SAE AMS 5878D-2015 Nickel Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 59Ni - 22Cr - 2Mo - 14W - 0 35AI - 0 03La Solution Heat Treated (UNS N06230).pdf
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1、AEROSPACE MATERIAL SPECIFICATION AMS5878 REV. D Issued 1990-01 Revised 2015-01 Superseding AMS5878C Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 59Ni - 22Cr - 2Mo - 14W - 0.35AI - 0.03La Solution Heat Treated (Composition similar to UNS N06230) RATIONALE AMS5878D revises Heat
2、Treatment (3.3), Properties (3.4.1), Reports (4.4, 4.4.5), and is a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate 0.015 to 1.5 inch (0.38 to 38 mm) in nominal thickness
3、 . (See 8.5). 1.2 Application These products have been used typically for parts requiring oxidation resistance up to 2100 F (1149 C) and relatively high strength up to 1800 F (982 C), but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documents in effec
4、t 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 superseding document has been spec
5、ified, 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 724-776-4970 (outside USA), www.sae.org. AMS2262 Tolerances, Nickel, Nickel Alloy, and
6、Cobalt Alloy Sheet, Strip, and Plate AMS2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys AMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock AMS2750 Pyrometry _ SAE Technical Standards Board R
7、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
8、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
9、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
10、 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/AMS5878D SAE INTERNATIONAL AMS5878D Page 2 of 6 AMS2807 Identification, Carbon and Low-Alloy Steels, Corrosion and
11、 Heat-Resistant Steels and Alloys, Sheet, Strip, Plate, and Aircraft Tubing AS4194 Sheet and Strip Surface Finish Nomenclature 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM A 480/
12、A 480M Flat-Rolled Stainless and Heat-Resistant Steel Plate, Sheet, and Strip ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 18 Rockwell Hardness of Metallic Materials ASTM E 112 Determining Average Grain Size ASTM E 139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metall
13、ic Materials ASTM E 290 Bend Test of Materials for Ductility ASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys ASTM E 384 Knoop and Vickers Hardness of Materials 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the per
14、centages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 - Composition Element min max Carbon 0.05 0.15 Manganese 0.30 1.00 Silicon 0.25 0.75 Phosphorus - 0.03 Su
15、lfur - 0.015 Chromium 20.00 24.00 Molybdenum 1.00 3.00 Tungsten 13.00 15.00 Aluminum 0.20 0.50 Lanthanum 0.005 0.05 Cobalt - 5.00 Titanium - 0.10 Boron - 0.015 Iron - 3.00 Copper - 0.50 Nickel remainder 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. SA
16、E INTERNATIONAL AMS5878D Page 3 of 6 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Sheet and Strip Hot or cold rolled, solution heat treated, and, unless solution heat treatment is performed in an atmosphere yielding a bright finish, descaled, having a surface appeara
17、nce comparable to the following commercial corrosion resistant steel finishes as described in ASTM A 480/A 480M and AS4194 and 3.2.1.1 or 3.2.1.2 as applicable. 3.2.1.1 Sheet No. 2D finish. 3.2.1.2 Strip No. 1 strip finish. 3.2.2 Plate Hot rolled, solution heat treated, and descaled. 3.3 Heat Treatm
18、ent Pyrometry shall be in accordance with AMS2750. Except as specified in 3.3.1 the product shall be solution heat treated by heating to a temperature within the range 2150 to 2275 F (1177 to 1246 C), holding at the selected temperature within 25 F (14 C) for a time commensurate with section thickne
19、ss, and cooling rapidly. 3.3.1 Continuous Heat Treating Process parameters (e.g., furnace temperature set points, heat input, travel rate, etc.) for continuous heat treating lines shall be established by the material producer and validated by testing of product to the other requirements of this spec
20、ification. 3.4 Properties Product 0.015 to 1.5 inch (0.38 to 38 mm) in nominal thickness shall conform to the following requirements: 3.4.1 Mechanical property requirements for product outside of the range covered by 1.1 shall be agreed upon between purchaser and producer. 3.4.2 Tensile Properties S
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