SAE AMS 5869C-2008 Nickel Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 62Ni - 21 5Cr - 9 0Mo - 3 7Cb Solution Heat Treated (UNS N06625)《溶解热处理的62Ni 21 5Cr 9 0Mo 3 7Cb耐腐蚀.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/AMS5869C AEROSPACE MATERIAL SPECIFICATION AMS5869 REV. C Issued 1990-10 Revised 2

5、008-02 Reaffirmed 2013-12 Superseding AMS5869B Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 62Ni - 21.5Cr - 9.0Mo - 3.7Cb Solution Heat Treated (Composition similar to UNS N06625) RATIONALE AMS5869C has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE 1

6、.1 Form This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate. 1.2 Application These products have been used typically for parts requiring resistance to corrosion, oxidation, creep, and rupture up to 2000 F (1093 C), but usage is not limited to

7、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 document issue is specified. W

8、hen 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 International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or

9、 724-776-4970 (outside USA), www.sae.org. AMS 2262 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip, and Plate AMS 2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys AMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and All

10、oys, Wrought Products and Forging Stock 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 Finish Nomenclature SAE INTERNATIONAL AMS5869C Page 2 of 6 2.2 ASTM Publications Avail

11、able 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 480/A 480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and Strip ASTM E 8 Tension Testing of Metallic Materials ASTM E 8M Tension Testing of

12、Metallic Materials (Metric) ASTM E 112 Determining Average Grain Size ASTM E 139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials ASTM E 290 Bend Test for Ductility of Metallic Materials ASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other

13、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 E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1

14、 - COMPOSITION Element min max Carbon - 0.10 Manganese - 0.50 Silicon - 0.50 Phosphorus - 0.015Sulfur - 0.015Chromium 20.00 23.00 Molybdenum 8.00 10.00 Columbium 3.15 4.15 Cobalt - 1.00 Titanium - 0.40 Aluminum - 0.40 Iron - 5.00 Nickel remainder 3.1.1 Check Analysis Composition variations shall mee

15、t the applicable requirements of AMS 2269. 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Sheet and Strip Hot or cold rolled, solution heat treated, and, unless solution heat treatment is performed in an atmosphere yielding a bright finish, descaled, having a surface a

16、ppearance 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. SAE INTERNATIONAL AMS5869C Page 3 of 6 3.2.1.2 Strip No. 1 strip finish. 3.2.2 Plate Hot rolled, solution heat treated, and descaled. 3.3 Heat Treatment The product

17、shall be solution heat treated by heating to a temperature not lower than 2000 F (1093 C), holding at the selected temperature within 25 F (14 C) for a time commensurate with section thickness, and cooling at a rate equivalent to an air cool or faster (See 8.2). 3.3.1 Product may be given a subseque

18、nt stabilization treatment at a temperature not lower than 1800 F (982 C) to increase resistance to sensitization. 3.4 Properties 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 (25.40 mm) in nominal thicknes

19、s, determined in accordance with ASTM E 8 or ASTM E 8M. TABLE 2 - MINIMUM TENSILE PROPERTIES Property Value Tensile Strength 100 ksi (689 MPa) Yield Strength at 0.2% Offset 40.0 ksi (276 MPa) Elongation in 2 Inches (50.8 mm) or 4D 30% 3.4.1.1 Yield strength requirement does not apply to product unde

20、r 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. 3.4.2 Bending Product 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 b

21、ending parallel to the direction of rolling and shall withstand without 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. In case of dispute, the results of tests using the

22、 guided bend test of ASTM E 290 shall govern. TABLE 3 - BENDING PARAMETERS Nominal Thickness Inch Nominal Thickness Millimeters Bend Factor 0.010 to 0.050, incl Up to 1.27, incl 1 Over 0.050 to 0.1874, incl Over 1.27 to 4.760, incl 2 3.4.2.1 ASTM E 290 is not applicable to product thicknesses under

23、0.010 inch (0.25 mm). SAE INTERNATIONAL AMS5869C Page 4 of 6 3.4.3 Average Grain Size Shall be as follows, determined in accordance with ASTM E 112: 3.4.3.1 Sheet and Strip Shall be not finer than shown in Table 4. TABLE 4 - AVERAGE GRAIN SIZE Nominal Thickness Inch Nominal Thickness Millimeters AST

24、M No. Up to 0.050, incl Up to 1.27, incl 7 Over 0.050 to 0.1874, incl Over 1.27 to 4.760, incl 6 3.4.3.2 Plate Shall be not finer than ASTM No. 6. 3.4.3.3 Sheet, Strip, and Plate Shall be not coarser than ASTM No. 2. 3.4.4 Stress-Rupture Properties at 1500 F (816 C) A tensile specimen, maintained at

25、 1500 F 3 (816 C 2) while a load sufficient to produce an initial axial stress of 19.0 ksi (131 MPa) or higher is applied continuously, shall not rupture in less than 23 hours. The test shall be continued to rupture without change of load. Time to rupture and elongation after rupture shall be report

26、ed. Test shall be conducted in accordance with ASTM E 139. 3.4.4.1 The test of 3.4.4 may be conducted using incremental loading. In such case, the load required to produce an initial axial stress of 19.0 ksi (131 MPa) or higher shall be used to rupture or for 23 hours, whichever occurs first. After

27、the 23 hours and at intervals of 8 hours minimum, thereafter, the stress shall be increased in increments of 2.0 ksi (13.8 MPa). Time to rupture requirement shall be as specified in 3.4.4. 3.5 Quality The product, as received by purchaser, shall be uniform in quality and condition, sound, and free f

28、rom foreign materials and from imperfections detrimental to usage of the product. 3.6 Tolerances Shall conform to all applicable requirements of AMS 2262. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for inspection The vendor of the product shall supply all samples for vendors tests and shall

29、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. SAE INTERNATIONAL AMS5869C Page 5 of 6 4.2 Classification of Tests 4.2.1 Acceptance

30、 Tests Composition (3.1), tensile properties (3.4.1), bending (3.4.2), average grain size (3.4.3), and tolerances (3.6) are acceptance tests and shall be performed on each heat or lot as applicable. 4.2.2 Periodic Tests Stress-rupture properties (3.4.4) is a periodic test and shall be performed at a

31、 frequency selected by the vendor unless frequency of testing is specified by purchaser. 4.3 Sampling 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 following results of tests and relevant information: 4.4

32、.1 For each heat Composition. 4.4.2 For each lot Tensile properties Bending, when applicable depending upon thickness Average grain size. 4.4.3 A statement that the product conforms to the other technical requirements. 4.4.4 Purchase order number Heat and lot numbers AMS 5869C Size Quantity. 5. PREP

33、ARATION FOR DELIVERY 5.1 Identification Shall be in accordance with AMS 2807. 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 produ

34、ct 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. SAE INTERNATIONAL AMS5869C Page 6 of 6 7. REJECTIONS Product not conforming to this specification, o

35、r 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 user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of a specification. An (R) sy

36、mbol to the left of the document title indicates a complete revision of the specification, including technical revision. Change bars and (R) are not used in original publications, nor in specifications that contain editorial changes only. 8.2 The 2000 F (1093 C) solution heat treatment temperature o

37、ptimizes properties for use above 1100 F (593 C). 8.3 Terms used in AMS are clarified in ARP1917. 8.4 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. 8.5 Purchase documents should specify not less than the following: AMS 5869C Form and size of product desired Quantity of product desired. PREPARED BY AMS COMMITTEE “F“