1、Designation: B564 11Standard 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 Department of Defense.1. Scope*1.1 This specification2covers forgings of:Alloy Type UNS Number(s)Fe-Ni-Cr-Mo-N N0836
3、7Low-carbon Cr-Ni-Fe-N R20033Low-carbon Ni-Cr-Mo N06035, N06058, N06059Low-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 N02200Ni-Co-Cr-Si N12160Ni-Cr-Co-Mo N06617Ni-Cr-Fe N06600, N06603,
4、 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 The nickel-iron-chromium alloys are UN
5、S 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 resistance to creep andrupture is required,
6、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, andis annealed to develop optimum pr
7、operties 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 standard does not purport to address all o
8、f 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 appropriateMaterial Safety Data Sheet (MSDS) for this product/materialas provided by the manufacturer, to establish appropr
9、iatesafety and health practices, and determine the applicability ofregulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:3B880 Specification for General Requirements for ChemicalCheck Analysis Limits for Nickel, Nickel Alloys andCobalt AlloysE8 Test Methods for Tension Testin
10、g of Metallic MaterialsE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE76 Test Methods for Chemical Analysis of Nickel-CopperAlloys4E112 Test Methods for Determining Average Grain SizeE350 Test Methods for Chemical Analysis of Carbon Steel,Low-Alloy
11、 Steel, Silicon Electrical Steel, Ingot Iron, andWrought IronE1473 Test Methods for Chemical Analysis of Nickel,1This specification is under the jurisdiction of ASTM Committee B02 onNonferrous Metals and Alloys and is the direct responsibility of SubcommitteeB02.07 on Refined Nickel and Cobalt and T
12、heir Alloys.Current edition approved Oct. 1, 2011. Published November 2011. Originallyapproved in 1972. Last previous edition approved in 2010 as B564 10. DOI:10.1520/B0564-11.2For ASME Boiler and Pressure Vessel Code applications see related Specifi-cation SB-564 in Section II of that Code.* New de
13、signations established in accordance withASTM E527 and SAE J1086,Practice for Numbering Metals and Alloys (UNS).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 the
14、standards Document Summary page onthe ASTM website.4Withdrawn. The last approved version of this historical standard is referencedon www.astm.org.1*A Summary of Changes section appears at the end of this standard.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA
15、 19428-2959, United States.Cobalt, and High-Temperature Alloys2.2 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 necessar
16、y for material ordered under 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
17、 of testresults is required (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 of manu-facture, the purchase order must so s
18、tate indicating which testsor 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 variation
19、s in accordance with Specification 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
20、. 5 or coarser. Annealed alloy 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
21、be uniform in quality and 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 testingshall consist of all material from the same heat, size, finish,conditio
22、n, and processed at one time.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 m
23、aterial to provide test specimens 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
24、 N08811,and N06674, one test 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
25、point midway between the inner and outer surfacesof the wall of hollow forgings, and shall be parallel to thedirection of greatest metal flow.10.3 The specimens shall be the largest possible round typeshown in Test Methods E8.11. Test Methods11.1 The chemical composition, mechanical, and otherproper
26、ties 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 E8Rounding Procedure E29Grain Size E11211.2 The measurement of average grain size may be carrie
27、dout 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 planimetric method.11.3 For purposes of determining compliance with thespecified limits for requirement
28、s 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 Unit for Observed orCalculated ValueChemical composition nearest unit in the last right-hand placeof
29、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 than 0.0024 in. (0.060 mm) nearest multiple of 0.0001 in. (0.002 mm)12. Inspection12.1 Inspection of
30、 the material by the purchaser shall bemade as agreed upon between the purchaser and the seller aspart of the purchase contract.5Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http:/www.dodssp.daps.mil.B564 112TABLE 1 Ch
31、emical RequirementsAComposition, %ElementNickelAlloyNickel-CopperAlloyLow-CarbonNickel-Molybdenum-ChromiumAlloyNickel-Chromium-Iron-AluminumAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyNickel-Chromium-Iron-SiliconAlloyLow-CarbonNickel-Chromium-MolybdenumAlloyLow-CarbonNickel-Chromium-MolybdenumAllo
32、yNickel-Chromium-Molybdenum-TungstenAlloyUNSN02200UNSN04400UNSN06022UNSN06025UNSN06035UNSN06045UNSN06058UNSN06059UNSN06110Nickel 99.0Bmin 63.0Bmin balanceBbalance balanceB45 min balance balanceB51.0BminCopper 0.25 28.034.0 . 0.10 0.30 0.3 0.50 0.50 0.50Iron 0.40 2.5 2.06.0 8.011.0 2.00 21.025.0 1.5
33、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 32.2534.25 26.029.0 20.023.0 22.024.0 28.0
34、33.0Aluminum . . . 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 . 19.0 - 21.0 15.016.5 9.012.0Phosphorus . . 0.02 0.02 0.030 0.02 0.015 0.015 0.50Tungsten . . 2.53.5 . 0.60 . 0.3 . 1.0-4.0Cobalt . . 2.5 . 1
35、.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 . . . . .Cerium . . . . . 0.030.09 . . .Yttrium .
36、. . 0.050.12 . . . . .AMaximum 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.BElement shall be determined arithmetically by difference.B564 113TABLE 1 Chemical RequirementsA(continued)Compos
37、ition, %ElementLow-CarbonNickel-Chromium-Molybdenum-CopperAlloyLow-CarbonNickel-Molybdenum-Chromium-TantalumAlloyNickel-Chromium-Molybdenum-SiliconAlloyNickelChromium-Tungsten-MolybdenumAlloyNickel-Chromium-Iron-AluminumAlloyNickelChromium-Cobalt-MolybdenumAlloyNickel-Chromium-Molybdenum-ColumbiumAl
38、loyNickel-Chromium-IronAlloyNickel-Iron-Chromium-TungstenAlloyUNSN06200UNSN06210UNSN06219UNSN06230UNSN06603UNSN06617UNSN06625UNSN06600UNSN06674Nickel balanceBbalanceBbalanceBbalanceBbalanceB44.5 min 58.0Bmin 72.0Bmin 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
39、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 0.200.40 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.
40、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 . 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 . 0.01
41、5 . 0.030Tungsten . . . 13.015.0 . . . . 6.0-8.0Cobalt 2.0 1.0 1.0 5.0 . 10.0 min15.0. . .Vanadium . 0.35 . . . . . . .Nitrogen . . . . . . . . 0.02Boron . . . 0.015 . 0.006 . . 0.0005-0.006LanthanumAluminum +Titanium. . . 0.0050.050. .Nickel +Molybdenum. . . . . . . . .Columbium(Nb). . . . . . . .
42、0.10-0.35Tantalum . 1.5-2.2 . . . . . . .Zirconium . . . . 0.010.10 . . . .Cerium . . . . . . . . .Yttrium . . . . 0.010.15 . . . .AMaximum 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.BEle
43、ment shall be determined arithmetically by difference.B564 114TABLE 1 Chemical RequirementsA(continued)Composition, %ElementLow-CarbonNickel-Chromium-Molybdenum-TungstenAlloyNickel-Chromium-IronAlloyLow-CarbonNickel-Iron-Chromium-Molybdenum-CopperAlloyNickel-Iron-ChromiumAlloyIron-Nickel-Chromium-Mo
44、lybdenum-NitrogenAlloyNickel-Iron-ChromiumAlloyNickel-Iron-ChromiumAlloyNickel-Iron-ChromiumAlloyNickel-Iron-Chromium-Molybdenum-CopperAlloyUNSN06686UNSN06690UNSN08031UNSN08120UNSN08367UNSN08800UNSN08810UNSN08811UNSN08825Nickel remainder 58.0Bmin 30.032.0 35.039.0 23.5025.50 30.035.0 30.035.0 30.035
45、.0 38.046.0Copper . 0.5 1.01.4 0.50 0.75 0.75 0.75 0.75 1.53.0Iron 5.0 7.011.0 balanceBbalance balanceB39.5Bmin 39.5Bmin 39.5Bmin 22.0BminManganese 0.75 0.5 2.0 1.5 2.00 1.5 1.5 1.5 1.0Carbon 0.010 0.05 0.015 0.020.10 0.030 0.10 0.050.10 0.060.10 0.05Silicon 0.08 0.5 0.3 1.0 1.00 1.0 1.0 1.0 0.5Sulf
46、ur 0.02 0.015 0.010 0.03 0.030 0.015 0.015 0.015 0.03Chromium 19.023.0 27.031.0 26.0-28.0 23.027.0 20.022.0 19.023.0 19.023.0 19.023.0 19.523.5Aluminum . . . 0.40 . 0.150.60 0.150.60 0.150.60 0.2Titanium 0.020.25 . . 0.20 . 0.150.60 0.150.60 0.150.60 0.61.2Columbium(Nb) +Tantalum. . . 0.40.9 . . . .
47、 .Molybdenum 15.017.0 . 6.0-7.0 2.50 6.007.00 . . . 2.53.5Phosphorus 0.04 . 0.020 0.040 0.040 . . . .Tungsten 3.04.4 . . 2.50 . . . . .Cobalt . . . 3.0 . . . . .Vanadium . . . . . . . . .Nitrogen . . 0.15-0.25 0.150.30 0.180.25 . . . .Boron . . . 0.010 . . . . .LanthanumAluminum +Titanium. .0.851.20
48、.Nickel +Molybdenum. . . . . . . . .Columbium(Nb). . . . . . . . .Tantalum . . . . . . . . .Zirconium . . . . . . . . .Cerium . . . . . . . . .Yttrium . . . . . . . . .AMaximum unless range or minimum is given. Where ellipses (.) appear in this table there is no requirement and the element need neit
49、her be analyzed for nor reported.BElement shall be determined arithmetically by difference.B564 115TABLE 1 Chemical RequirementsA(continued)Composition, %ElementNickel-Molybdenum-Chromium-IronAlloyLow-CarbonNickel-Molybdenum-ChromiumAlloyLow-CarbonNickel-Molybdenum-ChromiumAlloyNickel-Molybdenum-Chromium-IronAlloyNickel-MolybdenumAlloyNickel-MolybdenumAlloyNickel-MolybdenumAlloyNickel-Cobalt-Chromium-SiliconAlloyChromium-Nickel-Iron-Nit
