ASTM B564-2010 2500 Standard Specification for Nickel Alloy Forgings《镍合金锻件标准规格》.pdf

1、Designation: B564 10Standard 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 nickel alloy UNSN02200, Ni-Cu alloy UNS N04

3、400, Ni-Cr-Fe alloys UNSN06600, UNS N06603, and UNS N06690, Ni-Cr-Mo-Nb alloyUNS N06625, Ni-Cr-Mo-Si alloy UNS N06219, low-carbonNi-Mo-Cr alloys UNS N10276 and UNS N06022, Ni-Cr-Mo-W alloy UNS N06110, low-carbon Ni-Cr-Mo-W alloyUNS N06686, Ni-Fe-Cr-Mo-Cu alloy UNS N08825, Fe-Ni-Cr-Mo-N alloy UNS N08

4、367, low-carbon Ni-Cr-Mo alloys UNSN06035, UNS N06058, and UNS N06059, low carbon Ni-Cr-Mo-Cu alloy UNS N06200, low-carbon Ni-Mo-Cr alloy UNSN10362, Ni-Mo-Cr-Fe alloy UNS N10242, Ni-Mo alloys UNSN10665 and UNS N10675, low-carbon Ni-Fe-Cr-Mo-Cu alloyUNS N08031, Ni-Cr-W-Mo alloy UNS N06230, Ni-Cr-Co-M

5、oalloy UNS N06617, Ni-Co-Cr-Si alloy UNS N12160, Ni-Fe-Cralloys, Ni-Mo alloy UNS N10629, Ni-Cr-Fe-Al alloy UNSN06025, Ni-Cr-Fe-Si alloy UNS N06045, Low-Carbon Ni-Mo-Cr-Ta alloy UNS N06210, Ni-Mo-Cr-Fe alloy UNSN10624, and low-carbon Cr-Ni-Fe-N alloy UNS R20033*.1.1.1 The nickel-iron-chromium alloys

6、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 where resistance to creep and rupture isrequired, a

7、nd are annealed to develop controlled grain size foroptimum properties in this temperature range.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 consider

8、ed standard.1.3 This standard 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 appropriateMaterial Safety Data Sheet (MSDS) for this produc

9、t/materialas provided by the manufacturer, to establish appropriatesafety 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, N

10、ickel Alloys andCobalt AlloysE8 Test Methods for Tension Testing 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 SizeE3

11、50 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,Cobalt, and High-Temperature Alloys2.2 Military Standards:5MIL-STD-129 Marking for Shipment and StorageMIL-STD-271 Nondestruc

12、tive Testing Requirements forMetals3. Ordering Information3.1 It is the responsibility of the purchaser to specify allrequirements that are necessary for material ordered under thisspecification. Examples of such requirements include, but arenot limited to, the following:3.1.1 Alloy (Table 1).1This

13、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 Their Alloys.Current edition approved Oct. 1, 2010. Published October 2010. Originallyapproved in 1972. Last previous e

14、dition approved in 2006 as B564 06A. DOI:10.1520/B0564-10.2For ASME Boiler and Pressure Vessel Code applications see related Specifi-cation SB-564 in Section II of that Code.* New designations established in accordance withASTM E527 and SAE J1086,Practice for Numbering Metals and Alloys (UNS).3For r

15、eferenced 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 standards Document Summary page onthe ASTM website.4Withdrawn. The last approved version of this historical standard i

16、s referencedon www.astm.org.5Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http:/www.dodssp.daps.mil.1*A Summary of Changes section appears at the end of this standard.Copyright ASTM International, 100 Barr Harbor Drive

17、, PO Box C700, West Conshohocken, PA 19428-2959, United States.TABLE 1 Chemical RequirementsComposition, %ElementNickel-CopperAlloyNickel-Chromium-Iron AlloyNickel-Chromium-Iron AlloyNickel-IronChromiumAlloyNickel-Iron-ChromiumAlloyNickel-Iron-ChromiumAlloyNickel-Chromium-Iron-AluminumAlloyNickel-Ch

18、romium-Iron-AluminumAlloyNickel-Chromium-Iron-SiliconAlloyLow-CarbonNickel-Molybdenum-Chromium-TantalumAlloyUNSN04400UNSN06600UNSN06690UNSN08120UNSN08800UNSN08810UNSN06603UNSN06025UNSN06045UNSN06210Nickel 63.0Amin 72.0Amin 58.0 minA35.039.0 30.035.0 30.035.0 balanceAbalance 45 min remainderACopper 2

19、8.034.0 0.5 max 0.5 max 0.50 max 0.75 max 0.75 max 0.5 max 0.10 max 0.3 max .Iron 2.5 max 6.010.0 7.011.0 remainder 39.5 minA39.5 minA8.011.0 8.011.0 21.025.0 1.0 maxManganese 2.0 max 1.0 max 0.5 max 1.5 1.5 max 1.5 max 0.15 max 0.15 1.0 0.5 maxCarbon 0.3 max 0.15 max 0.05 max 0.020.10 0.10 max 0.05

20、0.10 0.200.40 0.150.25 0.050.12 0.015 maxSilicon 0.5 max 0.5 max 0.5 max 1.0 1.0 max 1.0 max 0.5 max 0.5 2.53.0 0.08 maxSulfur, max 0.024 0.015 0.015 0.03 0.015 0.015 0.010 0.01 0.010 0.02Chromium . 14.017.0 27.031.0 23.027.0 19.023.0 19.023.0 24.026.0 24.026.0 26.029.0 18.0-20.0Aluminum . . . 0.40

21、max 0.150.60 0.150.60 2.43.0 1.82.4 . .Titanium . . . 0.20 max 0.150.60 0.150.60 0.010.25 0.10.2 . .Columbium(Nb) +tantalum. . . 0.40.9 . . . . . .Molybdenum . . . 2.50 max . . . . . 18.0-20.0Phosphorus . . . 0.040 max . . 0.02 max 0.02 max 0.02 max 0.02 maxTungsten . . . 2.50 max . . . . . .Cobalt,

22、 max . . . 3.0 . . . . . 1.0Vanadium,max. . . . . . . . . 0.35Nitrogen . . . 0.150.30 . . . . . .Boron . . . 0.010 max . . . . . .LanthanumAluminum +Titanium. .Nickel +Molybdenum. . . . . . . . . .Columbium(Nb) max. . . . . . . . . .Tantalum . . . . . . . . . 1.5-2.2Zirconium, max . . . . . . 0.010.

23、10 0.010.10 . .Cerium . . . . . . . . 0.030.09 .Yttrium . . . . . . 0.010.15 0.050.12 . .AElement shall be determined arithmetically by difference.B564 102TABLE 1 Chemical Requirements (continued)Composition, %ElementNickel-Iron-ChromiumAlloyNickel-Chromium-Molybdenum-ColumbiumAlloyNickel-Chromium-M

24、olybdenum-TungstenAlloyNickel-IronChromium-Molybdenum-Copper AlloyLow-CarbonNickel-Molyb-denum-ChromiumAlloyLow-CarbonNickel-Molyb-denum-Chro-miumAlloyIron-Nickel-Chromium-Molyb-denum-NitrogenAlloyLow-CarbonNickel-ChromiumMolyb-denumAlloyLow-CarbonNickel-ChromiumMolyb-denumAlloyUNSN08811UNSN06625UNS

25、N06110UNSN08825UNSN10276UNSN06022UNSN08367UNSN06059UNSN06058Nickel 30.035.0 58.0 minA51.0 minA38.046.0 remainderAremainderA23.5025.50 balanceAbalanceCopper 0.75 max . 0.50 max 1.53.0 . . 0.75 max 0.50 max 0.50 maxIron 39.5 minA5.0 max 1.0 max 22.0 minA4.07.0 2.06.0 remainderA1.5 max 1.5 maxManganese

26、 1.5 max 0.5 max 1.0 max 1.0 max 1.0 max 0.50 max 2.00 max 0.5 max 0.50 maxCarbon 0.060.10 0.10 max 0.15 max 0.05 max 0.010 max 0.015 max 0.030 max 0.010 max 0.010 maxSilicon 1.0 max 0.5 max 1.0 max 0.5 max 0.08 max 0.08 max 1.00 max 0.10 max 0.10 maxSulfur, max 0.015 0.015 0.015 0.03 0.03 0.02 0.03

27、0 0.010 0.010Chromium 19.023.0 20.023.0 28.033.0 19.523.5 14.516.5 20.022.5 20.022.0 22.024.0 20.023.0Aluminum 0.150.60 0.4 max 1.0 max 0.2 max . . . 0.10.4 0.40 maxTitanium 0.150.60 0.4 max 1.0 max 0.61.2 . . . . .Columbium(Nb) +tantalum. 3.154.15 1.0 max . . . . . .Molybdenum . 8.010.0 9.012.0 2.5

28、3.5 15.017.0 12.514.5 6.007.00 15.016.5 19.0 - 21.0Phosphorus . 0.015 max 0.50 max . 0.04 max 0.02 max 0.040 max 0.015 max 0.015 maxTungsten . . 1.0-4.0 . 3.04.5 2.53.5 . . 0.3 maxCobalt . . . . 2.5 max 2.5 max . 0.3 max 0.3 maxVanadium,max. . . . 0.35 0.35 . . .Nitrogen . . . . . . 0.180.25 . 0.02

29、- 0.15Boron . . . . . . . . .LanthanumAluminum +Titanium.0.851.20.Nickel +Molybdenum. . . . . . . . .Columbium(Nb), max. . . . . . . . .Tantalum . . . . . . . . .Zirconium,max. . . . . . . . .Cerium . . . . . . . . .Yttrium . . . . . . . . .AElement shall be determined arithmetically by difference.B

30、564 103TABLE 1 Chemical Requirements (continued)Composition, %ElementLow-CarbonNickel-Chromium-MolybdenumAlloyLow-CarbonNickel-Chromium-Molyb-dnum-CopperAlloyLow-CarbonNickel-Molybdenum-ChromiumNickel-Chromium-Molyb-dnum-SiliconAlloyLow-CarbonNickel-IronChromium-Molyb-dnum-CopperAlloyNickelChro-mium

31、-Tungsten-Molyb-denumAlloyNickelChromium-Cobalt-Molyb-denumAlloyNickel-Molyb-denumAlloyUNS UNSUNSN06035UNSN06200UNSN10362UNSN06219UNSN08031UNSN06230UNSN06617UNSN10629Nickel remainderAremainderBremainderBbalanceB30.032.0 remainderA44.5 min balanceCopper 0.30 max 1.31.9 . 0.50 max 1.01.4 . 0.5 max 0.5

32、 maxIron 2.00 max 3.0 max 1.25 max 2.0-4.0 balanceB3.0 max 3.0 max 1.06.0Manganese 0.50 max 0.50 max 0.60 max 0.50 max 2.0 max 0.301.00 1.0 max 1.5Carbon 0.050 max 0.010 max 0.010 max 0.05 max 0.015 max 0.050.15 0.050.15 0.010 maxSilicon 0.60 max 0.08 max 0.08 max 0.70-1.10 0.3 max 0.250.75 1.0 max

33、0.05Sulfur, max 0.015 0.010 0.010 0.010 0.010 0.015 0.015 0.01Chromium 32.2534.25 22.024.0 13.8-15.6 18.0-22.0 26.0-28.0 20.024.0 20.024.0 0.51.5Aluminum 0.40 max 0.50 max 0.50 max 0.50 max . 0.50 max 0.81.5 0.10.5Titanium . . . 0.50 max . . 0.6 max .Columbium(Nb) +tantalum. . . . . . . .Molybdenum

34、7.609.00 15.017.0 21.5-23.0 7.0-9.0 6.0-7.0 1.03.0 8.010.0 26.030.0Phosphorus 0.030 max 0.025 max 0.025 max 0.020 max 0.020 max 0.030 max . 0.04 maxTungsten 0.60 max . . . . 13.015.0 . .Cobalt 1.00 max 2.0 max . 1.0 max . 5.0 max 10.0 min15.0 max2.5Vanadium,max0.20 . . . . . . .Nitrogen . . . . 0.15

35、-0.25 . . .Boron . . . . . 0.015 max 0.006 max .LanthanumAluminum +Titanium. . . . . 0.0050.050.Nickel +Molybdenum. . . . . . . .Columbium(Nb), max. . . . . . . .Tantalum . . . . . . . .Zirconium,max. . . . . . . .Cerium . . . . . . . .Yttrium . . . . . . . .BElement shall be determined arithmetical

36、ly by difference.B564 104TABLE 1 Chemical Requirements (continued)Composition, %ElementNickel-Molyb-denumAlloyNickel-Molyb-denumAlloyNickel-Molyb-denum-Chromium-Iron AlloyLow-CarbonNickel-Chro-mium-Molyb-denum-TungstenAlloyNickel-Cobalt-Chro-mium-SiliconAlloyNickelAlloyNickel-Molyb-denumChro-mium-Ir

37、onAlloyChromium-Nickel-Iron-NitrogenAlloyUNSN10665UNSN10675UNSN10242UNSN06686UNSN12160UNSN02200UNSN10624UNSR00033Nickel remainderA65.0 min remainderAremainder remainderA99.0Amin remainderA30.033.0Copper . 0.20 max . . . 0.25 max 0.5 max 0.301.20Iron 2.0 max 1.03.0 2.0 max 5.0 max 3.5 max 0.40 max 5.

38、0-8.0 balanceAManganese 1.0 max 3.0 max 0.80 max 0.75 max 1.5 max 0.35 max 1.0 max 2.0Carbon 0.02 max 0.01 max 0.03 0.010 max 0.15 max 0.15 max 0.01 max 0.015 maxSilicon 0.10 max 0.10 max 0.80 max 0.08 max 2.43.0 0.35 max 0.10 max 0.50Sulfur, max 0.03 0.010 0.015 0.02 0.015 0.01 0.01 max 0.01Chromiu

39、m 1.0 max 1.03.0 7.0-9.0 19.023.0 26.030.0 . 6.0-10.0 31.035.0Aluminum . 0.50 max 0.50 max . . . 0.5 max .Titanium . 0.20 max . 0.020.25 0.200.80 . . .Columbium(Nb) +tantalum. . . . . . . .Molybdenum 26.030.0 27.032.0 24.0-26.0 15.017.0 1.0 max . 21.0-25.0 0.502.0Phosphorus 0.04 max 0.030 max 0.030

40、max 0.04 max 0.030 max . 0.025 max 0.02 maxTungsten . 3.0 max . 3.04.4 1.0 max . . .Cobalt 1.00 max 3.0 max1.00 max . 27.033.0 . 1.0 max .Vanadium,max. 0.20 . . . . . .Nitrogen . . . . . . . 0.350.60Boron . . 0.006 max . . . . .LanthanumAluminum +Titanium. . .Nickel +Molybdenum. 94.098.0 . . . . . .

41、Columbium(Nb), max. 0.20 . . 1.0 . . .Tantalum . 0.20 max . . . . . .Zirconium,max. 0.10 . . . . . .Cerium . . . . . . . .Yttrium . . . . . . . .AElement shall be determined arithmetically by difference.B564 1053.1.2 Condition (Table 2).3.1.3 Quantity (mass or number of pieces).3.1.4 Forging, sketch

42、 or drawing.3.1.5 CertificationState if certification or a report 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 ma

43、terial at the place of manu-facture, the purchase order must so state 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, th

44、e material shall conform to the product (check)analysis variations 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, N081

45、20,and UNS N08811) shall conform to an average grain size ofASTM No. 5 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 a

46、nd 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,condition, and processed at one

47、 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 material to provide test

48、 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, and UNSN08811, one test pe

49、r 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 inner and outer surfacesof the wall of hollow forgings, and shall be parallel to thedirection of greatest metal flow