1、Designation: B619/B619M 17B619/B619M 17aStandard Specification forWelded Nickel and Nickel-Cobalt Alloy Pipe1This standard is issued under the fixed designation B619/B619M; the number immediately following the designation indicates the yearof original adoption or, in the case of revision, the year o
2、f last revision. A number in parentheses indicates the year of last reapproval.A superscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope*1.1 This specification2 covers welded pipe of nickel and nickel-cobalt alloys (UNS N10001; UNS N10242; UNS N10665; UNSN
3、12160; UNS N10624; UNS N10629; UNS N10675; UNS N10276; UNS N06455; UNS N06007; UNS N06975; UNS N08320;UNS N06002; UNS N06022; UNS N06035; UNS N06044; UNS N06058; UNS N06059; UNS N06200; UNS N10362; UNSN06985; UNS N06030; UNS R30556; UNS N08031; UNS N08034; UNS N06230; UNS N06686; UNS N06210; and UNS
4、R20033)3 as shown in Table 1.1.2 This specification covers pipe in Schedules 5S, 10S, 40S, and 80S through 8-in. nominal pipe size and larger as set forthin ANSI B36.19 (see Table 2).1.3 Two classes of pipe are covered as follows:1.3.1 Class IAs welded and solution annealed or welded and sized and s
5、olution annealed.1.3.2 Class IIWelded, cold worked, and solution annealed.1.4 All pipe shall be furnished in the solution annealed and descaled condition. When atmosphere control is used, descaling isnot necessary.1.5 The values stated in either SI units or inch-pound units are to be regarded separa
6、tely as standard. The values stated in eachsystem may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from thetwo systems may result in non-conformance with the standard.1.6 This standard does not purport to address all of the safety concer
7、ns, 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/material as provided by the manufacturer, to establish appropriate safety safety, health
8、 and healthenvi-ronmental practices, and determine the applicability of regulatory limitations prior to use.1.7 This international standard was developed in accordance with internationally recognized principles on standardizationestablished in the Decision on Principles for the Development of Intern
9、ational Standards, Guides and Recommendations issuedby the World Trade Organization Technical Barriers to Trade (TBT) Committee.2. Referenced Documents2.1 ASTM Standards:4B775 Specification for General Requirements for Nickel and Nickel Alloy Welded PipeB899 Terminology Relating to Non-ferrous Metal
10、s and AlloysE527 Practice for Numbering Metals and Alloys in the Unified Numbering System (UNS)2.2 ANSI Standards:5B36.19 Stainless Steel PipeB2.1 Pipe Threads2.3 ASME Boiler and Pressure Vessel Code6Section IX Welding and Brazing Qualifications1 This specification is under the jurisdiction ofASTM C
11、ommittee B02 on Nonferrous Metals andAlloys and is the direct responsibility of Subcommittee B02.07 on RefinedNickel and Cobalt and Their Alloys.Current edition approved June 1, 2017July 1, 2017. Published June 2017August 2017. Originally approved in 1981. Last previous edition approved in 20152017
12、asB619/B619M 15.B619/B619M 17. DOI: 10.1520/B0619_B0619M-17.10.1520/B0619_B0619M-17a.2 For ASME Boiler and Pressure Vessel Code applications see related Specification SB-619 in Section II of that Code.3 New designation established in accordance with Practice E527 and SAE J1086, Practice for Numberin
13、g Metals and Alloys (UNS).4 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page on the ASTM website.5 Available from American National
14、Standards Institute (ANSI), 25 W. 43rd St., 4th Floor, New York, NY 10036, http:/www.ansi.org.6 Available from American Society of Mechanical Engineers (ASME), ASME International Headquarters, Three Park Ave., New York, NY 10016-5990, http:/www.asme.org.This document is not an ASTM standard and is i
15、ntended only to 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 cu
16、rrent versionof 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 States1TABLE 1 Chemical Requirements
17、Composition Limits, %Ni Cr Mo Fe W C Simax Co Mn V Pmax Smax Ti CuCb(Nb)+TaAl Zr La N B Cb(Nb) Ta Ni+Mo MgNi-Mo AlloysN10001 remainderA 1.0max26.0-30.04.0-6.0 . 0.05max1.0 2.5max1.0max0.2-0.40.04 0.03 . . .N10665 remainderA 1.0max26.0-30.02.0 max . 0.02max0.10 1.0max1.0max. 0.04 0.03 . . .N10675 65.
18、0 min 1.0-3.027.0-32.01.0-3.0 3.0max0.01max0.10 3.0max3.0max0.20max0.030 0.010 0.20max0.20max. 0.50max0.10max. . . 0.20max0.20max94.0-98.0N10629 remainderA 0.5-1.526.0-30.01.0-6.0 . 0.01max0.05 2.5max1.5max. 0.04 0.01 . 0.5max. 0.1-0.5. . . . . . .N10624 remainderA 6.0-10.021.0-25.05.0-8.0 . 0.01max
19、0.10 1.0max1.0max. 0.025 0.01 . 0.5max. . . . . . . . .Ni-Mo-Cr-FeAlloyN10242 remainderA 7.0-9.024.0-26.02.0 max 0.03max0.80 1.00max0.80max0.030 0.015 0.50max0.50max0.006maxLow C Ni-Cr-Mo AlloysN10276 remainderA 14.5-16.515.0-17.04.0-7.0 3.0-4.50.010max0.08 2.5max1.0max0.35max0.04 0.03 . . .N06022 r
20、emainderA 20.0-22.512.5-14.52.0-6.0 2.5-3.50.015max0.08 2.5max0.5max0.35max0.02 0.02 . . .N06035 remainderA 32.25-34.257.60-9.002.00 max 0.60max0.050max0.60 1.00max0.50max0.20max0.030 0.015 . 0.30max. 0.40maxN06044 balance 43.5-45.30.80-1.20 0.3 max. 0.02max 0.20. 0.07-0.30. 0.020 0.020 0.10-0.30. .
21、 0.30max. . . . . . . .N06058 balance 20.0-23.018.5-21.01.5 max 0.3max0.010max0.10max0.3max0.50max0.015 0.010 . 0.50max. 0.40max0.02-0.15N06059 balance 22.0-24.015.0-16.51.5 max . 0.010max0.10 0.3max0.5max. 0.015 0.010 . 0.50max. 0.1-0.4. . . . . . .N06455 remainderA 14.0-18.014.0-17.03.0 max . 0.01
22、5max0.08 2.0max1.0max. 0.04 0.03 0.70max. .Ni-Cr-Fe-Mo-CuAlloysN06007 remainderA 21.0-23.55.5-7.518.0-21.0 1.0max0.05max1.0 2.5max1.0-2.0. 0.04 0.03 . 1.5-2.51.75-2.5N06975 47.0-52.0 23.0-26.05.0-7.0remainder . 0.03max1.0 . 1.0max. 0.03 0.03 0.70-1.500.70-1.20.N06985 remainderA 21.0-23.56.0-8.018.0-
23、21.0 1.5max0.015max1.0max5.0max1.0max. 0.04 0.03 . 1.5-2.50.50maxN06030 remainderA 28.0-31.54.0-6.013.0-17.0 1.5-4.00.03max0.8 5.0max1.5max. 0.04 0.02 . 1.0-2.40.30-1.50Ni-Fe-Cr-MoAlloysN08320 25.0-27.0 21.0-23.04.0-6.0remainder . 0.05max1.0 . 2.5max. 0.04 0.03 4xCmin. .Ni-Cr-Mo-FeAlloyN06002 remain
24、derA 20.5-23.08.0-10.017.0-20.0 0.20-1.00.05-0.151.0 0.5-2.51.0max. 0.04 0.03 . . .Ni-Fe-Cr-CoAlloyR30556 19.0-22.5 21.0-23.02.5-4.0remainder 2.0-3.50.05-0.150.20-0.8016.0-21.00.50-2.00. 0.04 0.015 . . . 0.10-0.500.001-0.100.005-0.100.10-0.300.02max0.30max0.3-1.25B619/B619M17a2TABLE 1 ContinuedCompo
25、sition Limits, %Ni Cr Mo Fe W C Simax Co Mn V Pmax Smax Ti CuCb(Nb)+TaAl Zr La N B Cb(Nb) Ta Ni+Mo MgNi-Cr-W-MoAlloyN06230 remainderA 20.0-24.01.0-3.03.0 max 13.0-15.00.05-0.150.25-0.755.0max0.30-1.00. 0.03 0.015 . . . 0.50max. 0.005-0.050. 0.015max. .Low C-Ni-Cr-Mo-CuAlloyN06200 remainderA 22.0-24.
26、015.0-17.03.0 max . 0.010max0.08 2.0max0.50max. 0.025 0.010 . 1.3-1.9. 0.50maxLow-C-Ni-Mo-Cr AlloyN10362 remainderA 13.8-15.621.5-23.01.25 max . 0.010max0.08 . 0.60max. 0.025 0.010 . . . 0.50max. . . . . . . .Low C-Ni-Fe-Cr-Mo-Cu AlloyN08031 30.0-32.0 26.0-28.06.0-7.0balance . 0.015max0.3 . 2.0max.
27、0.020 0.010 . 1.0-1.4. . . . 0.15-0.25. . .N08034 33.5-35.0 26.0-27.06.0-7.0balance . 0.01max0.1 . 1.0-4.0. 0.020 0.010 . 0.5-1.5. 0.3max. . 0.10-0.25. . . . .Low C-Ni-Cr-Mo-WAlloyN06686 remainderA 19.0-23.015.0-17.05.0 max 3.0-4.40.010max0.08 . 0.75max. 0.04 0.02 0.02-0.25. . . . . . . . .Ni-Co-Cr-
28、SiAlloyN12160 remainderA 26.0-30.01.0max3.5 max 1.0max0.15max2.4-3.027.0-33.01.5max. 0.030 0.015 0.20-0.80. . . . . . . 1.0max. . .Cr-Ni-Fe-NAlloyR20033 30.0-33.0 31.0-35.00.50-2.0balance . 0.015max0.50 . 2.0max. 0.02 0.01 . 0.3-1.20. . . . 0.35-0.60. . . . .Low C-Ni-Mo-Cr-TaAlloyN06210 remainderA 1
29、8.0-20.018.0-20.01.0 max . 0.015max0.08 1.0max0.5 0.35max0.02 0.02 . . . . . . . 1.5-2.2A The composition of the remainder shall be determined arithmetically by difference.B619/B619M17a33. Terminology3.1 For definitions of terms used in this standard refer to Terminology B899.4. General Requirement4
30、.1 Material furnished under this specification shall conform to the applicable requirements of Specification B775 unlessotherwise provided herein.5. Ordering Information5.1 It is the responsibility of the purchaser to specify all requirements that are necessary for material ordered under thisspecifi
31、cation. Examples of such requirements include, but are not limited to the following:5.1.1 Alloy (Table 1),5.1.2 Class (see 1.3),5.1.3 Quantity (feet or number of lengths),5.1.4 Size (nominal size or outside diameter and schedule number or average wall thickness),5.1.5 LengthSpecify cut length or ran
32、dom,5.1.6 CertificationState if certification or a report of test results is required,5.1.7 Purchaser InspectionState which tests or inspections are to be witnessed,5.1.8 EndsPlain ends cut and deburred will be furnished, unless otherwise specified, and5.1.9 Samples for Product (Check) AnalysisState
33、 whether samples shall be furnished.6. Materials and Manufacture6.1 The pipe shall be made from flat-rolled alloy by an automatic welding process with no addition of filler metal.6.2 Subsequent to welding and prior to final heat treatment, Class II pipes shall be cold worked either in both weld and
34、basemetal or in weld metal only. The method of cold working may be specified by the purchaser.7. Chemical Composition7.1 The material shall conform to the composition limits specified in Table 1.7.2 If a product (check) analysis is made by the purchaser, the material shall conform to the requirement
35、s specified in Table 1subject to the permissible tolerances in Specification B775.8. Mechanical Properties and Other Requirements8.1 Tension TestThe tensile properties of the material at room temperature shall conform to those shown in Table 3.8.1.1 One tension test shall be made on each lot of pipe
36、.8.2 Flattening TestOne flattening test shall be made on a specimen from one end of one pipe from each lot.TABLE 2 Dimensions of Welded PipeNOTE 1The following table is a partial reprint of Table 1 of ANSI B36.19.NOTE 2The decimal thickness listed for the respective pipe sizes represents their nomin
37、al or average wall dimensions.NominalPipe Size, Outside DiameterNominal Wall ThicknessSchedule 5SA Schedule 10SA Schedule 40S Schedule 80Sin. in. mm in. mm in. mm in. mm in. mm18 0.405 10.29 . . 0.049 1.24 0.068 1.7314 0.540 13.72 . . 0.065 1.65 0.088 2.2438 0.675 17.15 . . 0.065 1.65 0.091 2.3112 0
38、.840 21.34 0.065 1.65 0.083 2.11 0.109 2.7734 1.050 26.67 0.065 1.65 0.083 2.11 0.113 2.871.0 1.315 33.41 0.065 1.65 0.109 2.77 0.133 3.38114 1.660 42.16 0.065 1.65 0.109 2.77 0.140 3.56112 1.900 48.26 0.065 1.65 0.109 2.77 0.145 3.682 2.375 60.33 0.065 1.65 0.109 2.77 0.154 3.91 0.218 5.54212 2.875
39、 73.03 0.083 2.11 0.120 3.05 0.203 5.16 0.276 7.013 3.500 88.90 0.083 2.11 0.120 3.05 0.216 5.33312 4.000 101.60 0.083 2.11 0.120 3.05 0.226 5.744 4.500 114.30 0.083 2.11 0.120 3.05 0.237 6.025 5.563 141.30 0.109 2.77 0.134 3.40 0.258 6.556 6.625 168.28 0.109 2.77 0.134 3.40 0.280 7.118 8.625 219.18
40、 0.109 2.77 0.148 3.76 0.322 8.18A Schedules 5S and 10S wall thicknesses do not permit threading in accordance with ANSI B2.1-1960.B619/B619M 17a4TABLE 3 Mechanical Properties of PipeAlloy Tensile Strength,min, ksi MPaYield Strength(0.2 % Offset),min, ksi MPaElongationin 2 in.50.8 mmor 4D,Amin, %Ni-
41、Mo Alloysalloy N10001 100 690 45 310 40alloy N10665 110 760 51 350 40alloy N10675 110 760 51 350 40alloy N10629 110 760 51 350 40alloy N10624 104 720 46 320 40Ni-Mo-Cr-Fe Alloyalloy N10242 105 725 45 310 40Low C Ni-Cr-Mo Alloysalloy N10276 100 690 41 283 40alloy N06022 100 690 45 310 45alloy N06035
42、85 586 35 241 30alloy N06044 90 620 45 310 20alloy N06455 100 690 40 276 40Ni-Cr-Fe-Mo-Cu Alloysalloy N06007 90 621 35 241 35alloy N06975 85 586 32 221 40alloy N06985 90 621 35 241 45alloy N06030 85 586 35 241 30Ni-Fe-Cr-Mo Alloy (N08320) 75 517 28 193 35Ni-Cr-Mo-Fe Alloy (N06002) 100 690 40 276 35N
43、i-Fe-Cr-Co Alloy (R30556) 100 690 45 310 40Ni-Cr-W-Mo Alloy (N06230)B 110 760 45 310 40Low C-Ni-Cr-Mo Alloysalloy N06058 110 760 52 360 40alloy N06059 100 690 45 310 45Low C-Ni-Cr-Mo-Cu Alloy(N06200)100 690 45 310 45Low C-Ni-Mo-Cr Alloy(N10362)105 725 45 310 40Ni-Fe-Cr-Mo-Cu Low CarbonAlloy (N08031)
44、 94 65040 276 40Alloy (N08034) 94 650 40 280 40Low C Ni-Cr-Mo-W Alloy(N06686)100 690 45 310 45Ni-Co-Cr-Si alloy (N12160) 90 620 35 240 40Cr-Ni-Fe-N Low Carbon Alloy(R20033) 109 75055 380 40Low C Ni-Cr-Mo-Ta Alloy(N06210) 100 69045 310 45A D refers to the diameter of the tension specimen.B Solution a
45、nnealed at a temperature between 2200 to 2275F 1204 to 1246Cfollowed by a water quench or rapidly cooled by other means.TABLE 4 Permissible Variations in Outside DiameterNominalPipe Size, in.Permissible Variation in Outside DiameterAin. mm18 10.29 +0.002 0.006 +0.05 0.1514 13.72 +0.003 0.008 +0.08 0
46、.2038 17.15 +0.004 0.008 +0.08 0.2012 21.34 +0.004 0.010 +0.10 0.2534 26.67 +0.005 0.012 +0.13 0.301 33.41 +0.005 0.012 +0.13 0.30114 42.16 +0.005 0.012 +0.13 0.30112 48.26 +0.008 0.015 +0.20 0.382 60.22 +0.010 0.016 +0.25 0.41212 73.03 +0.010 0.016 +0.25 0.413 88.90 +0.012 0.018 +0.30 0.46312 101.6
47、0 +0.012 0.018 +0.30 0.464 114.30 +0.014 0.020 +0.36 0.515 141.30 +0.063 0.031 +1.60 0.796 168.28 +0.063 0.031 +1.60 0.798 219.18 +0.063 0.031 +1.60 0.79A The permissible variations in the above table apply to individual measurements,including out of roundness (ovality).B619/B619M 17a58.3 Transverse
48、 Guided Bend Test:8.3.1 At the option of the pipe manufacturer, the transverse guided bend test may be substituted in lieu of the flattening test.Two bend specimens shall be taken transversely from pipe or the test specimens may be taken from a test plate of the same materialand heat as pipe, which
49、is attached to the end of the cylinder and welded as a prolongation of the pipe longitudinal seam. Exceptas provided in 8.3.2, one shall be subjected to a face guided bend and a second to a root guided bend test. One specimen shall bebent with the inside surface of the pipe against the plunger and the other with the outside surface of the pipe agains
