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 2014 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/AMS5510S AEROSPACE MATERIAL SPECIFICATION AMS5510 REV. S Issued 1939-12 Revised 2
5、008-12 Reaffirmed 2014-06 Superseding AMS5510R Steel, Corrosion and Heat-Resistant, Sheet, Strip and Plate 18Cr - 10.5Ni - 0.40Ti (SAE 30321) Solution Heat Treated (Composition similar to UNS S32100) RATIONALE This document has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE
6、 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 both corrosion and heat resistance, especially when such parts require welding during fabrication and for parts
7、 requiring oxidation resistance up to 1500 F (816 C) but useful at that temperature only when stresses are low, but usage 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 t
8、o 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 last published issue of that document shall apply. SAE INTERNA
9、TIONAL AMS5510S Page 2 of 5 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, Iron Alloy, Titanium, and
10、 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 Alloys, Wrought Products a
11、nd 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 Nomenclature 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C
12、700, 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-Resisting Steel Plate, Sheet, and Strip A
13、STM 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 1, determined by wet chemical method
14、s 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 0.25 1.00 Phosphorus - 0.040Sulfur - 0.030Chromium 17.00 19.00 Nickel 9.00 12.00 Titanium 5x(C+N) 0.70 Mol
15、ybdenum - 0.75 Copper - 0.75 Nitrogen - 0.10 SAE INTERNATIONAL AMS5510S Page 3 of 5 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
16、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 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
17、.1.1 Sheet No. 2D finish, except No. 2B finish may be supplied if acceptable to purchaser. 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 performed
18、 in accordance with ASTM A 370: 3.3.1 Tensile Properties Shall be as shown in Table 2: TABLE 2A - TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness Inch Tensile Strength ksi Yield Strength at 0.2% Offset ksi, min Elongation in 2 inches or 4D %, min Over 0.002 to 0.003, incl 70 to 110 25.0 ksi 2
19、0 Over 0.003 to 0.004, incl 70 to 105 25.0 ksi 30 Over 0.004 70 to 100 25.0 ksi 40 TABLE 2B - TENSILE PROPERTIES, SI UNITS Nominal Thickness Millimeter Tensile Strength MPa Yield Strength at 0.2% Offset MPa, min Elongation in 50.8 mm or 4D %, min Over 0.05 to 0.08, incl 483 to 758 172 20 Over 0.08 t
20、o 0.10, incl 483 to 724 172 30 Over 0.10 483 to 689 172 40 SAE INTERNATIONAL AMS5510S Page 4 of 5 3.3.2 Bending Product 0.749 inch (19.02 mm) and under in nominal thickness shall be tested in accordance with ASTM E 290 using specimens prepared nominally 0.75 inch (19.0 mm) in width, with its axis pa
21、rallel to the direction of 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 tes
22、t of ASTM E 290 shall apply. 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 3.3.3 Susceptibility to Intergranular Attack The product, after s
23、ensitizing treatment, shall pass the intergranular 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 t
24、he product. 3.5 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 performance of all required tests. Purchaser res
25、erves 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 4.2.1 Acceptance Tests Composition (3.1), tensile properties (3.3.1), bending of product 0.1874 inch (4.762 mm) and under in n
26、ominal thickness (3.3.2), 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) to 0.749 inch (19.02 mm), inclusive, in nominal thickness (3.3.2) and susceptibility of intergranular atta
27、ck (3.3.3) are periodic tests 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. SAE INTERNATIONAL AMS5510S Page 5 of 5 4.4 Reports The vendor of the product shall furnish w
28、ith each shipment a report showing the results of tests for composition of each heat and for tensile properties and for bending tests of product 0.1874 inch (4.762 mm) and under in nominal thickness of each lot, and stating that the product conforms to the other technical requirements. This report s
29、hall include the purchase order number, heat and lot numbers, AMS5510S, product form, size, and quantity. 4.5 Resampling and Retesting 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
30、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 specification number and
31、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 convenience of the
32、user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of a document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revision. Change bars and (R) are not used in original publi
33、cations, 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 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 Purchase documents should specify not less than the following: AMS5510S Product form and size of product desired Quantity of product desired. PREPARED BY AMS COMMITTEE “F”
