SAE AMS 5536N-2012 Nickel Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 47 5Ni - 22Cr - 1 5Co - 9 0Mo - 0 60W - 18 5Fe Solution Heat Treated (UNS N06002)《47 5Ni 22Cr 1 5.pdf

《SAE AMS 5536N-2012 Nickel Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 47 5Ni - 22Cr - 1 5Co - 9 0Mo - 0 60W - 18 5Fe Solution Heat Treated (UNS N06002)《47 5Ni 22Cr 1 5.pdf》由会员分享，可在线阅读，更多相关《SAE AMS 5536N-2012 Nickel Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 47 5Ni - 22Cr - 1 5Co - 9 0Mo - 0 60W - 18 5Fe Solution Heat Treated (UNS N06002)《47 5Ni 22Cr 1 5.pdf（6页珍藏版）》请在麦多课文档分享上搜索。

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/AMS5536N AEROSPACE MATERIAL SPECIFICATION AMS5536 REV. N Issued 1954-05 Revised 2012-12 Super

5、seding AMS5536M Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe Solution Heat Treated (Composition similar to UNS N06002) RATIONALE AMS5536N revises heat treatment (3.3) and bending (3.4.2), and is a Five Year Review and update of th

6、is specification. 1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate procured in inch/pound units. 1.2 Application These products have been used typically for parts requiring oxidation resistance up to 2200 F and relatively

7、high strength up to 1500 F, 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 to the extent specified herein. The supplier may work to a subsequent revision of a d

8、ocument 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 AMS5536N Page 2 of 6 2.1 SAE Publications Available from SAE International, 400 Commonweal

9、th Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2262 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip, and Plate AMS2269 Chemical Check Analysis, Wrought Nickel Alloys and Cobalt Alloys AMS2371 Quality Assur

10、ance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock AMS2750 Pyrometry 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

11、 Finish Nomenclature 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 480/A 480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and Strip ASTM E 8/E 8M Tension Testin

12、g of Metallic Materials 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 Testing of Material for Ductility ASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iro

13、n, 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. SAE AMS5536N Page

14、3 of 6 TABLE 1 COMPOSITION Element min max Carbon 0.05 0.15 Manganese - 1.00 Silicon - 1.00 Phosphorus - 0.040 Sulfur - 0.030 Chromium 20.50 23.00 Cobalt 0.50 2.50 Molybdenum 8.00 10.00 Tungsten 0.20 1.00 Iron 17.00 20.00 Aluminum - 0.50 Titanium - 0.15 Boron - 0.010 Copper - 0.50 Nickel remainder 3

15、.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. 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 yie

16、lding a bright finish, descaled having a surface appearance comparable to the following commercial corrosion resistant steel finishes as described in ASTM A 480/A480M and AS4194 and the following: 3.2.1.1 Sheet No. 2D finish. 3.2.1.2 Strip No. 1 strip finish. 3.2.2 Plate Hot rolled, solution heat tr

17、eated, and descaled. 3.3 Heat Treatment Except as specified in 3.3.1, the product shall be solution heat treated by heating in a suitable atmosphere within the range 2100 to 2150 F, holding at the selected temperature within 25 F for a time commensurate with product thickness, and rapidly cooling. P

18、yrometry shall be in accordance with AMS2750. 3.3.1 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 specified requ

19、irements. SAE AMS5536N Page 4 of 6 3.4 Properties The product shall conform to the following requirements: 3.4.1 Tensile Properties Shall be as specified in Table 2, determined in accordance with ASTM E 8/E 8M. TABLE 2 - MINIMUM TENSILE PROPERTIES Nominal Thickness Inches Tensile Strength ksi Yield

20、Strength at 0.2% Offset ksi Elongation in 2 Inches or 4D % Up to 0.010, excl 105 45.0 - 0.010 to 0.020, excl 105 45.0 29 0.020 to 0.1874, incl 105 45.0 35 Over 0.1874 to 2.000, incl 100 40.0 35 Over 2.000 95.0 40.0 35 3.4.2 Bending Product 0.1874 inch and under in nominal thickness shall be tested i

21、n accordance with ASTM E 290 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, without cracking, bending at room temperature through an angle of 180 degrees around a diameter equal to the bend factor show

22、n 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 bend test of ASTM E 290 shall govern. TABLE 3 - BENDING PARAMETERS Nominal Thickness Inch Bend Factor Up to 0.050, incl 1.5 Over 0

23、.050 to 0.1874, incl 2 3.4.3 Stress-Rupture Properties at 1500 F A tensile specimen, maintained at 1500 F 3 while a load sufficient to produce an initial axial stress of 16.0 ksi is applied continuously, shall not rupture in less than the time indicated in Table 4. The test shall be continued to rup

24、ture without change of load. Elongation after rupture, measured at room temperature, shall be not less than shown in Table 4. Tests shall be conducted in accordance with ASTM E 139. TABLE 4 - STRESS RUPTURE PARAMETERS Nominal Thickness Inches Time to Rupture Hours, minimum Elongation % in 4D 0.010 t

25、o 0.020, excl 15 3 0.020 and over 24 8 3.4.3.1 The test of 3.4.3 may be conducted using a load higher than required to produce an initial axial stress of 16,0 ksi but load shall not be changed while test is in progress. Time to rupture and elongation requirements shall be as specified in Table 4. 3.

26、4.3.2 The test of 3.4.3 may be conducted using incremental loading. In such case, the load required to produce an initial axial stress of 16.0 ksi shall be used to rupture or for 24 hours, whichever occurs first. After the 24 hours and at intervals of 8 hours minimum, thereafter, the stress shall be

27、 increased in increments of 2000 psi. Time to rupture and elongation requirements shall be as specified in Table 4. SAE AMS5536N Page 5 of 6 3.4.3.2.1 The test of 3.4.3.2 applies only to product 0.020 inch and over in nominal thickness. 3.4.4 Average Grain Size Sheet and strip 0.125 inch and under i

28、n nominal thickness shall have average grain size of ASTM No. 4 or finer, determined in accordance with ASTM E 112. 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

29、product. 3.6 Tolerances Shall conform to all applicable requirements of AMS2262. 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 reserv

30、es 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 (3.4.1), bending (3.4.2), grain size (3.4.4), and tolerances (3.6) a

31、re acceptance tests and shall be performed on each heat or lot as applicable. 4.2.2 Periodic Tests Stress-rupture properties (3.4.3) 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 Sampling and Testing Shall b

32、e in accordance with AMS2371. 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 and bending properties and grain size of each lot and, when performed, the results of tests to determine conformance

33、 to the stress rupture property requirements. This report shall include the purchase order number, heat and lot numbers, AMS5536N, 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.

34、 SAE AMS5536N Page 6 of 6 5.2 Packaging 5.2.1 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 deliv

35、ery. 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 to rejection. 8. NOTES 8.

36、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 this document. An (R) symbol to the left of the document title indicates a complete revision of the document, i

37、ncluding 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 Fahrenheit temperatures are primary; dimensions and pro

38、perties in SI units and 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: AMS5536N Form and Size of product desired Quantity of product desired. PREPARED BY AMS COMMITTEE “F”