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    ASTM B564-2018 Standard Specification for Nickel Alloy Forgings.pdf

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    ASTM B564-2018 Standard Specification for Nickel Alloy Forgings.pdf

    1、Designation: B564 18Standard 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 indica

    2、tes 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 specification2covers forgings of:Alloy Type UNS Number(s)Fe-Ni-Cr-Mo-N

    3、N08367Low-carbon Cr-Ni-Fe-N R20033Low-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 N08031, N08034Low-carbon Ni-Mo-Cr N10276, N06022, N10362Low-carbon Ni-Mo-Cr-Ta N06210Ni N02200Ni-Co-Cr-Si N12160Ni-Cr-Al N06699Ni-Cr-

    4、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-Cr-Fe N10242, N106241.1.1 Th

    5、e nickel-iron-chromium alloys are UNS N08120,UNS N08800, UNS N08810, and UNS N08811. Alloy UNSN08800 is normally employed in service temperatures up toand including 1100F (593C). Alloys UNS N08810, N08120,and UNS N08811 are normally employed in service tempera-tures above 1100F (593C) where resistan

    6、ce to creep andrupture is required, and are annealed to develop controlledgrain size for optimum properties in this temperature range.1.1.2 Nickel-iron-chromium-tungsten alloy UNS N06674 isnormally employed in service temperatures above 1100F(593C) where resistance to creep and rupture is required,

    7、andis annealed to develop optimum properties in this temperaturerange.1.2 The values stated in inch-pound units are to be regardedas standard. The values given in parentheses are mathematicalconversions to SI units that are provided for information onlyand are not considered standard.1.3 This standa

    8、rd does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to become familiarwith all hazards including those identified in the appropriateSafety Data Sheet (SDS) for this product/material as providedby the manufact

    9、urer, to establish appropriate safety, health,and environmental practices, and determine the applicabilityof regulatory limitations prior to use.1.4 This international standard was developed in accor-dance with internationally recognized principles on standard-ization established in the Decision on

    10、Principles for theDevelopment of International Standards, Guides and Recom-mendations issued by the World Trade Organization TechnicalBarriers to Trade (TBT) Committee.2. Referenced Documents2.1 ASTM Standards:3B880 Specification for General Requirements for ChemicalCheck Analysis Limits for Nickel,

    11、 Nickel Alloys andCobalt AlloysE8/E8M Test Methods for Tension Testing of Metallic Ma-terialsE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE76 Test Methods for Chemical Analysis of Nickel-CopperAlloys (Withdrawn 2003)4E112 Test Methods for Determin

    12、ing Average Grain SizeE350 Test Methods for Chemical Analysis of Carbon Steel,Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, andWrought IronE1473 Test Methods for Chemical Analysis of Nickel, Co-balt and High-Temperature Alloys1This specification is under the jurisdiction of ASTM Committee B

    13、02 onNonferrous Metals and Alloys and is the direct responsibility of SubcommitteeB02.07 on Refined Nickel and Cobalt and Their Alloys.Current edition approved Nov. 1, 2018. Published November 2018. Originallyapproved in 1972. Last previous edition approved in 2017 as B564 17a. DOI:10.1520/B0564-18.

    14、2For ASME Boiler and Pressure Vessel Code applications see related Specifi-cation SB-564 in Section II of that Code.3For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to

    15、the standards Document Summary page onthe ASTM website.4The last approved version of this historical standard is referenced onwww.astm.org.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-29

    16、59. United StatesThis international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recommendations issued by the World Trade Organization Technical

    17、Barriers to Trade (TBT) Committee.12.2 Military Standards:5MIL-STD-129 Marking for Shipment and StorageMIL-STD-271 Nondestructive Testing Requirements forMetals3. Ordering Information3.1 It is the responsibility of the purchaser to specify allrequirements that are necessary for material ordered unde

    18、r thisspecification. Examples of such requirements include, but arenot 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 testresults is required

    19、 (14.1).3.1.6 Samples for Product (Check) AnalysisWhethersamples for product (check) analysis should be furnished (see4.2).3.1.7 Purchaser InspectionIf the purchaser wishes towitness tests or inspection of material at the place ofmanufacture, the purchase order must so state indicating whichtests or

    20、 inspections are to be witnessed (12.1).4. Chemical Composition4.1 The material shall conform to the composition limitsspecified in Table 1.4.2 If a product (check) analysis is performed by thepurchaser, the material shall conform to the product (check)analysis variations in accordance with Specific

    21、ation B880.5. Mechanical Properties and Other Requirements5.1 Mechanical PropertiesThe material shall conform tothe mechanical properties specified in Table 2.5.2 Grain SizeAnnealed alloys UNS N08810, N08120,and UNS N08811 shall conform to an average grain size ofASTM No. 5 or coarser. Annealed allo

    22、y UNS N06674 shallconform 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 theapplicable forging sketch or drawing.7. Workmanship, Finish, and Appearance7.1 The material shall be uniform in quality and co

    23、ndition,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 testingshall consist of all material from the same heat, size, finish,condition, and processed at one time

    24、.8.2 Test Material Selection:8.2.1 Chemical AnalysisRepresentative samples shall betaken during pouring or subsequent processing.8.2.1.1 Product (check) analysis shall be wholly the respon-sibility of the purchaser.8.2.2 Mechanical Properties and Grain SizeSamples ofthe material to provide test spec

    25、imens for mechanical proper-ties and grain size shall be taken from such locations in each lotas to be representative of that lot.9. Number of Tests9.1 Chemical AnalysisOne test per lot.9.2 Mechanical PropertiesOne test per lot.9.3 Grain SizeFor alloys N08810, N08120, UNS N08811,and N06674, one test

    26、 per lot.10. Specimen Preparation10.1 The tension test specimen representing each lot shallbe taken from a forging or from a test prolongation.10.2 The axis of the specimen shall be located at any pointmidway between the center and the surface of solid forgingsand at any point midway between the inn

    27、er and outer surfacesof the wall of hollow forgings, and shall be parallel to thedirection of greatest metal flow. Specimens transverse to thedirection of flow may be used provided all other requirementsof this standard are satisfied.10.3 The specimens shall be the largest possible round typeshown i

    28、n Test Methods E8/E8M.11. Test Methods11.1 The chemical composition, mechanical, and otherproperties of the material as enumerated in this specificationshall be determined, in case of disagreement, in accordancewith the following methods:Test ASTM DesignationChemical Analysis E76, E350, E1473Tension

    29、 E8/E8MRounding Procedure E29Grain Size E11211.2 The measurement of average grain size may be carriedout by the planimetric method, the comparison method, or theintercept method described in Test Methods E112. In case ofdispute, the “referee” method for determining average grainsize shall be the pla

    30、nimetric method.11.3 For purposes of determining compliance with thespecified limits for requirements of the properties listed in thefollowing table, an observed value, or a calculated value, shallbe rounded as indicated as follows, in accordance with therounding method of Practice E29:TestRounded U

    31、nit for Observed orCalculated ValueChemical composition nearest unit in the last right-hand placeof figures of the specified limitTensile strength, yield strength nearest 1000 psi (6.9 MPa)Elongation nearest 1 %Grain size:0.0024 in. (0.060 mm) or larger nearest multiple of 0.0002 in. (0.005 mm)less

    32、than 0.0024 in. (0.060 mm) nearest multiple of 0.0001 in. (0.002 mm)5Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http:/www.dodssp.daps.mil.B564 182TABLE1ChemicalRequirementsAComposition,%ElementNickel AlloyNickel- Cop

    33、per AlloyLow- Carbon Nickel- Molybdenum- Chromium AlloyNickel- Chromium- Iron- Aluminum AlloyLow-Carbon Nickel- Chromium- Molybdenum AlloyLow- Carbon Nickel- Chromium- Molybdenum AlloyNickel- Chromium- Iron-Silicon AlloyLow- Carbon Nickel- Chromium- Molybdenum AlloyLow- Carbon Nickel- Chromium- Moly

    34、bdenum AlloyNickel- Chromium- Molybdenum- TungstenAlloyUNS N02200UNS N04400UNS N06022UNS N06025UNS N06035UNS N06044UNS N06045UNS N06058UNS N06059UNS N06110Nickel99.0Bmin63.0BminbalanceBbalancebalanceBbalance45minbalancebalanceB51.0BminCopper0.2528.0-34.0.0.100.30.0.30.500.500.50Iron0.402.52.0-6.08.0

    35、-11.02.000.3max21.0-25.01.51.51.0Manganese0.352.00.500.150.500.07-0.301.00.500.51.0Carbon0.150.30.0150.15-0.250.0500.02max0.05-0.120.0100.0100.15Silicon0.350.50.080.50.600.20max2.5-3.00.100.101.0Sulfur0.010.0240.020.010.0150.020max0.0100.0100.0100.015Chromium.20.0-22.524.0-26.032.25-34.2543.5-45.326

    36、.0-29.020.0-23.022.0-24.028.0-33.0Aluminum.1.8-2.40.400.30max.0.400.1-0.41.0Titanium.0.1-0.2.0.10-0.30.1.0Columbium(Nb)+Tantalum.1.0Molybdenum.12.5-14.5.7.60-9.000.80-1.20.18.5-21.015.0-16.59.0-12.0Phosphorus.0.020.020.0300.020max0.020.0150.0150.50Tungsten.2.5-3.5.0.60.0.3.1.0-4.0Cobalt.2.5.1.00.0.3

    37、0.3.Vanadium.0.35.0.20.Nitrogen.0.02-0.15.Boron.Lanthanum.Aluminum+Titanium.Nickel+Molybdenum.Columbium(Nb).Tantalum.Zirconium.0.01-0.10.Cerium.0.03-0.09.Yttrium.0.05-0.12.AMaximumunlessrangeorminimumisgiven.Whereellipses(.)appearinthistablethereisnorequirementandtheelementneedneitherbeanalyzedforno

    38、rreported.BElementshallbedeterminedarithmeticallybydifference.B564 183TABLE1ChemicalRequirementsA(continued)Composition,%ElementLow- Carbon Nickel- Chromium- Molybdenum- Copper AlloyLow-Carbon Nickel- Molybdenum- Chromium- TantalumAlloyNickel- Chromium- Molybdenum- Silicon AlloyNickel Chromium- Tung

    39、sten-Molybdenum AlloyNickel- Chromium- Iron- Aluminum AlloyNickel Chromium- Cobalt- Molybdenum AlloyNickel- Chromium- Molybdenum- Columbium AlloyNickel- Chromium- Iron AlloyNickel- Iron- Chromium- TungstenAlloyUNS N06200UNS N06210UNS N06219UNS N06230UNS N06603UNS N06617UNS N06625UNS N06600UNS N06674

    40、NickelbalanceBbalanceBbalanceBbalanceBbalanceB44.5min58.0Bmin72.0BminbalanceBCopper1.31.9.0.50.0.50.5.0.5.Iron3.01.02.0-4.03.08.011.03.05.06.010.020.0-27.0Manganese0.500.50.500.301.000.151.00.51.01.50Carbon0.0100.0150.050.050.150.200.400.050.150.100.150.10Silicon0.080.080.70-1.100.250.750.51.00.50.5

    41、1.0Sulfur0.0100.020.0100.0150.0100.0150.0150.0150.015Chromium22.024.018.0-20.018.0-22.020.024.024.026.020.024.020.023.014.017.021.5-24.5Aluminum0.50.0.500.502.43.00.81.50.4.Titanium.0.50.0.010.250.60.4.0.05-0.20Columbium(Nb)+Tantalum.3.154.15.Molybdenum15.017.018.0-20.07.0-9.01.03.0.8.010.08.010.0.P

    42、hosphorus0.0250.020.0200.0300.02.0.015.0.030Tungsten.13.015.0.6.0-8.0Cobalt2.01.01.05.0.10.0min15.0.Vanadium.0.35.Nitrogen.0.02Boron.0.015.0.006.0.0005- 0.006Lanthanum Aluminum+Titanium.0.0050.050 . . . .Nickel+Molybdenum.Columbium(Nb).0.10-0.35Tantalum.1.5-2.2.Zirconium.0.010.10.Cerium.Yttrium.0.01

    43、0.15.AMaximumunlessrangeorminimumisgiven.Whereellipses(.)appearinthistablethereisnorequirementandtheelementneedneitherbeanalyzedfornorreported.BElementshallbedeterminedarithmeticallybydifference.B564 184TABLE1ChemicalRequirementsA(continued)Composition,%ElementLow- Carbon Nickel- Chromium- Molybdenu

    44、m- TungstenAlloyNickel- Chromium- Iron AlloyNickel- Chromium- Aluminum AlloyLow- Carbon Nickel- Iron- Chromium- Molybdenum- Copper AlloyLow- Carbon Nickel- Iron- Chromium- Molybdenum- Copper AlloyNickel- Iron- Chromium AlloyIron- Nickel- Chromium- Molybdenum- Nitrogen AlloyNickel- Iron- Chromium All

    45、oyNickel-Iron- Chromium AlloyNickel-Iron- Chromium AlloyNickel- Iron- Chromium- Molybdenum- Copper AlloyUNS N06686UNS N06690UNS N06699UNS N08031UNS N08034UNS N08120UNS N08367UNS N08800UNS N08810UNS N08811UNS N08825Nickelremainder58.0Bminremanider30.032.033.535.035.039.023.5025.5030.035.030.035.030.0

    46、35.038.046.0Copper.0.50.501.01.40.51.50.500.750.750.750.751.53.0Iron5.07.011.02.5balanceBbalanceBbalancebalanceB39.5Bmin39.5Bmin39.5Bmin22.0BminManganese0.750.50.502.01.04.01.52.001.51.51.51.0Carbon0.0100.050.005-0.100.0150.010.020.100.0300.100.050.100.060.100.05Silicon0.080.50.500.30.11.01.001.01.0

    47、1.00.5Sulfur0.020.0150.010.0100.0100.030.0300.0150.0150.0150.03Chromium19.023.027.031.026.0-30.026.0-28.026.027.023.027.020.022.019.023.019.023.019.023.019.523.5Aluminum.1.9-3.0.0.30.40.0.150.600.150.600.150.600.2Titanium0.020.25.0.60.0.20.0.150.600.150.600.150.600.61.2Columbium(Nb)+Tantalum.0.40.9.

    48、Molybdenum15.017.0.6.0-7.06.07.02.506.007.00.2.53.5Phosphorus0.04.0.020.0200.0200.0400.040.Tungsten3.04.4.2.50.Cobalt.3.0.Vanadium.Nitrogen.0.050.15-0.250.100.250.150.300.180.25.Boron.0.008.0.010.Lanthanum Aluminum+Titanium. . . . . . . 0.851.20. .Nickel+Molybdenum.Columbium(Nb).0.50.Tantalum.Zirconium.0.10.Cerium.Yttrium.AMaximumunlessrangeorminimumisgiven.Whereellipses(.)appearinthistablethereisnorequirementandtheelementneedneitherbeanalyzedfornorreported.BElementshallbedeterminedarithme


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