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 2016 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:/standards.sae.org/AMS5599H AEROSPACE MATERIAL SPECIFICATION AMS5599 REV. H Issued 1967-11 Reaffirmed 2015-05 Revi
5、sed 2016-10Superseding AMS5599G Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 62Ni - 21.5Cr - 9.0Mo - 3.7 Cb (Nb) Annealed (Composition similar to UNS N06625) RATIONALE AMS5599H revises the Title, Condition (3.2), Heat Treatment (3.3), Properties (3.4.1.3), and Reports (4.4), a
6、nd introduces a new requirement for compliance with AS6279 (3.7). 1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate up to 1.000 inch (25.4 mm) in nominal thickness. 1.2 Application These products have been used typically fo
7、r parts requiring corrosion and oxidation resistance up to 2000 F (1095 C), particularly where such parts may require welding during fabrication, 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 fo
8、rms 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 no superseding document has been specified, the last published issue of tha
9、t 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 +1 724-776-4970 (outside USA), www.sae.org. AMS2262 Tolerances Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip, and Plate
10、 AMS2269 Chemical Check Analysis Limits Nickel, Nickel Alloys, and Cobalt Alloys AMS2371 Quality Assurance Sampling and Testing Corrosion and Heat-Resistant Steels and Alloys Wrought Products and Forging Stock SAE INTERNATIONAL AMS5599H Page 2 of 6 AMS2807 Identification Carbon and Low-Alloy Steels,
11、 Corrosion and Heat-Resistant Steels and Alloys Sheet, Strip, Plate, and Aircraft Tubing ARP1917 Clarification of Terms Used in Aerospace Metals Specifications AS4194 Sheet and Strip Surface Finish Nomenclature 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box
12、C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM A480/A480M Flat-Rolled Stainless and Heat-Resistant Steel Plate, Sheet and Strip ASTM E8/E8M Tension Testing of Metallic Materials ASTM E112 Determining Average Grain Size ASTM E290 Bend Test for Ductility of Metallic Mate
13、rials ASTM E354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt 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 E354, by sp
14、ectrochemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element min max Carbon - 0.10 Manganese - 0.50 Silicon - 0.50 Phosphorus - 0.015 Sulfur - 0.015 Chromium 20.00 23.00 Molybdenum 8.00 10.00 Columbium (Niobium) 3.15 4.15 Iron - 5.00 Cobalt (3.1.1) - 1
15、.00 Titanium - 0.40 Aluminum - 0.40 Nickel remainder SAE INTERNATIONAL AMS5599H Page 3 of 6 3.1.1 Determination not required for routine acceptance. 3.1.2 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. 3.2 Condition The product shall be supplied in the follo
16、wing condition: 3.2.1 Sheet and Strip Hot or cold rolled, annealed, and, unless annealing is performed in an atmosphere yielding a bright finish, descaled having a surface appearance in accordance with ASTM A480/A480M and AS4194 comparable to 3.2.1.1 and 3.2.1.2, as applicable, except that product 0
17、.010 inch (0.25 mm) and under in nominal thickness shall have a surface appearance comparable to a No. 2B finish. 3.2.1.1 Sheet No. 2D finish. 3.2.1.2 Strip No. 1 strip finish. 3.2.2 Plate Hot rolled, annealed, and, unless annealing is performed in an atmosphere yielding a bright finish, descaled. 3
18、.3 Heat Treatment The product shall be annealed by heating to a temperature not lower than 1600 F (870 C), holding at the selected temperature within 25 F (15 C) for a time commensurate with section thickness, and cooling at a rate equivalent to an air cool or faster, except as specified in 3.3.1. 3
19、.3.1 Continuous Heat Treating Process parameters (e.g., furnace temperature set points, heat input, travel rate, etc.) for continuous heat treating lines shall be established by the material producer and validated by testing of product to the other requirements of this specification. 3.4 Properties
20、The product shall conform to the following requirements: 3.4.1 Tensile Properties Shall be as shown in Table 2 for product up to 1.000 inch (25.4 mm) in nominal thickness, determined in accordance with ASTM E8/E8M. Table 2A - Minimum tensile properties, inch/pound units Property Value Tensile Streng
21、th 120.0 ksi Yield Strength at 0.2% Offset 60.0 ksi Elongation in 2 Inches or 4D 30% SAE INTERNATIONAL AMS5599H Page 4 of 6 Table 2B - Minimum tensile properties, SI units Property Value Tensile Strength 827 MPa Yield Strength at 0.2% Offset 414 MPa Elongation in 50 mm or 4D 30% 3.4.1.1 Yield streng
22、th requirement does not apply to product under 0.020 inch (0.51 mm) in nominal thickness. 3.4.1.2 Elongation requirement does not apply to product under 0.010 inch (0.25 mm) in nominal thickness. 3.4.1.3 Mechanical properties for product outside the range listed in 1.1 shall be shall be agreed upon
23、between purchaser and producer. 3.4.2 Bending Product 0.1874 inch (4.76 mm) and under in nominal thickness shall, be tested in accordance with ASTM E290 using a sample prepared nominally 0.75 inch (19.0 mm) in width with its axis of bending parallel to the direction of rolling and shall withstand wi
24、thout cracking when bending at room temperature through an angle of 180 degrees around a diameter equal to the bend factor shown in Table 3 times the nominal thickness of the product with axis of bend parallel to the direction of rolling. In case of dispute, the results of tests using the guided ben
25、d test of ASTM E290 shall govern. Table 3 - Bending parameters Nominal Thickness Inch Nominal Thickness Millimeters Bend Factor Up to 0.050, incl Over 0.050 to 0.1874, incl Up to 1.25, incl Over 1.25 to 4.75, incl 1 2 3.4.3 Average Grain Size Shall be as follows, determined in accordance with ASTM E
26、112: 3.4.3.1 Sheet and Strip Shall be as shown in Table 4 or finer. Table 4 - Maximum average grain size Nominal Thickness Inch Nominal Thickness Millimeters ASTM Grain Size No. Up to 0.050, incl Over 0.050 to 0.1874, incl Up to 1.25, incl Over 1.25 to 4.75, incl 5 4 3.4.3.2 Plate Shall be ASTM No.
27、3 or finer. 3.5 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. 3.6 Tolerances Shall conform to all applicable requirements of AMS2262. SAE INTERNATIONAL AMS55
28、99H Page 5 of 6 3.7 Production, distribution, and procurement of metal stock shall comply with AS6279. The requirement for compliance with AS6279 becomes effective April 1, 2018. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The producer of the product shall supply all samples fo
29、r producers tests and shall be responsible for the performance 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
30、are acceptance tests and shall be performed on each heat or lot as applicable. 4.3 Sampling and Testing In accordance with AMS2371. 4.4 Reports The producer of the product shall furnish with each shipment a report showing the producers name and country where the metal was melted (e.g., final melt in
31、 the case of metal processed by multiple melting operations) and the results of tests for composition (see 3.1.1) of each heat and for tensile properties, bending properties, and average grain size requirements of each lot, and stating that the product conforms to the other technical requirements. T
32、his report shall include the purchase order number, heat and lot numbers, AMS5599H, size, product form and quantity. 4.4.1 When the product size is outside the range covered by 1.1, the report shall contain a statement to that effect. 4.5 Resampling and Retesting In accordance with AMS2371. 5. PREPA
33、RATION FOR DELIVERY 5.1 Identification 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 ensur
34、e carrier acceptance and safe delivery. 6. ACKNOWLEDGMENT A producer 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
35、 be subject to rejection. SAE INTERNATIONAL AMS5599H Page 6 of 6 8. NOTES 8.1 Revision Indicator 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. A
36、n (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 Terms used in AMS are clarified in ARP1917. 8.3 Dimensions
37、 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: AMS5599H Form and size of product desired Property and acceptance requirements from the cognizant engineering organization applicable to sizes outside the range listed in 1.1 Quantity of product desired. PREPARED BY AMS COMMITTEE “F“
