SAE AMS 4530J-2011 Copper-Beryllium Alloy Sheet Strip and Plate 98Cu - 1 9Be Solution Heat Treated (TB00) (UNS C17200)《固溶热处理(TB00)的含98Cu-1 9Be铍铜合金薄板 带材和板材》.pdf
《SAE AMS 4530J-2011 Copper-Beryllium Alloy Sheet Strip and Plate 98Cu - 1 9Be Solution Heat Treated (TB00) (UNS C17200)《固溶热处理(TB00)的含98Cu-1 9Be铍铜合金薄板 带材和板材》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4530J-2011 Copper-Beryllium Alloy Sheet Strip and Plate 98Cu - 1 9Be Solution Heat Treated (TB00) (UNS C17200)《固溶热处理(TB00)的含98Cu-1 9Be铍铜合金薄板 带材和板材》.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 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/AMS4530JAEROSPACEMATERIALSPECIFICATIONAMS4530 REV. J Issued 1946-01 Revised 2011-09Supersedin
5、g AMS4530H Copper-Beryllium Alloy Sheet, Strip, and Plate 98Cu - 1.9Be Solution Heat Treated (TB00) (Composition similar to UNS C17200) RATIONALE AMS4530J corrects an error in temperature conversion (3.3.4). 1. SCOPE 1.1 Form This specification covers one type of copper-beryllium alloy in the form o
6、f sheet, strip, and plate. 1.2 Application This product has been used typically for parts requiring high strength with good electrical conductivity or lack of magnetic susceptibility, but usage is not limited to such applications. 1.3 Safety-Hazardous Materials While the materials, methods, applicat
7、ions, and processes described or referenced in this specification may involve the use of hazardous materials, this specification 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 hazardo
8、us materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved. 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 supplie
9、r 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 SAE Internationa
10、l, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS2222 Tolerances, Copper and Copper Alloy Sheet, Strip, and Plate SAE AMS4530J Page 2 of 6 2.2 ASTM Publications Available from ASTM International, 100 Barr Ha
11、rbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM B 194 Copper-Beryllium Alloy Plate, Sheet, Strip, and Rolled Bar ASTM B 194 Annex - Chemical Analysis of Copper-Beryllium Alloys ASTM B 248 General Requirements for Wrought Copper and Copper-Alloy Plate
12、, Sheet, Strip, and Rolled Bar ASTM B 601 Temper Designations of Copper and Copper Alloys - Wrought and Cast ASTM E 3 Preparation of Metallographic Specimens 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 A
13、lloys 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 B 194 and/or ASTM E 478, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 - COMPOSITION E
14、lement min max Beryllium 1.80 2.00 Nickel + Cobalt 0.20 - Nickel + Cobalt + 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 preclude the presence of other elements. Limits may be established and analysis re
15、quired 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 listed elements and 100%, or as the result of direct analysis. 3.1.3 When all the elements in Table 1 are an
16、alyzed, the sum shall be 99.5% minimum, but such determination is not required for routine acceptance of each lot. 3.2 Condition Solution heat treated (Temper TB00). SAE AMS4530J Page 3 of 6 3.3 Properties 3.3.1 Tensile Properties Shall be as shown in Table 2, determined in accordance with ASTM E 8/
17、E 8M; elongation requirements apply only to product 0.004 inch (0.10 mm) and over in nominal thickness. TABLE 2 - TENSILE PROPERTIES Property Value Tensile Strength 60.0 to 78.0 ksi (414 to 538 MPa) Elongation 35% minimum 3.3.2 Microstructure Product shall contain not more than 6% beta phase constit
18、uent, determined at 100X magnification on specimens prepared in accordance with ASTM E 3. Product may be precipitation heat treated before examination. 3.3.3 Grain Count and Grain Size Shall be as specified in Table 2, determined in accordance with ASTM B 194. Product may be precipitation heat treat
19、ed as in 3.4 prior to examination. TABLE 3A - GRAIN COUNT/SIZE, INCH/POUND UNITS Nominal Thickness Inches Grain Count Minimum Average Grain Size mm, max Over 0.004 to 0.006, incl 6 - Over 0.006 to 0.008, incl 7 - Over 0.008 to 0.010, incl 8 - Over 0.010 to 0.030, incl - 0.035 Over 0.030 to 0.090, in
20、cl - 0.045 Over 0.090 to 0.188, incl - 0.060 TABLE 3B - GRAIN COUNT/SIZE, SI UNITS Nominal Thickness MillimetersGrain Count Minimum Average Grain Size mm, max Over 0.10 to 0.15, incl 6 - Over 0.15 to 0.20, incl 7 - Over 0.20 to 0.25, incl 8 - Over 0.25 to 0.76, incl - 0.035 Over 0.76 to 2.29, incl -
21、 0.045 Over 2.29 to 4.78, incl - 0.060 3.3.4 Response to Precipitation Heat Treatment Product shall have the following properties after being precipitation heat treated by heating to 600 to 675 F (315 to 357 C), holding at heat for 2 to 3 hours and cooling in air. 3.3.4.1 Tensile Properties Shall be
22、 as specified in Table 4, determined in accordance with ASTM E 8/E 8M. SAE AMS4530J Page 4 of 6 TABLE 4A - TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness Inches Tensile Strength ksi, min Tensile Strength ksi, max Yield Strength at 0.2% Offset ksi, min Elongationin 2 Inches or 4D %, min Up to
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