1、Designation: B564 15B564 17Standard Specification forNickel Alloy Forgings1This standard is issued under the fixed designation B564; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A number in parentheses
2、 indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.This standard has been approved for use by agencies of the U.S. Department of Defense.1. Scope*1.1 This specification2 covers forgings of:Alloy Type UNS Number(s)Fe-Ni-
3、Cr-Mo-N N08367Low-carbon Cr-Ni-Fe-N R20033Low-carbon Ni-Cr-Mo N06035, N06058, N06059Low-carbon Ni-Cr-Mo N06035, N06058, N06059, N06044Low-carbon Ni-Cr-Mo-Cu N06200Low-carbon Ni-Cr-Mo-W N06686Low-carbon Ni-Fe-Cr-Mo-Cu N08031Low-carbon Ni-Mo-Cr N10276, N06022, N10362Low-carbon Ni-Mo-Cr-Ta N06210Ni N02
4、200Ni-Co-Cr-Si N12160Ni-Cr-Co-Mo N06617Ni-Cr-Fe N06600, N06603, N06690Ni-Cr-Fe-Al N06025Ni-Cr-Fe-Si N06045Ni-Cr-Mo-Nb N06625Ni-Cr-Mo-Si N06219Ni-Cr-Mo-W N06110Ni-Cr-W-Mo N06230Ni-Cu N04400Ni-Fe-Cr N08120, N08800, N08810, N08811Ni-Fe-Cr-Mo-Cu N08825Ni-Fe-Cr-W N06674Ni-Mo N10665, N10675, N10629Ni-Mo-C
5、r-Fe N10242, N106241.1.1 The nickel-iron-chromium alloys are UNS N08120, UNS N08800, UNS N08810, and UNS N08811. Alloy UNS N08800is normally employed in service temperatures up to and including 1100F (593C). Alloys UNS N08810, N08120, and UNSN08811 are normally employed in service temperatures above
6、 1100F (593C) where resistance to creep and rupture is required,and are annealed to develop controlled grain size for optimum properties in this temperature range.1.1.2 Nickel-iron-chromium-tungsten alloy UNS N06674 is normally employed in service temperatures above 1100F (593C)where resistance to c
7、reep and rupture is required, and is annealed to develop optimum properties in this temperature range.1.2 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematicalconversions to SI units that are provided for information only and are not c
8、onsidered standard.1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibilityof the user of this standard to become familiar with all hazards including those identified in the appropriate Safety Data Sheet(SDS) for this product
9、/material as provided by the manufacturer, to establish appropriate safety and health practices, anddetermine the applicability of regulatory limitations prior to use.1.4 This international standard was developed in accordance with internationally recognized principles on standardizationestablished
10、in the Decision on Principles for the Development of International Standards, Guides and Recommendations issuedby the World Trade Organization Technical Barriers to Trade (TBT) Committee.1 This specification is under the jurisdiction ofASTM Committee B02 on Nonferrous Metals andAlloys and is the dir
11、ect responsibility of Subcommittee B02.07 on RefinedNickel and Cobalt and Their Alloys.Current edition approved Oct. 1, 2015June 1, 2017. Published October 2015June 2017. Originally approved in 1972. Last previous edition approved in 20112015 asB564 11B564 15.1. DOI: 10.1520/B0564-15.10.1520/B0564-1
12、7.2 For ASME Boiler and Pressure Vessel Code applications see related Specification SB-564 in Section II of that Code.* New designations established in accordance with ASTM E527 and SAE J1086, Practice for Numbering Metals and Alloys (UNS).This document is not an ASTM standard and is intended only t
13、o provide the user of an ASTM standard an indication of what changes have been made to the previous version. Becauseit may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current versiono
14、f the standard as published by ASTM is to be considered the official document.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States12. Referenced Documents2.1 ASTM Standards:3
15、B880 Specification for General Requirements for Chemical Check Analysis Limits for Nickel, Nickel Alloys and Cobalt AlloysE8 Test Methods for Tension Testing of Metallic MaterialsE29 Practice for Using Significant Digits in Test Data to Determine Conformance with SpecificationsE76 Test Methods for C
16、hemical Analysis of Nickel-Copper Alloys (Withdrawn 2003)4E112 Test Methods for Determining Average Grain SizeE350 Test Methods for Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and WroughtIronE1473 Test Methods for Chemical Analysis of Nickel, Cobalt and
17、High-Temperature Alloys2.2 Military Standards:5MIL-STD-129 Marking for Shipment and StorageMIL-STD-271 Nondestructive Testing Requirements for Metals3. Ordering Information3.1 It is the responsibility of the purchaser to specify all requirements that are necessary for material ordered under thisspec
18、ification. Examples of such requirements include, but are not limited to, the following:3.1.1 Alloy (Table 1).3.1.2 Condition (Table 2).3.1.3 Quantity (mass or number of pieces).3.1.4 Forging, sketch or drawing.3.1.5 CertificationState if certification or a report of test results is required (14.1).
19、3.1.6 Samples for Product (Check) AnalysisWhether samples for product (check) analysis should be furnished (see 4.2).3.1.7 Purchaser InspectionIf the purchaser wishes to witness tests or inspection of material at the place of manufacture, thepurchase order must so state indicating which tests or ins
20、pections are to be witnessed (12.1).4. Chemical Composition4.1 The material shall conform to the composition limits specified in Table 1.4.2 If a product (check) analysis is performed by the purchaser, the material shall conform to the product (check) analysisvariations in accordance with Specificat
21、ion B880.5. Mechanical Properties and Other Requirements5.1 Mechanical PropertiesThe material shall conform to the mechanical properties specified in Table 2.5.2 Grain SizeAnnealed alloys UNS N08810, N08120, and UNS N08811 shall conform to an average grain size of ASTMNo. 5 or coarser. Annealed allo
22、y UNS N06674 shall conform to an average grain size of ASTM No. 7 or coarser.6. Dimensions and Permissible Variations6.1 Dimensions and tolerances shall be as specified on the applicable forging sketch or drawing.7. Workmanship, Finish, and Appearance7.1 The material shall be uniform in quality and
23、condition, sound, and free of injurious imperfections.8. Sampling8.1 Lot Definition:8.1.1 A lot for chemical analysis shall consist of one heat.8.1.2 A lot for mechanical properties and grain size testing shall consist of all material from the same heat, size, finish,condition, and processed at one
24、time.8.2 Test Material Selection:8.2.1 Chemical AnalysisRepresentative samples shall be taken during pouring or subsequent processing.8.2.1.1 Product (check) analysis shall be wholly the responsibility of the purchaser.8.2.2 Mechanical Properties and Grain SizeSamples of the material to provide test
25、 specimens for mechanical properties andgrain size shall be taken from such locations in each lot as to be representative of that lot.3 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume infor
26、mation, refer to the standards Document Summary page on the ASTM website.4 The last approved version of this historical standard is referenced on www.astm.org.5 Available from Standardization Documents Order Desk, DODSSP, Bldg. 4, Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http:/www.d
27、odssp.daps.mil.B564 172TABLE 1 Chemical RequirementsAComposition, %Element NickelAlloyNickel-CopperAlloyLow-CarbonNickel-Molybdenum-ChromiumAlloyNickel-Chromium-Iron-AluminumAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyNickel-Chromium-Iron-SiliconAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyLow-Ca
28、rbonNickel-Chromium-MolybdenumAlloyNickel-Chromium-Molybdenum-TungstenAlloyUNSN02200UNSN04400UNSN06022UNSN06025UNSN06035UNSN06045UNSN06058UNSN06059UNSN06110Nickel 99.0B min 63.0B min balanceB balance balanceB 45 min balance balanceB 51.0B minCopper 0.25 28.034.0 . 0.10 0.30 0.3 0.50 0.50 0.50Iron 0.
29、40 2.5 2.06.0 8.011.0 2.00 21.025.0 1.5 1.5 1.0Manganese 0.35 2.0 0.50 0.15 0.50 1.0 0.50 0.5 1.0Carbon 0.15 0.3 0.015 0.150.25 0.050 0.050.12 0.010 0.010 0.15Silicon 0.35 0.5 0.08 0.5 0.60 2.53.0 0.10 0.10 1.0Sulfur 0.01 0.024 0.02 0.01 0.015 0.010 0.010 0.010 0.015Chromium . . 20.022.5 24.026.0 32
30、.2534.25 26.029.0 20.023.0 22.024.0 28.033.0Aluminum . . . 1.82.4 0.40 . 0.40 0.10.4 1.0Titanium . . . 0.10.2 . . . . 1.0Columbium(Nb) +Tantalum. . . . . . . . 1.0Molybdenum . . 12.514.5 . 7.609.00 . 18.521.0 15.016.5 9.012.0Phosphorus . . 0.02 0.02 0.030 0.02 0.015 0.015 0.50Tungsten . . 2.53.5 . 0
31、.60 . 0.3 . 1.0-4.0Cobalt . . 2.5 . 1.00 . 0.3 0.3 .Vanadium . . 0.35 . 0.20 . . . .Nitrogen . . . . . . 0.02 - 0.15 . .Boron . . . . . . . . .LanthanumAluminum +Titanium.Nickel +Molybdenum. . . . . . . . .Columbium(Nb). . . . . . . . .Tantalum . . . . . . . . .Zirconium . . . 0.010.10 . . . . .Ceri
32、um . . . . . 0.030.09 . . .Yttrium . . . 0.050.12 . . . . .TABLE 1 Chemical RequirementsAComposition, %Element NickelAlloyNickel-CopperAlloyLow-CarbonNickel-Molybdenum-ChromiumAlloyNickel-Chromium-Iron-AluminumAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyNic
33、kel-Chromium-Iron-SiliconAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyNickel-Chromium-Molybdenum-TungstenAlloyUNSN02200UNSN04400UNSN06022UNSN06025UNSN06035UNSN06044UNSN06045UNSN06058UNSN06059UNSN06110Nickel 99.0B min 63.0B min balanceB balance balanceB balan
34、ce 45 min balance balanceB 51.0B minCopper 0.25 28.0-34.0 . 0.10 0.30 . 0.3 0.50 0.50 0.50Iron 0.40 2.5 2.0-6.0 8.0-11.0 2.00 0.3 max 21.0-25.0 1.5 1.5 1.0Manganese 0.35 2.0 0.50 0.15 0.50 0.07-0.30 1.0 0.50 0.5 1.0Carbon 0.15 0.3 0.015 0.15-0.25 0.050 0.02 max 0.05-0.12 0.010 0.010 0.15Silicon 0.35
35、 0.5 0.08 0.5 0.60 0.20 max 2.5-3.0 0.10 0.10 1.0Sulfur 0.01 0.024 0.02 0.01 0.015 0.020 max 0.010 0.010 0.010 0.015Chromium . . 20.0-22.5 24.0-26.0 32.25-34.2543.5-45.3 26.0-29.0 20.0-23.0 22.0-24.0 28.0-33.0Aluminum . . . 1.8-2.4 0.40 0.30 max . 0.40 0.1-0.4 1.0Titanium . . . 0.1-0.2 . 0.10-0.30 .
36、 . . 1.0Columbium(Nb) +Tantalum. . . . . . . . . 1.0Molybdenum . . 12.5-14.5 . 7.60-9.00 0.80-1.20 . 18.5-21.0 15.0-16.5 9.0-12.0Phosphorus . . 0.02 0.02 0.030 0.020 max 0.02 0.015 0.015 0.50Tungsten . . 2.5-3.5 . 0.60 . . 0.3 . 1.0-4.0Cobalt . . 2.5 . 1.00 . . 0.3 0.3 .Vanadium . . 0.35 . 0.20 . .
37、. . .Nitrogen . . . . . . . 0.02 - 0.15 . .Boron . . . . . . . . . .Lanthanum . . . . . . . . . .B564 1739. Number of Tests9.1 Chemical AnalysisOne test per lot.9.2 Mechanical PropertiesOne test per lot.Composition, %Element NickelAlloyNickel-CopperAlloyLow-CarbonNickel-Molybdenum-ChromiumAlloyNicke
38、l-Chromium-Iron-AluminumAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyNickel-Chromium-Iron-SiliconAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyNickel-Chromium-Molybdenum-TungstenAlloyAluminum +Titanium. . . . . . . .
39、. .Nickel +Molybdenum. . . . . . . . . .Columbium(Nb). . . . . . . . . .Tantalum . . . . . . . . . .Zirconium . . . 0.01-0.10 . . . . . .Cerium . . . . . . 0.03-0.09 . . .Yttrium . . . 0.05-0.12 . . . . . .A Maximum unless range or minimum is given. Where ellipses (.) appear in this table there is n
40、o requirement and the element need neither be analyzed for nor reported.B Element shall be determined arithmetically by difference.TABLE 1 Chemical RequirementsA (continued)Composition, %ElementLow-CarbonNickel-Chromium-Molybdenum-CopperAlloyLow-CarbonNickel-Molybdenum-Chromium-TantalumAlloyNickel-C
41、hromium-Molybdenum-SiliconAlloyNickelChromium-Tungsten-MolybdenumAlloyNickel-Chromium-Iron-AluminumAlloyNickelChromium-Cobalt-MolybdenumAlloyNickel-Chromium-Molybdenum-ColumbiumAlloyNickel-Chromium-IronAlloyNickel-Iron-Chromium-TungstenAlloyUNSN06200UNSN06210UNSN06219UNSN06230UNSN06603UNSN06617UNSN0
42、6625UNSN06600UNSN06674Nickel balanceB balanceB balanceB balanceB balanceB 44.5 min 58.0B min 72.0B min balanceBCopper 1.31.9 . 0.50 . 0.5 0.5 . 0.5 .Iron 3.0 1.0 2.0-4.0 3.0 8.011.0 3.0 5.0 6.010.0 20.0-27.0Manganese 0.50 0.5 0.50 0.301.00 0.15 1.0 0.5 1.0 1.50Carbon 0.010 0.015 0.05 0.050.15 0.200.
43、40 0.050.15 0.10 0.15 0.10Silicon 0.08 0.08 0.70-1.10 0.250.75 0.5 1.0 0.5 0.5 1.0Sulfur 0.010 0.02 0.010 0.015 0.010 0.015 0.015 0.015 0.015Chromium 22.024.0 18.0-20.0 18.0-22.0 20.024.0 24.026.0 20.024.0 20.023.0 14.017.0 21.5-24.5Aluminum 0.50 . 0.50 0.50 2.43.0 0.81.5 0.4 . .Titanium . . 0.50 .
44、0.010.25 0.6 0.4 . 0.05-0.20Columbium(Nb) +Tantalum. . . . . . 3.154.15 . .Molybdenum 15.017.0 18.0-20.0 7.0-9.0 1.03.0 . 8.010.0 8.010.0 . .Phosphorus 0.025 0.02 0.020 0.030 0.02 . 0.015 . 0.030Tungsten . . . 13.015.0 . . . . 6.0-8.0Cobalt 2.0 1.0 1.0 5.0 . 10.0 min15.0. . .Vanadium . 0.35 . . . .
45、. . .Nitrogen . . . . . . . . 0.02Boron . . . 0.015 . 0.006 . . 0.0005-0.006LanthanumAluminum +Titanium. . . 0.0050.050. .Nickel +Molybdenum. . . . . . . . .Columbium(Nb). . . . . . . . 0.10-0.35Tantalum . 1.5-2.2 . . . . . . .Zirconium . . . . 0.010.10 . . . .Cerium . . . . . . . . .Yttrium . . . .
46、 0.010.15 . . . .A Maximum unless range or minimum is given. Where ellipses (.) appear in this table there is no requirement and the element need neither be analyzed for nor reported.B Element shall be determined arithmetically by difference.B564 1749.3 Grain SizeFor alloys N08810, N08120, UNS N0881
47、1, and N06674, one test per lot.10. Specimen Preparation10.1 The tension test specimen representing each lot shall be taken from a forging or from a test prolongation.10.2 The axis of the specimen shall be located at any point midway between the center and the surface of solid forgings andat any poi
48、nt midway between the inner and outer surfaces of the wall of hollow forgings, and shall be parallel to the direction ofgreatest metal flow. Specimens transverse to the direction of flow may be used provided all other requirements of this standard aresatisfied.10.3 The specimens shall be the largest
49、 possible round type shown in Test Methods E8.11. Test Methods11.1 The chemical composition, mechanical, and other properties of the material as enumerated in this specification shall bedetermined, in case of disagreement, in accordance with the following methods:Test ASTM DesignationChemical Analysis E76, E350, E1473Tension E8Rounding Procedure E29Grain Size E11211.2 The measurement of average grain size may be carried out by the planimetric method, the comparison method, or thein
