SAE AMS 5606F-2013 Alloy Corrosion and Heat-Resistant Sheet Strip and Plate 41 5Ni - 16Cr - 37Fe - 2 9Cb - 1 8Ti Consumable Electrode or Vacuum Induction Melted 1750 (954 Solution .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 theref

2、rom, 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 InternationalAll rights reserved. No part of this publi

3、cation 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: +1 724-776-4970 (out

4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS5606FAEROSPACE MATERIAL SPECIFICATIONAMS5606 REV. FIssued 1971-11Revised 2013-12Supersedin

5、g AMS5606EAlloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate41.5Ni - 16Cr - 37Fe - 2.9Cb (NB) - 1.8TiConsumable Electrode or Vacuum Induction Melted1750 F (954 C) Solution Heat Treated(Composition similar to UNS N09706)RATIONALEAMS5606F adjusts the size breaks for various properties (Table

6、s 2, 3, 4, and 5) to more accurately reflect the breakpoint between sheet and plate, revises Bending (3.5.1.3), Stress Rupture Testing (3.5.2.3.2), Reports (4.4), and results from a Five Year Review and update of this specification.1. SCOPE1.1 FormThis specification covers a corrosion and heat-resis

7、tant nickel alloy in the form of sheet, strip, and plate.1.2 ApplicationThese products have been used typically for parts requiring resistance to creep and stress-rupture up to 1300 F (704 C), oxidation resistance up to 1800 F (982 C), and good machinability, particularly for those parts which are f

8、ormed or welded and then heat treated to develop required properties, but usage is not limited to such applications.2. APPLICABLE DOCUMENTSThe 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

9、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.2.1 SAE PublicationsAvailable from SAE International, 4

10、00 Commonwealth 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 PlateAMS2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt AlloysSAE

11、 INTERNATIONAL AMS5606F Page 2 of 7AMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockAMS2807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys, Sheet, Strip, Plate, and Aircraft

12、TubingAS4194 Sheet and Strip Surface Finish Nomenclature2.2 ASTM PublicationsAvailable 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 S

13、tripASTM E 8/E 8M Tension Testing of Metallic MaterialsASTM E 18 Rockwell Hardness of Metallic MaterialsASTM E 112 Determining Average Grain SizeASTM E 139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic MaterialsASTM E 290 Bend Test of Materials for DuctilityASTM E 354 Chemica

14、l Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt AlloysASTM E 384 Knoop and Vickers Hardness of Materials3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordan

15、ce with ASTM E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser.TABLE 1 - COMPOSITIONElement min maxCarbon - 0.06Manganese - 0.35Silicon - 0.35Phosphorus - 0.020Sulfur - 0.015Chromium 14.50 17.50Nickel 39.00 44.00Columbium (Niobium) 2.50 3.30Tantalum - 0.05Tita

16、nium 1.50 2.00Aluminum - 0.40Boron - 0.006Copper - 0.30Iron remainder3.1.1 Check AnalysisComposition variations shall meet the applicable requirements of AMS2269.SAE INTERNATIONAL AMS5606F Page 3 of 73.2 Melting PracticeAlloy shall be produced by multiple melting using consumable electrode practice

17、in the remelt cycle or shall be induction melted under vacuum. If consumable electrode remelting is not performed in vacuum, electrodes which have been produced by vacuum induction melting shall be used for remelting. 3.3 ConditionThe product shall be supplied in the following condition:3.3.1 Sheet

18、and StripCold rolled, solution heat 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 A480/A 480M and AS4194 and the

19、following:3.3.1.1 SheetNo. 2D finish.3.3.1.2 StripNo. 1 Strip finish.3.3.2 PlateHot rolled, solution heat treated, and descaled.3.4 Heat TreatmentNo specific solution heat treatment is specified but it is recommended that the product be solution heat treated by heating in a suitable protective atmos

20、phere to a temperature within the range 1700 to 1800 F (927 to 982 C), holding at the selected temperature within 25 F (14 C) for a time commensurate with section thickness but not less than 5 minutes, and cooling at a rate equivalent to an air cool or faster.3.5 PropertiesThe product shall conform

21、to the following requirements:3.5.1 As Solution Heat Treated: 3.5.1.1 Tensile PropertiesShall be as specified in Table 2, determined in accordance with ASTM E 8/E 8M.TABLE 2A - TENSILE PROPERTIES, INCH/POUND UNITSNominal ThicknessInchesTensile Strengthksi, maxYield Strength at 0.2% Offsetksi, maxElo

22、ngation in2 Inches or 4D%, minUp to 0.1875, excl0.1875 and over13014080.090.03030SAE INTERNATIONAL AMS5606F Page 4 of 7TABLE 2B - TENSILE PROPERTIES, SI UNITSNominal ThicknessMillimetersTensile StrengthMPa, maxYield Strength at 0.2% OffsetMPa, maxElongation in50.8 mm or 4D%, minUp to 4.762, excl4.76

23、2 and over89696555262130303.5.1.2 HardnessShall be not higher than shown in Table 3, or equivalent (See 8.2), determined in accordance with ASTM E 18; for thin gages, where superficial hardness testing is impractical, microhardness testing in accordance with ASTM E 384 may be used. Product shall not

24、 be rejected on the basis of hardness if the tensile properties of 3.5.1.1 are acceptable, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similar nonconforming hardness. TABLE 3 - MAXIMUM HARDNESSNominal ThicknessInchesNominal Thick

25、nessMillimeters HardnessUp to 0.1875, excl0.1875 and overUp to 4.762, excl4.762 and over102 HRB25 HRC3.5.1.3 BendingProduct 0.1874 inch (4.75 mm) and under in nominal thickness 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

26、of bending 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 times the nominal thickness of the product shown in Table 4. In case of dispute, the results of tests usi

27、ng the guided bend test of ASTM E 290 shall govern.TABLE 4 - BENDINGNominal ThicknessInchesNominal ThicknessMillimeters Bend FactorUp to 0.050, inclOver 0.050 to 0.1874, inclUp to 1.27, inclOver 1.27 to 4.762, incl123.5.1.4 Average Grain SizeShall be as shown in Table 5, determined in accordance wit

28、h ASTM E 112.TABLE 5 - AVERAGE GRAIN SIZENominal ThicknessInchesNominal ThicknessMillimeters Grain SizeUp to 0.1875, excl0.1875 and overUp to 4.762, inclOver 4.7625 or finer4 or finer3.5.2 After Stabilization and Precipitation Heat TreatmentThe product, 0.010 to 1.000 inch (0.25 to 25.40 mm) in nomi

29、nal thickness, shall have the following properties after being stabilization heat treated by heating to 1550 F 15 (843 C 8), holding at heat for 3 hours 0.25, and cooling in air to room temperature and precipitation heat treated by heating to 1325 F 15 (718 C 8), holding at heat for 8 hours 0.25, co

30、oling at a rate of 100 F (56 C) degrees per hour to 1150 F 15 (621 C 8), holding at 1150 F 15 (621 C 8) for 8 hours 0.25, and cooling in air. Instead of the 100 F (56 C) degrees per hour cooling rate to 1150 F 15 (621 C 8), furnace cooling may be at any rate provided the time at 1150 F 15 (621 C 8)

31、is adjusted to give a total precipitation heat treatment time of not less than 18 hours. Properties of product under 0.010 inch (0.25 mm) or over 1.000 inch (25.40 mm) in nominal thickness shall be as agreed upon by purchaser and vendor.SAE INTERNATIONAL AMS5606F Page 5 of 73.5.2.1 Tensile Propertie

32、sShall be as specified in Table 6, determined in accordance with ASTM E 8/E 8M.TABLE 6 - MINIMUM TENSILE PROPERTIESProperty ValueTensile StrengthYield Strength at 0.2% OffsetElongation in 2 Inches (50.8 mm) or 4D170 ksi (1172 MPa)135 ksi ( 931 MPa)12%3.5.2.2 HardnessShall be not lower than 30 HRC, o

33、r equivalent (See 8.2), determined in accordance with ASTM E 18; for thin gages, where superficial hardness testing is impractical, microhardness testing in accordance with ASTM E 384 may be used. Product shall not be rejected on the basis of hardness if the tensile properties of 3.5.2.1 are accepta

34、ble, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similar nonconforming hardness.3.5.2.3 Stress-Rupture Properties at 1200 F (649 C)A tensile specimen, maintained at 1200 F 3 (649 C 2) while a load sufficient to produce the initia

35、l axial stress specified in Table 7 is applied continuously, shall not rupture in less than 23 hours. The test shall be continued to rupture without change of load. Elongation after rupture, measured at room temperature, shall be as specified in Table 7. Tests shall be conducted in accordance with A

36、STM E 139.TABLE 7A - STRESS-RUPTURE PROPERTIES, INCH/POUND UNITSNominal ThicknessInchesInitial Axial StressksiElongation in 2 Inches or 4D %, minUp to 0.015, inclOver 0.015 to 0.025, incl Over 0.0259595100-33TABLE 7B - STRESS-RUPTURE PROPERTIES, SI UNITSNominal ThicknessMillimetersInitial Axial Stre

37、ss MPaElongation in 50.8 mm or 4D %, minUp to 0.38, inclOver 0.38 to 0.64, inclOver 0.64655655689-333.5.2.3.1 The test of 3.5.2.3 may be conducted using a load higher than required to produce the initial axial stress specified in Table 7 but load shall not be changed while test is in progress. Time

38、to rupture and elongation requirements shall be as specified in 3.5.2.3.3.5.2.3.2 When permitted by purchaser, the test of 3.5.2.3 may be conducted using incremental loading. In such case, the load required to produce the initial axial stress specified in Table 7 shall be maintained to rupture or fo

39、r 23 hours, whichever occurs first. After the 23 hours and at intervals of 8 hours, minimum, thereafter, the stress shall be increased in increments of 5.0 ksi (34.5 MPa). Time to rupture and elongation requirements shall be as specified in 3.5.2.3.3.6 QualityThe product, as received by purchaser, s

40、hall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the product.SAE INTERNATIONAL AMS5606F Page 6 of 73.7 TolerancesShall conform to all applicable requirements of AMS2262.4. QUALITY ASSURANCE PROVISIONS4.1 Responsibility fo

41、r InspectionThe vendor of the product shall supply all samples for vendors 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 requir

42、ements.4.2 Classification of TestsAll technical requirements are acceptance tests and shall be performed on each heat or lot as applicable.4.3 Sampling and TestingShall be in accordance with AMS2371. 4.4 ReportsThe vendor of the product shall furnish with each shipment a report showing the results o

43、f tests for composition of each heat and for tensile properties, hardness, bending and average grain size as solution heat treated for each lot, and for tensile properties, hardness and stress rupture properties as precipitation heat treated for each lot, and stating that the product conforms to the

44、 other technical requirements. This report shall include the purchase order number, heat and lot numbers, AMS5606F, solution heat treatment temperature used, size, product form, and quantity.4.5 Resampling and RetestingShall be in accordance with AMS2371.5. PREPARATION FOR DELIVERY5.1 Identification

45、Shall be in accordance with AMS2807.5.2 PackagingThe 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 de

46、livery. 6. ACKNOWLEDGMENTA vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders.7. REJECTIONSProduct not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection.8. NOTES8.1

47、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, inc

48、luding technical revisions. Change bars and (R) are not used in original publications, nor in documents that contain editorial changes only.SAE INTERNATIONAL AMS5606F Page 7 of 78.2 Hardness conversion tables for metals are presented in ASTM E 140.8.3 Terms used in AMS are clarified in ARP1917.8.4 D

49、imensions 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:AMS5606FProduct form and size of product desiredQu