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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2012 SAE International All rights reserved. No part of this publication m
3、ay 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: +1 724-776-4970 (outside U
4、SA) 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/AMS5507G AEROSPACE MATERIAL SPECIFICATION AMS5507 REV. G Issued 1963-01 Revised 2012-06 Super
5、seding AMS5507F Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 17Cr - 13Ni - 2.5Mo (316L) Solution Heat Treated (Composition similar to UNS S31603) RATIONALE AMS5507G revises Tensile Properties (Table 2) to add minimum properties for tensile strength and yield strength, adds provisions
6、 for intergranular corrosion testing (3.4), and is a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate. 1.2 Application These products have been used typically for parts requiring
7、 both corrosion and heat resistance up to 1600 F (871 C) and for welding, but usage is not limited to such applications. At elevated temperatures, the strength of this steel is slightly higher than, and the oxidation resistance is similar to, that of 18-8 type steels. 2. APPLICABLE DOCUMENTS The iss
8、ue 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. When the referenced document has been cancelled and
9、 no superseding 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 724-776-4970 (outside USA), www.sae.org. AMS2242
10、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 and Other Highly-Alloyed Steels, and Iron Alloys SAE AMS5507G Page 2 of 5 AMS2371 Quality
11、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, Plate, and Aircraft Tubing AS4194 Sheet and Strip Surface Finish Nomen
12、clature 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 240 Chromium and Chromium-Nickel Stainless Steel Plate, Sheet, and Strip for Pressure Vessels and for General Applications
13、ASTM A 262 Detecting Susceptibility to Intergranular Attack in Austenitic Stainless Steels ASTM A 480/A 480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and Strip ASTM E 8/E 8M Tension Testing of Metallic Materials ASTM E 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging,
14、 and Other Similar Chronium-Nickel-Iron Alloys 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 E 353, by spectrochemical methods, or by other analytical methods acceptable to purchaser.
15、TABLE 1 - COMPOSITION Element min max Carbon - 0.030 Manganese - 2.00 Silicon - 1.00 Phosphorus - 0.040 Sulfur - 0.030 Chromium 16.00 18.00 Nickel 10.00 14.00 Molybdenum 2.00 3.00 Copper - 0.75 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2248. 3.2 Conditi
16、on The product shall be supplied in the following condition: SAE AMS5507G Page 3 of 5 3.2.1 Sheet and Strip Cold rolled, solution heat treated, and, unless solution heat treatment is performed in an atmosphere yielding a bright finish, descaled having a surface appearance in accordance with ASTM A 4
17、80/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 or cold rolled, solution heat treated, and descaled. 3.3 Properties The product shall conform to the following requirements; tensile testing shall be pe
18、rformed in accordance with ASTM E 8/E 8M. 3.3.1 Tensile Properties Shall be as shown in Table 2 for product over 0.005 inch (0.13 mm) in nominal thickness. TABLE 2 - TENSILE PROPERTIES Property Value Tensile Strength Minimum Yield Strength at 0.2% Offset 70 - 100 ksi (482 - 689 MPa) 25 ksi (172.4 MP
19、a) Elongation in 2 inches (50.8 mm) or 4D, minimum Nominal Thickness Up to 0.025 inch (0.64 mm), excel 40% 0.025 inch (0.64 mm) and over 45% NOTE: Minimum tensile strength and yield strength values have been taken directly from ASTM A 240 (See 8.4). 3.4 Susceptibility to Integranular Attack Specimen
20、s from the product shall pass, after sensitization, the intergranular corrosion test performed in accordance with ASTM A 262, Practice E. 3.5 Quality The product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfection detrime
21、ntal; to usage of the product. SAE AMS5507G Page 4 of 5 3.6 Tolerances 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 perf
22、ormance of all required tests. Purchaser reserves the 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 All technical requirements are acceptance tests and shall be performed on each hea
23、t or lot as applicable. 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 following results of tests and relevant information: 4.4.1 For each heat: Composition 4.4.2 For each lot: Tensile properti
24、es. 4.4.3 The report shall include statement that the product conforms to the other technical requirements. 4.4.4 Purchase order number Heat and lot numbers AMS5507G Size Quantity. 4.5 Resampling and Retesting Shall be in accordance with AMS2371. 5. PREPARATION FOR DELIVERY 5.1 Identification Shall
25、be in accordance with AMS2807. 5.2 Packaging The product 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 delive
26、ry. SAE AMS5507G Page 5 of 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 subject t
27、o 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 document. An (R) symbol to the left of the document title indicates a complete rev
28、ision 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 Terms used in AMS are clarified in ARP1917. 8.3 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are
29、 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. 8.4 Minimum tensile strength and yield strength properties shown in Table 2 have been taken directly from ASTM A 240, and have not been statistically substantiated in accordance with Aerospace Materials Division policy. 8.5 Purchase documents should specify not less than the following: AMS5507G Form and size of product desired Quantity of product desired. PREPARED BY AMS COMMITTEE “F”
