SAE AMS 4863-2015 Copper-Nickel-Tin Alloy Castings Cu C 15Ni C 8Sn Hot Isostatically Pressed Solution Annealed and Spinodal Heat Treated (UNS C96900).pdf
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1、AEROSPACE MATERIAL SPECIFICATION AMS4863 Issued 2015-02 Copper-Nickel-Tin Alloy Castings Cu 15Ni 8Sn Hot Isostatically Pressed, Solution Annealed and Spinodal Heat Treated (Composition similar to UNS C96900) RATIONALE AMS4863 is a new specification for copper-nickel-tin alloy castings. 1. SCOPE 1.1
2、Form This specification covers a copper-nickel-tin alloy in the form of castings, made using the investment process unless sand or centrifugal processes are agreed upon by the purchaser. 1.2 Application These copper alloy castings are for use as non-magnetic small parts of intricate design requiring
3、 good corrosion resistance and anti-friction and wear characteristics with high strength, 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
4、 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 published issue of that document shall apply. 2.1 SAE Publications Available f
5、rom SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2360 Room Temperature Tensile Properties of Castings AMS2750 Pyrometry AMS2804 Identification, Castings _ SAE Technical Standards Board R
6、ules 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 responsibility
7、of the user.” 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 2015 SAE International All rights reserved. No part of this publication may be reproduced, sto
8、red 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: 724-776-0790
9、 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/AMS4863 SAE INTERNATIONAL AMS4863 Page 2 of 6 2.2 ASTM Publications Available from ASTM International, 100 Barr Ha
10、rbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM E8/E8M Tension Testing of Metallic Materials ASTM E18 Rockwell Hardness of Metallic Materials ASTM E29 Using Significant Digits in Test Da
11、ta to Determine Conformance with Specifications ASTM E272 Reference Radiographs for High-Strength Copper-Base and Nickel-Copper Alloy Castings ASTM E478 Chemical Analysis of Copper Alloys ASTM E1417 Liquid Penetrant Testing ASTM E1742 Radiographic Examination 3. TECHNICAL REQUIREMENTS 3.1 Compositio
12、n Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E478, by spectro-chemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element (3.1.1) min max Nickel (+ Cobalt) 14.5 15.5 Tin 7.5 8.5 I
13、ron - 0.50 Zinc - 0.50 Manganese - 0.30 Columbium - 0.10 Magnesium - 0.15 Lead - 0.02 Copper (3.1.2) remainder Copper + 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 elemen
14、ts 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 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.
15、5% minimum, but such determination is not required for routine acceptance of each lot. 3.1.4 Test results may be rounded in accordance with the “rounding off” method of ASTM E29. SAE INTERNATIONAL AMS4863 Page 3 of 6 3.2 Condition Hot isostatically pressed, solution heat treated and spinodally harde
16、ned. 3.3 Casting Castings shall be made by the investment casting process unless another process is agreed to by purchaser. Castings shall be poured from a single furnace charge of not more than 2000 pounds (907 kg). The furnace charge may consist of virgin material, gates, sprues, risers, or other
17、recycled material. 3.4 Heat Qualification Each heat shall be qualified by chemical analysis and tensile specimens conforming to 3.4.1 and 3.4.2 respectively. Heat identity of all specimens and parts shall be maintained through all operations. 3.4.1 Chemical Analysis Specimens Shall be cast from each
18、 heat after the last melt addition, and shall be of any suitable size, shape, and form. 3.4.2 Tensile Specimens Unless otherwise specified by the purchaser, specimens shall be cast separately as net shape tensile specimens which are ready for testing after heat treatment (3.5). Specimens shall be of
19、 standard proportions in accordance with ASTM E8/E8M with 0.350 inch (8.89 mm) diameter at the reduced parallel gage section or shall be prepared as agreed upon with purchaser. 3.5 Heat Treatment All castings and representative tensile specimens shall be subjected to hot isostatic pressing (HIP) in
20、the as-cast condition, followed by solution annealing and spinodal heat treatment. Pyrometry shall be in accordance with AMS2750. Hot isostatic pressing, solution heat treatment and spinodal hardening heat treatment practices are proprietary. 3.6 Properties Separately-cast net shape tensile samples
21、shall conform to the following requirements: 3.6.1 Tensile Properties Shall be as shown in Table 2, determined in accordance with ASTM E8/E8M on specimens in accordance with 3.4.2. Table 2 - Minimum tensile properties Property Value Tensile Strength 113 ksi (779 MPa) Yield Strength at 0.2% Offset 96
22、 ksi (662 MPa) Elongation in 4D 2% 3.6.2 Hardness Shall be not lower than HBW277, or equivalent, determined in accordance with ASTM E18. 3.6.3 When properties other than those of 3.6.1 and 3.6.2 are required, the engineering drawing or purchase order shall specify tensile property and hardness limit
23、s. Property requirements may be designated in accordance with AMS2360. 3.6.4 Microstructure When specified, microstructure and grain size shall conform to standards acceptable to purchaser. SAE INTERNATIONAL AMS4863 Page 4 of 6 3.7 Quality 3.7.1 Castings, as received by purchaser, shall be uniform i
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