SAE AMS 4676E-2003 Nickel-Copper Alloy Corrosion-Resistant Bars and Forgings 66 5Ni - 3 0Al - 0 62Ti - 28Cu Hot-Finished Precipitation Hardenable (UNS N05500)《66 5Ni 3 0Al 0 62Ti 2.pdf
《SAE AMS 4676E-2003 Nickel-Copper Alloy Corrosion-Resistant Bars and Forgings 66 5Ni - 3 0Al - 0 62Ti - 28Cu Hot-Finished Precipitation Hardenable (UNS N05500)《66 5Ni 3 0Al 0 62Ti 2.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4676E-2003 Nickel-Copper Alloy Corrosion-Resistant Bars and Forgings 66 5Ni - 3 0Al - 0 62Ti - 28Cu Hot-Finished Precipitation Hardenable (UNS N05500)《66 5Ni 3 0Al 0 62Ti 2.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、Nickel-Copper Alloy, Corrosion-Resistant, Bars and Forgings66.5Ni - 3.0Al - 0.62Ti - 28CuHot-Finished, Precipitation Hardenable(Composition similar to UNS N05500)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、2 Application: These products have been used typically for parts requiring a combination of moderate strength, resistance to corrosion, and low magnetic permeability, but usage is not limited to such applications.2. APPLICABLE DOCUMENTS: The issue of the following documents in effect on the date of
3、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 document has been cancelled and no superseding document has been specified, the last p
4、ublished issue of that document shall apply.2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.AMS 2261 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and WireAMS 2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys, and C
5、obalt AlloysAMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockAMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy ForgingsAEROSPACE MATERIAL SPECIFICATIONAMS 4676EIssued JAN 196
6、4Revised MAY 2003Superseding AMS 4676DSAE 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 a
7、ny patent infringement arising therefrom, 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 2008 SAE International All rights res
8、erved. No part of this publication may 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 Can
9、ada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org Reaffirmed MAY 2008Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 4676E SA
10、E AMS 4676E- 2 -2.1 (Continued):AMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels, Corrosion and Heat-Resistant Steels and AlloysAMS 2808 Identification, Forgings2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 194
11、28-2959 or www.astm.org.ASTM E 8 Tension Testing of Metallic MaterialsASTM E 8M Tension Testing of Metallic Materials (Metric)ASTM E 10 Brinell Hardness of Metallic MaterialsASTM E 76 Chemical Analysis of Nickel-Copper Alloys3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the percentage
12、s by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 76, by spectrochemical methods, or by other analytical methods acceptable to purchaser.3.1.1 Determination not required for routine acceptance.3.1.2 Check Analysis: Composition variations shall meet the applic
13、able requirements of AMS 2269.TABLE 1 - CompositionElement min maxCarbon - 0.25Manganese - 1.50Silicon - 1.00Phosphorus (3.1.1) - 0.02Sulfur - 0.010Copper 27.00 33.00Aluminum 2.00 4.00Titanium 0.25 1.00Iron - 2.00Zinc (3.1.1) - 0.02Tin (3.1.1) - 0.006Lead (3.1.1) - 0.006Nickel remainderCopyright SAE
14、 International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 4676E SAE AMS 4676E- 3 -3.2 Condition: The product shall be supplied in the following condition:3.2.1 Bars and Forgings: Hot finished.3.2.1.1 Surface finish of
15、bars shall be as ordered.3.2.2 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-Finished: 3.3.1.1.1 Hardness: Shall be not higher than 248 HB, or equivalent (See 8.2), determined in a
16、ccordance with ASTM E 10.3.3.1.2 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), holding at heat for 8 to 16 hours, and furnace cooling at a rate of 15 to 25 F (8 to 14 C)
17、degrees 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), holding at heat up to 16 hours, and furnace cooling in steps of 100 F (56 C) degrees to
18、 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 Tensile Properties: Shall be as shown in Table 2, determined in accordance with ASTM
19、E 8 or ASTM E 8M.3.3.1.2.1.1 Round bars over 4.25 inches (108 mm) in diameter and over 12 feet (3.7 m) in length may have elongation as low as 17%.TABLE 2 - Minimum Tensile PropertiesProperty ValueTensile Strength 140 ksi (965 MPa)Yield Strength at 0.2% Offset 100 ksi (689 MPa)Elongation in 4D 20% (
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