SAE AMS 5511H-2003 Steel Corrosion-Resistant Sheet Strip and Plate 19Cr - 9 5Ni (304L) Solution Heat Treated (UNS S30403)《UNS S30403经溶液热处理的19Cr-9 5Ni(304 L)耐蚀钢制片材 带材和板材》.pdf

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/AMS5511H AEROSPACE MATERIAL SPECIFICATION AMS5511 REV. H Issued 1949-11 Revised 2

5、003-01 Reaffirmed 2013-08 Superseding AMS5511G Steel, Corrosion-Resistant, Sheet, Strip, and Plate 19Cr - 9.5Ni (304L) Solution Heat Treated (Composition similar to UNS S30403) RATIONALE This document has been reaffirmed to comply with the SAE 5-year Review policy. 1. SCOPE: 1.1 Form: This specifica

6、tion 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 requiring corrosion resistance up to 800 F (427 C), especially where such parts may require welding or brazing during fabrication, but u

7、sage 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 docume

8、nt 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. 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org. AMS 2242 Tolerance

9、s, Corrosion and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and Plate AMS 2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron Alloys AMS 2371 Quality Assurance Sampling and Testing,

10、Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock SAE INTERNATIONAL AMS5511H Page 2 of 5 AMS 2807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys, Sheet, Strip, Plate, and Aircraft Tubing AS4194 Sheet and Strip Surface Fini

11、sh Nomenclature 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM A 480/A 480M Flat Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and Strip ASTM A 262 Detecting Susceptibility to Intergranular Attack in Austenitic Stai

12、nless Steels ASTM E 8 Tension Testing of Metallic Materials ASTM E 8M Tension Testing of Metallic Materials (Metric) 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 per

13、centages 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 - 0.030 Manganese - 2.00 Silicon - 1.00 Phosphorus - 0.040 Sulfur - 0.

14、030 Chromium 18.00 20.00 Nickel 8.00 11.00 Molybdenum - 0.75 Copper - 0.75 3.1.1 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2248. SAE INTERNATIONAL AMS5511H Page 3 of 5 3.2 Condition: The product shall be supplied in the following condition: 3.2.1 Sheet and

15、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 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, e

16、xcept No. 2B finish may be supplied if acceptable to purchaser (See 8.2.1). 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: 3.3.1 Tensile Properties: Shall be as shown in

17、 Table 2 for product over 0.005 inch (0.13 mm) in nominal thickness, determined in accordance with ASTM E 8 or ASTM E 8M. TABLE 2 - TENSILE PROPERTIES Property Value Tensile Strength, maximum 100 ksi (689 MPa) Elongation in 2 Inches (50.8 mm) or 4D, minimum 40% 3.3.2 Susceptibility to Intergranular

18、Attack: The product, 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

19、he product. 3.5 Tolerances: Shall conform to all applicable requirements of AMS 2242. 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

20、 reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that the product conforms to specified requirements. SAE INTERNATIONAL AMS5511H Page 4 of 5 4.2 Classification of Tests: 4.2.1 Acceptance Tests: Composition (3.1), tensile properties (3.3.1), and toleran

21、ces (3.5) are acceptance tests and shall be performed on each heat or lot as applicable. 4.2.2 Periodic Tests: Susceptibility to intergranular attack (3.3.2) is a periodic test and shall be performed at a frequency selected by the vendor unless frequency of testing is specified by purchaser. 4.3 Sam

22、pling and Testing: Shall be in accordance with AMS 2371. 4.4 Reports: The vendor of the product shall furnish with each shipment a report showing the results of tests for composition of each heat and for tensile properties of each lot, and stating that the product conforms to the other technical req

23、uirements. This report shall include the purchase order number, heat and lot numbers, AMS 5511H, 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 s

24、hall 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

25、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. SAE INTERNATIONAL AMS5511H Page 5 of 5 8. NOTES: 8.1 A change bar (|

26、) 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 a specification. An (R) symbol to the left of the document title indicates a complete revision of the specification, including t

27、echnical revision. Change bars and (R) are not used in original publications, nor in specifications that contain editorial changes only. 8.2 Terms used in AMS are clarified in ARP1917. 8.3 Dimensions and properties in inch/pound units are primary; dimensions and properties in SI units are shown as the approximate equivalents of the primary units and are presented only for information. 8.4 Procurement documents should specify not less than the following: AMS 5511H Form and size of product desired Quantity of product desired. PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “F”