SAE AMS 4651C-2005 Copper-Beryllium Alloy Bars and Rods 98Cu - 1 9Be (CDA 172) Hard Temper (TD04) (UNS C17200)《(CDA 172)淬火(TD04)铜铍合金棒材和杆材98Cu 1 9Be》.pdf
《SAE AMS 4651C-2005 Copper-Beryllium Alloy Bars and Rods 98Cu - 1 9Be (CDA 172) Hard Temper (TD04) (UNS C17200)《(CDA 172)淬火(TD04)铜铍合金棒材和杆材98Cu 1 9Be》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4651C-2005 Copper-Beryllium Alloy Bars and Rods 98Cu - 1 9Be (CDA 172) Hard Temper (TD04) (UNS C17200)《(CDA 172)淬火(TD04)铜铍合金棒材和杆材98Cu 1 9Be》.pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、 AEROSPACE MATERIAL SPECIFICATION Copper-Beryllium Alloy, Bars and Rods 98Cu - 1.9Be (CDA 172) Hard Temper (TD04) (Composition similar to UNS C17200) AMS 4651C Superseding AMS 4651B1. SCOPE: 1.1 Form: This specification covers a copper-beryllium alloy in the form of bars and rods. 1.2 Application: T
2、hese products have been used typically for parts requiring high strength with good electrical conductivity and the nonmagnetic properties are important, but usage is not limited to such applications. 1.3 Safety - Hazardous Materials: While the materials, methods, applications, and processes describe
3、d or referenced in this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in each 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 nec
4、essary 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 supplier may work to a subsequent
5、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. Issued 1968-05 Revised 2005-07 Reaffirmed 2010-10 SAE Technical Standards Board
6、 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 therefrom, is the sole responsibilit
7、y 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 2010 SAE International All rights reserved. No part of this publication may be reproduced, stored in a r
8、etrieval 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 USA) Fax: 724-776-0790 Email: Cu
9、stomerServicesae.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/AMS4651C SAE - 2 - AMS 4651C AMS 4651C 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 1509
10、6-0001 or www.sae.org. AMS 2221 Tolerances, Copper and Copper Alloy Bars and Rods AMS 2750 Pyrometry 2.2 ASTM Publications: Available from ASTM, 100 Bar Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM B 249 General Requirements for Wrought Copper and Copper-Alloy Rod, Bar, Shape
11、s, and Forgings ASTM B 249M General Requirements for Wrought Copper and Copper-Alloy Rod, Bar, Shapes, and Forgings (Metric) ASTM E 3 Preparation of Metallographic Specimens ASTM E 8 Tension Testing of Metallic Materials ASTM E 8M Tension Testing of Metallic Materials (Metric) ASTM E 18 Rockwell Har
12、dness and Rockwell Superficial Hardness of Metallic Materials ASTM B 194 Annex Copper-Beryllium Alloy Plate, Sheet, Strip, and Rolled Bar ASTM E 112 Determining the Average Grain Size 3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the percentages by weight shown in Table 1, determined
13、by the chemical methods in accordance with ASTM B 194; by spectrochemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element (3.1.1) 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 Lea
14、d - 0.20 Copper (see 3.1.2) - 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 elements by agreement between the manufacturer or supplier and purchaser. SAE - 3 - AMS 4651C
15、AMS 4651C 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 99.5% minimum, but such determination is not required for rou
16、tine acceptance of each lot. 3.2 Condition: Solution heat treated and cold worked to hard temper (TD04), in a suitable condition for precipitation heat treatment. 3.3 Properties: The product shall conform to the following requirements: The applicable limits are those that apply to the specified (ord
17、ered) dimension. 3.3.1 As Solution Heat Treated and Cold Rolled: 3.3.1.1 Tensile Properties: Shall be shown in Table 2, determined in accordance with ASTM E 8, or ASTM E 8M: TABLE 2A - Tensile Properties, Inch/Pound Units Nominal Diameter or Distance Between Parallel Sides Inches Tensile Strength ks
18、i Elongation in 4D %, minimum Up to 0.375, incl 95.0 to 130.0 10 Over 0.375 to 1.000, incl 90.0 to 120.0 10 Over 1.000 to 2.000, incl 85.0 to 115.0 8 TABLE 2B - Tensile Properties, SI Units Nominal Diameter or Distance Between Parallel Sides Millimeters Tensile Strength MPa Elongation in 4D %, Minim
19、um Up to 9.52, incl 655 to 896 10 Over 9.52 to 25.40, incl 621 to 827 10 Over 25.40 to 50.80, incl 586 to 793 8 3.3.1.2 Hardness: Should be as shown in Table 3 or equivalent, determined in accordance with ASTM E 18, but the product shall not be rejected on the basis of hardness if the tensile proper
20、ty requirements of 3.3.1.1 are met on material from the same lot with similar nonconforming hardness. SAE - 4 - AMS 4651C AMS 4651C TABLE 3 - Hardness Nominal Diameter or Least Distance Between Parallel Sides Inches Nominal Diameter or Least Distance Between Parallel Sides Millimeters Hardness HRB O
21、ver 0.188 to 0.249, incl Over 4.78 to 6.32, incl 88 to 96 Over 0.249 to 0.375, incl Over 6.32 to 9.52, incl 92 to 103 Over 0.375 to 1.000, incl Over 9.52 to 25.40, incl 91 to 102 Over 1.000 to 2.000, incl Over 25.40 to 50.80, incl 88 to 101 3.3.1.3 Microstructure: Shall reveal not more than 6% beta
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