SAE AMS 4676F-2017 Nickel-Copper Alloy Corrosion-Resistant Bars and Forgings 66 5Ni - 3 0Al - 0 62Ti - 28Cu Hot-Finished Precipitation Hardenable (UNS N05500).pdf
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1、_ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSX EOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDODQGHQJL neering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any SDUWLFXODUXVHLQFOXGLQJDQSDWHQWLQIULQJHPHQWDULVLQJWKHUHIURPLVWKH VROHUHVSRQVLELOLWRIW
2、KHXVHU 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, stored in
3、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: 724-776-0790 Email:
4、 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/AMS4676F AEROSPACE MATERIAL SPECIFICATION AMS4676 REV. F Issued 1964-01 Reaffirmed 2008-05 Revised 2017-01 Superseding AMS4676E Nickel-
5、Copper Alloy, Corrosion-Resistant, Bars and Forgings 66.5Ni - 3.0Al - 0.62Ti - 28Cu Hot-Finished, Precipitation Hardenable (Composition similar to UNS N05500) RATIONALE AMS4676F revises Composition (3.1), Condition (3.2.2), and Reports (4.4), and is a Five-Year Review and update of this specificatio
6、n. 1. SCOPE 1.1 Form This specification covers a corrosion-resistant nickel-copper alloy in the form of bars, forgings, and forging stock. 1.2 Application These products have been used typically for parts requiring a combination of moderate strength, resistance to corrosion, and low magnetic permeab
7、ility, 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 document unless a spec
8、ific 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 15096-0001, Tel: 877-
9、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, and Cobalt Alloys AMS2371 Quality Assurance Sampling and Testing Corrosion and
10、Heat-Resistant Steels and Alloys Wrought Products and Forging Stock SAE INTERNATIONAL AMS4676F Page 2 of 6 AMS2374 Quality Assurance Sampling and Testing Corrosion and Heat-Resistant Steel and Alloy Forgings AMS2806 Identification Bars, Wire, Mechanical Tubing, and Extrusions Carbon and Alloy Steels
11、 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 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-958
12、5, www.astm.org. ASTM E8/E8M Tension Testing of Metallic Materials ASTM E10 Brinell Hardness of Metallic Materials ASTM E140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness Rock
13、well 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 chemical methods in accordance with ASTM E1473, by spectrochemical methods, or by other a
14、nalytical methods acceptable to purchaser. Table 1 Composition Element Min Max Carbon - 0.25 Manganese - 1.50 Silicon - 1.00 Phosphorus (3.1.1) - 0.02 Sulfur - 0.010 Copper 27.00 33.00 Aluminum 2.00 4.00 Titanium 0.25 1.00 Iron - 2.00 Zinc (3.1.1) - 0.02 Tin (3.1.1) - 0.006 Lead (3.1.1) - 0.006 Nick
15、el remainder 3.1.1 Determination not required for routine acceptance. 3.1.2 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. 3.2 Condition The product shall be supplied in the following condition: SAE INTERNATIONAL AMS4676F Page 3 of 6 3.2.1 Bars and Forgings
16、Hot finished. 3.2.1.1 Surface finish of bars shall be as ordered. 3.2.2 Bars shall not be cut from plate (also see 4.4.1). 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 Bars and Forgings 3.3.1.1 As Hot-Finish
17、ed 3.3.1.1.1 Hardness Shall be not higher than 248 HB, or equivalent (see 8.2), determined in accordance with ASTM E10. 3.3.1.2 After Precipitation Heat Treatment The product shall conform to the following requirements after being precipitation heat treated by heating to 1100 to 1125 F (593 to 607 C
18、), holding at heat for 8 to 16 hours, and furnace cooling at a rate of 15 to 25 F (8 to 14 C) per hour to 900 F (482 C). Cooling from 900 F (482 C) may be accomplished without regard to cooling rate. As an alternate method, the precipitation heat treatment may be done by heating to 1100 F (607 C), h
19、olding at heat up to 16 hours, and furnace cooling in steps of 100 F (56 C) to 1000 F (538 C), holding at heat for approximately 6 hours, furnace cooling to 900 F (482 C), holding at heat for approximately 8 hours, and cooling to room temperature at a rate equivalent to air cooling. 3.3.1.2.1 Tensil
20、e Properties Shall be as shown in Table 2, determined in accordance with ASTM E8/E8M. Table 2 - Minimum tensile properties Property Value Tensile Strength 140 ksi (965 MPa) Yield Strength at 0.2% Offset 100 ksi (689 MPa) Elongation in 4D 20% (3.3.1.2.1.1) 3.3.1.2.1.1 Round bars over 4.25 inches (108
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