SAE AMS 4675E-2017 Nickel-Copper Alloy Corrosion-Resistant Bars and Forgings 67Ni - 30Cu (UNS N04400).pdf
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1、_ SAE Technical Standards Board Rules provide that: 7KLVUHSRUWLVSXEOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDO DQGHQJLQHHULQJVFLHQFHV7KHXVHRIWKLVUHSRUWLVHQWLUH ly voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is WKHVROHUHVSRQ
2、VLELOLWRIWKHXVHU SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2017 SAE International All rights reserved. No part of this publication may be reproduced,
3、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 USA) Fax: 724-776-0
4、790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AMS4675E AEROSPACE MATERIAL SPECIFICATION AMS4675 REV. E Issued 1963-07 Reaffirmed 2003-05 Revised 2017-01 Superseding AMS467
5、5D Nickel-Copper Alloy, Corrosion-Resistant, Bars and Forgings 67Ni - 30Cu (Composition similar to UNS N04400) RATIONALE AMS4675E revises Chemical Analysis Standards (3.1), Properties (3.3.1.3), and Reports (4.4), and is a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form This spe
6、cification covers a corrosion-resistant nickel-copper alloy in the form of bars 0.093 to 4.000 inches (2.35 to 100.00 mm) in diameter or distance between parallel sides, and forgings and forging stock of any size (see 8.5). 1.2 Application These products have been used typically for fittings, such a
7、s cones, nipples, and unions, in fluid line assemblies using AMS4574 or AMS4575 tubing, 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 h
8、erein. The supplier 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 fro
9、m SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2261 Tolerances Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire AMS2269 Chemical Check Analysis Limits Nickel, Nickel Alloys
10、, and Cobalt Alloys AMS2371 Quality Assurance Sampling and Testing Corrosion and Heat-Resistant Steels and Alloys Wrought Products and Forging Stock SAE INTERNATIONAL AMS4675E Page 2 of 6 AMS2374 Quality Assurance Sampling and Testing Corrosion and Heat-Resistant Steel and Alloy Forgings AMS2806 Ide
11、ntification Bars, Wire, Mechanical Tubing, and Extrusions Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS2808 Identification Forgings ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 2.2 ASTM Publications Available from ASTM International, 100 Bar
12、r Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM E8/E8M Tension Testing of Metallic Materials ASTM E18 Rockwell Hardness of Metallic Materials ASTM E140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness,
13、Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness Rockwell Hardness ASTM E1473 Chemical Analysis of Nickel, Cobalt, and High-Temperature Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemica
14、l methods in accordance with ASTM E1473, by spectrochemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element Min Max Carbon Manganese Silicon Copper Iron Nickel - - - 28.0 - remainder 0.30 2.00 0.50 34.00 2.50 3.1.1 Check Analysis Composition variations
15、shall meet the applicable requirements of AMS2269. 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Bars Cold drawn and stress relieved by heating to a temperature within the range 1000 to 1100 F (538 to 593 C), holding at the selected temperature within 25 F (14 C) for
16、1 hour 0.25 hour, and cooling at a rate equivalent to cooling in air. 3.2.1.1 Bars shall not be cut from plate (also see 4.4.2). SAE INTERNATIONAL AMS4675E Page 3 of 6 3.2.2 Forgings As forged. 3.2.3 Forging Stock As ordered by the forging manufacturer. 3.3 Properties The product shall conform to th
17、e following requirements: 3.3.1 Tensile Properties Shall be as follows, determined in accordance with ASTM E8/E8M: 3.3.1.1 Round Bars Shall be as shown in Table 2. Table 2 Table 2A - Minimum tensile properties, inch/pound units Nominal Diameter Inches Tensile Strength ksi Yield Strength at 0.2% Offs
18、et ksi Elongation in 4D % 0.093 to 0.500, excl 84 50 10 0.500 to 3.500, incl 87 60 22 Over 3.500 to 4.000, incl 84 55 25 Table 2B - Minimum tensile properties, SI units Nominal Diameter Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 4D % 2.35 to 12.50, excl 579 345
19、10 12.50 to 87.50, incl 600 414 22 Over 87.50 to 100.00, incl 579 379 25 3.3.1.2 Hexagonal, Square, and Rectangular Bars Shall be as shown in Table 3. Table 3 Table 3A - Minimum tensile properties, inch/pound units Nominal Distance Between Parallel Sides Inch Tensile Strength ksi Yield Strength at 0
20、.2% Offset ksi Elongation in 4D % 0.093 to 0.500, incl 84 50 10 0.500 and over 84 50 22 SAE INTERNATIONAL AMS4675E Page 4 of 6 Table 3B - Minimum Tensile properties, SI units Nominal Distance Between Parallel Sides Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 4D %
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