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 2013 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:/www.sae.org/technical/standards/AMS5592F RATIONALE AMS5592F revises Reports (4.4.5), and is a Five Year Review an
5、d update of this specification. 1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant iron-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), but us
6、age 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 herein. The supplier may work to a subsequent revision of a document unless a specific document
7、 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. AEROSPACE MATERIAL SPECIFICATION AMS5592 REV. F Issued 1963-07 Reaffirmed 2006-10 Revised 2013-08 Superseding AMS5592E Iron-Nick
8、el Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 44Fe - 18.5Cr - 35Ni - 1.15Si Solution Heat Treated (Composition similar to UNS N08330) SAE INTERNATIONAL AMS5592F Page 2 of 5 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel
9、: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2242 Tolerances, Corrosion and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and Plate AMS2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging
10、 and Other Highly-Alloyed Steels, and Iron Alloys AMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock AMS2807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys, Sheet, Strip, Plat
11、e, 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/A 480M Flat-Rolled, Stainless and Heat-Resisting Stee
12、l Plate, Sheet and Strip ASTM E 3 Preparation of Metallographic Specimens ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 18 Rockwell Hardness of Metallic Materials ASTM E 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron Alloys 3. TECHNI
13、CAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 353, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 COMPOSITION Element min max Carbon - 0.08 Mangan
14、ese - 2.00 Silicon 0.75 1.50 Phosphorus - 0.030 Sulfur - 0.030 Chromium 17.00 20.00 Nickel 34.00 37.00 Copper - 0.75 Tin - 0.025 Lead - 0.005 Iron remainder SAE INTERNATIONAL AMS5592F Page 3 of 5 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2248. 3.2 Condi
15、tion 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 appearance comparable to the following commercial corr
16、osion resistant steel finishes as described in ASTM A 480/A 480M and AS4194, and the following: 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 Te
17、nsile Properties Shall be as shown in Table 2, determined in accordance with ASTM E 8/E 8M. TABLE 2 - MINIMUM TENSILE PROPERTIES Property Value Tensile Strength 70 ksi (483 MPa) Yield Strength at 0.2% Offset 30.0 ksi (207 MPa) Elongation in 2 Inches (50.8mm) or 4D 30% 3.3.1.1 Elongation requirement
18、does not apply to sheet or strip under 0.020 inch (0.51 mm) in nominal thickness. 3.3.2 Hardness Shall be not higher than 95 HRB, or equivalent (See 8.2), determined in accordance with ASTM E 18. 3.3.3 Microstructure Shall be free from continuous carbide network, determined by metallographic examina
19、tion of specimens prepared in accordance 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. SAE INTERNATIONAL AMS5592F Page 4 of 5 3.5 Toleranc
20、es Shall conform to all applicable requirements of AMS2242. 4. QUALITY 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 samp
21、le and to perform any confirmatory testing deemed necessary to ensure 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 accord
22、ance with AMS2371. 4.4 Reports The vendor of the product shall furnish with each shipment a report showing the following results of tests and relevant information: 4.4.1 For each heat Composition. 4.4.2 For each lot Tensile properties Hardness Microstructure. 4.4.3 A statement that the product confo
23、rms to the other technical requirements. 4.4.4 Purchase order number Heat and lot numbers AMS5592F Size Quantity. 4.4.5 The vendor shall provide a copy of the original material manufacturers (producers) report (material certification), including: producer name and country where the metal was melted
24、(e.g., the final melt in the case of metal processed by multiple melting operations. 4.5 Resampling and Retesting Shall be in accordance with AMS2371. 5. PREPARATION FOR DELIVERY 5.1 Identification Shall be in accordance with AMS2807. SAE INTERNATIONAL AMS5592F Page 5 of 5 5.2 Packaging The product
25、shall be prepared for shipment in accordance with commercial practice and in compliance with applicable rules and regulations pertaining to the handling, packaging, and transportation of the product to ensure carrier acceptance and safe delivery. 6. ACKNOWLEDGMENT A vendor shall mention this specifi
26、cation 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 subject to rejection. 8. NOTES 8.1 A change bar (|) located in the left margin is for the c
27、onvenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of this document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revisions. Change bars and (R) are not
28、used in original publications, nor in documents 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 ARP1917. 8.4 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; d
29、imensions 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 specify not less than the following: AMS5592F Product form and size of product desired Quantity of product desired. PREPARED BY AMS COMMITTEE “F“
