1、AEROSPACE MATERIAL SPECIFICATIONAMS 5593FIssuedRevisedSuperseding AMS 5593ENickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate45.5Ni - 25.5Cr - 3.2Co - 3.2Mo - 3.2W - 18.5FeSolution Heat Treated(Composition similar to UNS N06333)1. SCOPE:1.1 Form: This specification covers a corrosio
2、n and heat resistant nickel alloy in the form of sheet, strip, and plate.1.2 Application: These products have been used typically for parts requiring heat and oxidation resistance up to 2150 F (1177 C), particularly where such parts may require welding during fabrication, but usage is not limited to
3、 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 specific document issue is specified.
4、 When the referenced document has been canceled and no superseding document has been specified, the last published issue of that document shall apply.2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.AMS 2242 Tolerances, Corrosion and Heat Resistant Steel, I
5、ron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and PlateMAM 2242 Tolerances, Metric, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and PlateAMS 2248 Chemical Check Analysis Limits, Corrosion and Heat Resistant Steels and Alloys, Maraging and Other
6、Highly-Alloyed Steels, and Iron AlloysReaffirmed 1963-072001-102010-05SAE 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
7、 any particular use, including any 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 2010
8、SAE International All rights reserved. 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:
9、877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (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:/www.sae.org/technical/standards/AMS5593F Copyright SAE In
10、ternational Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 5593F SAE AMS 5593F- 2 -2.1 (Continued):AMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat Resistant Steels and Alloys, Wrought Products and Forgi
11、ng StockAMS 2807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat Resistant Steels and Alloys, Sheet, Strip, Plate, and Aircraft TubingAS4194 Sheet and Strip Surface Finish Nomenclature2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.
12、ASTM A 480/A 480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and StripASTM E 3 Preparation of Metallographic SpecimensASTM E 8 Tension Testing of Metallic MaterialsASTM E 8M Tension Testing of Metallic Materials (Metric)ASTM E 18 Rockwell Hardness and Rockwell Superficial Hardness
13、of Metallic MaterialsASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys3. TECHNICAL REQUIREMENTS: 3.1 Composition:Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with
14、ASTM E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser:TABLE 1 - CompositionElement min maxCarbonManganeseSiliconPhosphorousSulfurChromiumNickelCobaltMolybdenumTungstenCopperTinLeadIron-0.75-24.0044.002.502.502.50-remainder0.082.001.500.0300.03027.0047.004.004
15、.004.000.500.0250.025Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 5593F SAE AMS 5593F- 3 -3.1.1 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2248.3.2 Co
16、ndition:The product shall be supplied in the following condition:3.2.1 Sheet and Strip: Hot or cold rolled, solution heat treated to meet the requirements of 3.3, and,unless solution heat treatment is performed in an atmosphere yielding a bright finish, descaled having a surface appearance in accord
17、ance with ASTM A 480/A 480M and AS4194 comparable to 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 Properties:The product shall conform to the following requirements:3.3.1 Tensile Prope
18、rties: Shall be as shown in Table 2, determined in accordance with ASTM E 8 or ASTM E 8M.3.3.2 Hardness: Shall be not higher than 95 HRB, or equivalent (See 8.2), determined in accordance with ASTM E 18. Product shall not be rejected on the basis of hardness if the tensile properties of 3.3.1 are ac
19、ceptable, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similar nonconforming hardness.3.3.3 Microstructure: Shall be free from continuous carbide network, determined by metallographic examination of specimens prepared in accordanc
20、e with ASTM E 3.3.4 Quality:The product, 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 product.TABLE 2 - Tensile PropertiesProperty ValueTensile Strength, maxElongation in 2 Inches (50.8
21、mm) or 4D, min120 ksi (827 MPa)30%Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 5593F SAE AMS 5593F- 4 -3.5 Tolerances:Shall conform to all applicable requirements of AMS 2242 or MAM 2242.4. QU
22、ALITY ASSURANCE PROVISIONS: 4.1 Responsibility for Inspection: The vendor of the product shall supply all samples for vendors tests and shall be responsible for the performance of all required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to e
23、nsure that the product conforms to specified requirements.4.2 Classification of Tests: All technical requirements are acceptance tests and shall be performed on each heat or lot as applicable.4.3 Sampling and Testing: Shall be in accordance with AMS 2371.4.4 Reports:The vendor of the product shall f
24、urnish with each shipment a report showing the results of tests for chemical composition of each heat and for tensile properties and hardness of each lot, and stating that the product conforms to the other technical requirements. This report shall include the purchase order number, heat and lot numb
25、ers, AMS 5593F, size, and quantity.4.5 Resampling and Retesting: Shall be in accordance with AMS 2371.5. PREPARATION FOR DELIVERY: 5.1 Identification:Shall be in accordance with AMS 2807.5.2 Packaging:The product shall be prepared for shipment in accordance with commercial practice and in compliance
26、 with applicable rules and regulations pertaining to the handling, packaging, and transportation of the product to ensure carrier acceptance and safe delivery.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from
27、IHS-,-,-AMS 5593F SAE AMS 5593F- 5 -6. ACKNOWLEDGMENT:A vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders.7. REJECTIONS:Product not conforming to this specification, or to modifications authorized by purchaser, will be sub
28、ject to rejection.8. NOTES:8.1 A change bar ( l ) located in the left margin is for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of this specification.An (R) symbol to the left of the document title indicates a c
29、omplete revision of the specification, including technical revisions. Change bars and (R) are not used in original publications, nor in specifications that contain editorial changes only.8.2 Hardness conversion tables for metals are presented in ASTM E 140.8.3 Terms used in AMS are clarified in ARP1
30、917.8.4 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions and properties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.8.5 Purchase documents should spe
31、cify not less than the following:AMS 5593FForm and size of product desiredQuantity of product desired.PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “F“Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
