Alloy Bars Rods Shapes and Forgings 98Cu - 1 9Be Solution Heat Treated TB00 (A) (UNS C17200)《溶解热处理TB00(A)铜铍合金棒材 棒条体 板材和铸件98Cu 1 9Be》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4650M-2013 Copper-Beryllium Alloy Bars Rods Shapes and Forgings 98Cu - 1 9Be Solution Heat Treated TB00 (A) (UNS C17200)《溶解热处理TB00(A)铜铍合金棒材 棒条体 板材和铸件98Cu 1 9Be》.pdf(7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/AMS4650M AEROSPACE MATERIAL SPECIFICATION AMS4650 REV. M Issued 1939-12 Revised 2013-02 Super
5、seding AMS4650L Copper-Beryllium Alloy, Bars, Rods, Shapes, and Forgings 98Cu - 1.9Be Solution Heat Treated TB00 (A) (Composition similar to UNS C17200) RATIONALE AMS4650M revises requirements for chemical analysis (3.1) and Heat Treatment (3.3), and is a Five Year Review and update of this specific
6、ation. 1. SCOPE This specification covers a copper-beryllium alloy in the form of bars, rods, shapes, and forgings. 1.1 Application These products have been used typically for parts after aging requiring a combination of high strength, good wear resistance, and corrosion resistance and where electri
7、cal conductivity or low magnetic susceptibility may be important, but usage is not limited to such applications. 1.2 Safety - Hazardous Materials While the materials, methods, applications, and processes described or referenced in this specification may involve the use of hazardous materials, this s
8、pecification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.
9、 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 referenced
10、 document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. SAE AMS4650M Page 2 of 7 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Can
11、ada) or 724-776-4970 (outside USA), www.sae.org. AMS2221 Tolerances, Copper and Copper Alloy Bars and Rods AMS2750 Pyrometry AMS2808 Identification, Forgings 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-
12、9585, www.astm.org. ASTM B 249/B 249M Specification for General Requirements for Wrought Copper and Copper-Alloy Rod, Bar, Shapes, and Forgings ASTM E 3 Practice for Preparation of Metallographic Specimens ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 18 Rockwell Hardness of Metallic Ma
13、terials ASTM E 112 Determining Average Grain Size 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 o
14、ther analytical methods acceptable to purchaser. TABLE 1 - COMPOSITION Element min max Beryllium 1.80 2.00 Nickel plus Cobalt 0.20 - Nickel plus Cobalt plus Iron - 0.6 Aluminum - 0.20 Silicon - 0.20 Copper (3.1.2) remainder Sum of Named Elements (3.1.3) 99.5 - 3.1.1 These composition limits do not p
15、reclude the presence of other elements. Limits may be established and analysis required for unnamed elements by agreement between the manufacturer or supplier and purchaser. SAE AMS4650M Page 3 of 7 3.1.2 Copper may be reported as “remainder”, or as the difference between the sum of results for all
16、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 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: 3.2.1 Bars
17、, Rods, and Shapes Hot or cold worked to size, solution heat treated, and cold straightened if necessary. 3.2.1.1 The cross-sectional area of bars, rods, and shapes shall be less than one-half that of the ingots from which they are formed; i.e., bars, rods, and shapes shall have been subjected to ov
18、er 50% reduction of area during formation. 3.2.2 Forgings Solution heat treated. 3.2.3 Stock for Forging As ordered by the forging manufacturer. 3.3 Heat Treatment Product shall be solution heat treated by heating within the range 1400 to 1475 F (760 to 802 C), holding at heat for a minimum time of
19、30 minutes, and quenching in water. Pyrometry shall be in accordance with AMS2750. 3.4 Properties The product shall conform to the following requirements: 3.4.1 As Solution Heat Treated (TB00) 3.4.1.1 Bars, Rods, and Shapes 3.4.1.1.1 Tensile Properties Shall be as shown in Table 2, determined in acc
20、ordance with ASTM E 8/E 8M; elongation requirement applies only to product over 0.311 inch (7.90 mm) in nominal diameter or distance between parallel sides. TABLE 2 - TENSILE PROPERTIES Property Value Tensile Strength, maximum 85.0 ksi (586 MPa) Elongation in 2 inches (50.8 mm), minimum 35% 3.4.1.1.
21、2 Maximum Average Grain Size Shall be not larger than shown in Table 3, determined in accordance with ASTM E 112. Product may be precipitation heat treated as in 3.4.2 before examination. SAE AMS4650M Page 4 of 7 TABLE 3 - MAXIMUM AVERAGE GRAIN SIZE Nominal Diameter or Least Distance Between Paralle
22、l Sides Inches Nominal Diameter or Least Distance Between Parallel Sides Millimeters Maximum Grain Size Millimeter Up to 1.000, excl Up to 25.40, excl 0.050 Over 1.000 to 1.500, excl Over 25.40 to 38.10, excl 0.075 Over 1.500 to 2.000, excl Over 38.10 to 50.80, excl 0.100 Over 2.000 to 3.000 excl Ov
23、er 50.80 to 76.20 excl 0.125 3.4.1.2 Forgings 3.4.1.2.1 Hardness Shall be not higher than 85 HRB, or equivalent, determined in accordance with ASTM E 18. 3.4.1.2.2 Average Grain Size Shall be as agreed upon by purchaser and vendor, determined in accordance with ASTM E 112. 3.4.1.2.3 Average Grain Fl
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