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 2015 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/AMS5513J AEROSPACE MATERIAL SPECIFICATION AMS5513 REV. J Issued 1953-06 Revised 2
5、009-09 Reaffirmed 2015-05 Superseding AMS5513H Steel, Corrosion-Resistant, Sheet, Strip, and Plate 19Cr 9.2Ni (SAE 30304) Solution Heat Treated (Composition similar to UNS S30400) RATIONALE AMS5513J was revised to require bend testing in accordance with ASTM E290 and added product form to the report
6、ing requirements, and has been subsequently reaffirmed to comply with the SAE five-year review policy. 1. SCOPE 1.1 Form This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate. 1.2 Application These products have been used typically for formed and drawn parts re
7、quiring corrosion resistance up to 800 F (427 C), but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 F (427 C) during fabrication may impair corrosion resistance. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the da
8、te of the purchase order forms a part of this specification to the extent supplied 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 l
9、ast 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. AMS2242 Tolerances, Corrosion and Heat-Resistant Steel, Ir
10、on Alloy, Titanium, and Titanium Alloy Sheet, Strip, and Plate AMS2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron Alloys AMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and All
11、oys, Wrought Products and Forging Stock (Continued) AMS2807 Identification, Carbon and Low-Alloy Steels, Corrosion and 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
12、 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959 , Tel: 610-832-9585, www.astm.org. ASTM A 262 Detecting Susceptibility to Intergranular Attack in Austenitic Stainless Steels ASTM A 370 Mechanical Testing of Steel Products ASTM A 480/A 480M Flat Rolled Stainless and Heat-Resi
13、sting Steel Plate, Sheet, and Strip ASTM E 290 Bend Testing of Material for Ductility ASTM E 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table
14、 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 Manganese - 2.00 Silicon - 1.00 Phosphorus - 0.040 Sulfur - 0.030 Chromium 18.00 20.00 Nickel
15、8.00 10.50 Molybdenum - 0.75 Copper - 0.75 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2248. 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Sheet and Strip Cold rolled, solution heat treated, and, unless solution heat treatm
16、ent is performed in an atmosphere yielding a bright finish, descaled having a surface appearance in accordance with ASTM A 480/A 480M and AS4194 and conforming to 3.2.1.1 or 3.2.1.2 as applicable. 3.2.1.1 Sheet No. 2D finish, except No. 2B finish may be supplied if acceptable to purchaser (See 8.3.1
17、). 3.2.1.2 Strip No. 1 strip finish. SAE INTERNATIONAL AMS5513J Page 2 of 5_ 3.2.2 Plate Hot rolled, solution heat treated, and descaled. 3.3 Properties The product shall conform to the following requirements; tensile and hardness testing shall be performed in accordance with ASTM A 370: 3.3.1 Tensi
18、le Properties Shall be as shown in Table 2 for product over 0.005 inch (0.13 mm) in nominal thickness. TABLE 2 - MINIMUM TENSILE PROPERTIES Property Value Tensile Strength 75 ksi (517 MPa) Yield Strength at 0.2% Offset 30.0 ksi (207 MPa) Elongation in 2 Inches (50.8 mm) or 4D 40% 3.3.2 Hardness Shal
19、l be not higher than 92 HRB, 202 HB, or equivalent (See 8.2). 3.3.3 Bending Product 0.749 inch (19.02 mm) and under in nominal thickness shall be tested in accordance with ASTM E 290 using a sample prepared nominally 0.75 inch (19.0 mm) in width with its axis of bending parallel to the direction of
20、rolling and shall withstand, without cracking, when bending at room temperature through the angle indicated in Table 3 around a diameter equal to the bend factor times the nominal thickness of the product. In case of dispute, the results of tests using the guided bend test of ASTM E 290 shall govern
21、 TABLE 3 - BENDING PARAMETERS Nominal Thickness Inch Nominal Thickness Millimeters Angle deg, min Bend Factor Up to 0.249,incl Up to 6.32,incl 180 1 Over 0.249 to 0.749,incl Over 6.32 to 19.02,incl 90 1 3.3.4 Susceptibility to Intergranular Attack The product, as supplied, shall pass the intergranu
22、lar corrosion test performed in accordance with ASTM A 262, Practice E. 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. 3.5 Tolerances Shall conform to all
23、 applicable requirements of AMS2242. SAE INTERNATIONAL AMS5513J Page 3 of 5_ 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 t
24、he right to sample and to perform any confirmatory testing deemed necessary to ensure that the product conforms to specified requirements. 4.2 Classification of Tests 4.2.1 Acceptance Tests Composition (3.1), tensile properties (3.3.1), hardness (3.3.2), bending of product 0.1874 inch (4.762 mm) and
25、 under in nominal thickness (3.3.3), and tolerances (3.5) are acceptance tests and shall be performed on each heat or lot as applicable. 4.2.2 Periodic Tests Bending of product over 0.1874 inch (4.762 mm) in nominal thickness (3.3.3) and susceptibility to intergranular attack (3.3.4) are periodic te
26、sts and shall be performed at a frequency selected by the vendor unless frequency of testing is specified by purchaser. 4.3 Sampling and Testing Shall be in accordance with AMS2371. 4.4 Reports The vendor of the product shall furnish with each shipment a report showing the results of tests for compo
27、sition of each heat and for tensile, hardness, and bending properties 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 numbers, AMS5513J, product form, size, and quantity. 4.5 Resampling and Rete
28、sting Shall be in accordance with AMS2371. 5. PREPARATION FOR DELIVERY 5.1 Identification Shall be in accordance with AMS2807. 5.2 Packaging The product shall be prepared for shipment in accordance with commercial practice and in accordance with applicable rules and regulations pertaining to the han
29、dling, packaging, and transportation of the product to ensure carrier acceptance and safe delivery. 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 specif
30、ication, or to modifications authorized by purchaser, will be subject to rejection. SAE INTERNATIONAL AMS5513J Page 4 of 5_ 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 t
31、o 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 used in original publications, nor in documents that contain editorial changes only. 8.2 Hardness conversio
32、n tables for metals are presented in ASTM E 140. 8.3 Terms used in AMS are clarified in ARP1917 and as follows: 8.3.1 Acceptable to Purchaser Does not require prior written approval from purchaser, but allows vendor to make a decision and purchaser the right to disapprove the decision. 8.4 Dimension
33、s 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 specify not less than the following: AMS5513J Product form and size of product desired Quantity of product desired. PREPARED BY AMS COMMITTEE “F” SAE INTERNATIONAL AMS5513J Page 5 of 5_
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