SAE AMS 4893D-2017 Alloy Castings Corrosion and Heat-Resistant 66Ni - 29Cu - 4 0Si Solution Treated (UNS N04019).pdf
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1、_ SAE 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 any patent infringement arising there
2、from, is the sole responsibility 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 2017 SAE International All rights reserved. No part of this p
3、ublication 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 Canada) Tel: +1 724-776-497
4、0 (outside USA) Fax: 724-776-0790 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/AMS4893D AEROSPACE MATERIAL SPECIFICATION AMS4893 REV. D Issued 1959-01 Revised 2017-08 Superse
5、ding AMS4893C Alloy Castings, Corrosion and Heat-Resistant 66Ni - 29Cu - 4.0Si Solution Treated (Composition similar to UNS N04019) RATIONALE AMS4893D revises Composition (3.1) to replace a withdrawn chemical analysis standard, Radiographic acceptance (3.7.4.1), Quality (3.7.5.1), Reports (4.5), and
6、 Control Factors (4.4.2.1), and results from a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers a nickel-copper alloy in the form of castings. 1.2 Application These castings have been used typically for parts requiring resistance to wear and galling unde
7、r light-to-medium loads against dissimilar materials of higher hardness, and retention of hot hardness up to 1000 F (538 C), and where improved machinability or grinding over that of as-cast material is desired, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the
8、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 specific document issue is specified. When the referenced document has been cancelled and no supers
9、eding 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: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2175 Casting
10、s, Classification and Inspection of AMS2694 In-Process Welding of Aerospace Castings AMS2750 Pyrometry SAE INTERNATIONAL AMS4893D Page 2 of 6 AMS2804 Identification, Castings ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 2.2 ASTM Publications Available from ASTM Internationa
11、l, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM E10 Brinell Hardness of Metallic Materials ASTM E76 Chemical Analysis of Nickel-Copper Alloys ASTM E140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers
12、Hardness, Rockwell Hardness, Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness ASTM E272 Reference Radiographs for High-Strength Copper-Base and Nickel-Copper Alloy Castings ASTM E478 Chemical Analysis of Copper Alloys ASTM E1417/E1417M Liquid Penetrant Testing ASTM E1742
13、E1742M Radiographic Examination 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 E478, by spectrochemical methods or by other analytical methods acceptable to purchaser. Table 1 - Composi
14、tion Element Min Max Nickel 60.0 - Copper 27.0 31.0 Silicon 3.5 4.5 Iron - 2.5 Manganese - 1.5 Cobalt - 1.0 Carbon - 0.25 Sulfur - 0.015 3.2 Condition Solution heat treated (see 3.5). 3.2.1 Centrifugal Castings Shall be rough turned and bored. 3.2.2 Sand Castings Solid round bars shall be rough turn
15、ed. SAE INTERNATIONAL AMS4893D Page 3 of 6 3.3 Casting Castings shall be produced in lots from metal conforming to 3.1. A lot shall be all castings produced from one furnace melt or crucible melt. When two or more furnace melts or crucible melts or combination thereof are used to charge a ladle for
16、pouring, the castings therefrom shall constitute a lot. A lot shall be not more than 2000 pounds (907 kg) of castings. 3.4 Chemical Analysis Specimens Shall be cast from each melt and shall be of any convenient size, shape, and form. When chemical analysis specimens are required by purchaser, specim
17、ens shall be cast to a size, shape, and form agreed upon by purchaser and producer. 3.5 Heat Treatment Castings shall be solution heat treated by heating from 1600 F to 1650 F (871 C to 899 C), holding at heat for 1 hour per inch (25 mm) of thickness for sections 1 inch (25 mm) and under plus an add
18、itional 1 hour per inch (25 mm) of cross section over 1 inch (25 mm), rapid furnace cooling to or transferring to another furnace held at 1200 F to 1300 F (649 C to 704 C), holding at heat for 30 minutes or until uniform temperature has been attained, and quenching in low-sulfur oil. For complicated
19、 sections, parts should be charged into a furnace which is at a temperature not higher than 600 F (316 C). Pyrometry shall be in accordance with AMS2750. 3.6 Response to Heat Treatment Castings shall conform to the following requirements: 3.6.1 Hardness as Solution Heat Treated Shall be not higher t
20、han 269 HB or equivalent (see 8.4) determined in accordance with ASTM E10. 3.6.2 Hardness after Precipitation Heat Treatment Shall be not lower than 302 HB, or equivalent, determined in accordance with ASTM E10, after being precipitation heat treated by heating to 1100 F 25 F (593 C 14 C), holding a
21、t heat for 4 to 6 hours, and air or furnace cooling. 3.7 Quality 3.7.1 Castings, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the castings. 3.7.1.1 Castings shall have smooth surfaces and sh
22、all be sufficiently cleaned to permit fluorescent penetrant inspection. Metallic shot or grit shall not be used for final cleaning. 3.7.2 Castings shall be produced under radiographic control. This control shall consist of radiographic examination of castings in accordance with ASTM E1742 until prop
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