ASTM B210 B210M-2019 Standard Specification for Aluminum and Aluminum-Alloy Drawn Seamless Tubes.pdf

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1、Designation: B210/B210M 19 Used in USNRC-NDT standardsStandard Specification forAluminum and Aluminum-Alloy Drawn Seamless Tubes1This standard is issued under the fixed designation B210/B210M; the number immediately following the designation indicates the yearof original adoption or, in the case of

2、revision, the year of 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 specification2covers aluminum and aluminum-alloy drawn seamless tubes in straight lengths

3、and coils forgeneral purpose and pressure applications in alloys (Note 2),tempers, and thicknesses shown in Table 2 Table 3. Coiledtubes are generally available only as round tubes with a wallthickness not exceeding 0.083 in. 2.00 mm and only innon-heat-treatable alloys.1.2 Alloy and temper designat

4、ions are in accordance withANSI H35.1/H35.1M. The equivalent Unified NumberingSystem alloy designations are those of Table 1 preceded byA9,for example, A91100 for aluminum designation 1100 in accor-dance with Practice E527.NOTE 1See Specification B483/B483M for aluminum-alloy drawntubes for general

5、purpose applications; Specification B234 for aluminum-alloy drawn seamless tubes for condensers and heat exchangers; andSpecification B241/B241M for aluminum-alloy seamless pipe and seam-less extruded tube.NOTE 2Throughout this specification, use of the term alloy in thegeneral sense includes alumin

6、um as well as aluminum alloy.1.3 For acceptance criteria for inclusion of new aluminumand aluminum alloys in this specification, see Annex A2.1.4 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

7、 to establish appro-priate safety, health, and environmental practices and deter-mine the applicability of regulatory limitations prior to use.1.5 This international standard was developed in accor-dance with internationally recognized principles on standard-ization established in the Decision on Pr

8、inciples for theDevelopment of International Standards, Guides and Recom-mendations issued by the World Trade Organization TechnicalBarriers to Trade (TBT) Committee.2. Referenced Documents2.1 The following documents of the issue in effect on dateof material purchase form a part of this specificatio

9、n to theextent referenced herein:2.2 ASTM Standards:3B234 Specification for Aluminum and Aluminum-AlloyDrawn Seamless Tubes for Surface Condensers,Evaporators, and Heat ExchangersB241/B241M Specification for Aluminum and Aluminum-Alloy Seamless Pipe and Seamless Extruded TubeB483/B483M Specification

10、 for Aluminum and Aluminum-Alloy Drawn Tube and Drawn Pipe for General PurposeApplicationsB557 Test Methods for Tension Testing Wrought and CastAluminum- and Magnesium-Alloy ProductsB557M Test Methods for Tension Testing Wrought and CastAluminum- and Magnesium-Alloy Products (Metric)B660 Practices f

11、or Packaging/Packing of Aluminum andMagnesium ProductsB666/B666M Practice for Identification Marking of Alumi-num and Magnesium ProductsB807/B807M Practice for Extrusion Press Solution HeatTreatment for Aluminum AlloysB881 Terminology Relating to Aluminum- and Magnesium-Alloy ProductsB918/B918M Prac

12、tice for Heat Treatment of Wrought Alu-minum AlloysB985 Practice for Sampling Aluminum Ingots, Billets, Cast-ings and Finished or Semi-Finished Wrought AluminumProducts for Compositional AnalysisE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE215 Pr

13、actice for Standardizing Equipment and Electromag-netic Examination of Seamless Aluminum-Alloy TubeE527 Practice for Numbering Metals and Alloys in theUnified Numbering System (UNS)1This specification is under the jurisdiction of ASTM Committee B07 on LightMetals and Alloys and is the direct respons

14、ibility of Subcommittee B07.03 onAluminum Alloy Wrought Products.Current edition approved Jan. 1, 2019. Published February 2019. Originallyapproved in 1946. Last previous edition approved in 2012 as B210 12. DOI:10.1520/B0210_B0210M-19.2For ASME Boiler and Pressure Vessel Code applications see relat

15、ed Specifi-cation SB-210 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 the standards Document Summary page onthe ASTM website.*A Summar

16、y 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 StatesThis international standard was developed in accordance with internationally recognized principles on standardization established i

17、n the Decision on Principles for theDevelopment of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.1E607 Test Method for Atomic Emission SpectrometricAnalysis Aluminum Alloys by the Point to Plane Tech-nique Nitro

18、gen Atmosphere (Withdrawn 2011)4E716 Practices for Sampling and Sample Preparation ofAluminum and Aluminum Alloys for Determination ofChemical Composition by Spark Atomic Emission Spec-trometryE1004 Test Method for Determining Electrical ConductivityUsing the Electromagnetic (Eddy Current) MethodE12

19、51 Test Method for Analysis of Aluminum and Alumi-num Alloys by Spark Atomic Emission SpectrometryE3061 Test Method for Analysis of Aluminum and Alumi-numAlloys by Inductively Coupled PlasmaAtomic Emis-sion Spectrometry (Performance Based Method)2.3 ANSI Standards:5H35.1/H35.1M Alloy and Temper Desi

20、gnation Systems forAluminumH35.2 H35.2M Dimensional Tolerances for AluminumMill Products2.4 Military Standard:6MIL-STD-129 Marking for Shipment and Storage2.5 AMS Specification:7AMS 2772 Heat Treatment of Aluminum Alloy Raw Mate-rials2.6 Federal Standard:6Fed. Std. No. 123 Marking for Shipment (Civi

21、l Agencies)2.7 Other Standards8CEN EN 14242 Aluminum and Aluminum Alloys Chemi-cal Analysis Inductively Coupled Optical EmissionSpectral Analysis3. Terminology3.1 Definitions:4The last approved version of this historical standard is referenced onwww.astm.org.5Available fromTheAluminumAssociation, In

22、c., 1400 Crystal Drive, Suite 430,Arlington, VA 22202, http:/www.aluminum.org.6Available from Standardization Documents Order Desk, Bldg. 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5098.7Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001.8A

23、vailable from European Committee for Standardization, Central Secretariat(CEN), rue de Stassart 36, B1050 Brussels, Belgium. http:/www.cen.eu/esearch.TABLE 1 Chemical Composition LimitsA,B,C,DAloy Si FeCuMnMgCrZn Ti Bi SnPbOther ElementsEAl, minEach TotalF1060 0.25 0.35 0.05 0.03 0.03 . . . 0.05 0.0

24、3 0.03G. . . 99.60 minH1100 -0.95 Si + Fe 0.050.20 0.05 . . . . . . 0.10 . . . 0.05 0.15 99.00 minH2011 0.40 0.7 5.06.0 . . . . . . . . . 0.30 . . . 0.200.6 0.200.6 0.05 0.15 rem2014 0.501.2 0.7 3.95.0 0.401.2 0.200.8 0.10 0.25 0.15 0.05 0.15 rem2024 0.50 0.50 3.84.9 0.300.9 1.21.8 0.10 0.25 0.15 0.

25、05 0.15 rem3003 0.6 0.7 0.050.20 1.01.5 . . . . . . 0.10 . . . 0.05 0.15 remAlclad 3003I3102 0.40 0.7 0.10 0.050.40 . . . . . . 0.30 0.10 0.05 0.15 remAlclad 3102I5005 0.30 0.7 0.20 0.20 0.501.1 0.10 0.25 . . . 0.05 0.15 rem5050 0.40 0.7 0.20 0.10 1.11.8 0.10 0.25 . . . 0.05 0.15 rem5052 0.25 0.40 0

26、.10 0.10 2.22.8 0.150.35 0.10 . . . 0.05 0.15 rem5083 0.40 0.40 0.10 0.401.0 4.04.9 0.050.25 0.25 0.15 0.05 0.15 rem5086 0.40 0.50 0.10 0.200.7 3.54.5 0.050.25 0.25 0.15 0.05 0.15 rem5154 0.25 0.40 0.10 0.10 3.13.9 0.150.35 0.20 0.20 0.05 0.15 rem5456 0.25 0.40 0.10 0.501.0 4.75.5 0.050.20 0.25 0.20

27、 0.05 0.15 rem6061 0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.35 0.25 0.15 0.05 0.15 rem6063 0.200.6 0.35 0.10 0.10 0.450.9 0.10 0.10 0.10 0.05 0.15 rem6262 0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.14 0.25 0.15 0.400.7 0.400.7 0.05 0.15 rem7072 claddingJ0.7 Si + Fe 0.10 0.10 0.10 . . . 0.81.3 . . . 0.05 0

28、.15 rem7075K0.40 0.50 1.22.0 0.30 2.12.9 0.180.28 5.16.1 0.20 0.05 0.15 remALimits are in weight percent maximum unless shown as a range or otherwise stated.BAnalysis shall be made for the elements for which limits are shown in this table.CFor purposes of determining conformance to these limits, an

29、observed value or a calculated value obtained from analysis shall be rounded to the nearest unit in the lastright-hand place of figures used in expressing the specified limit, in accordance with the rounding-off method of Practice E29.DIn case of a discrepancy in the values listed in Table 1 with th

30、ose listed in the International Alloy Designations and Chemical Composition Limits for Wrought Aluminumand Wrought Aluminum Alloys (known as the “Teal Sheets”), the composition limits registered with the Aluminum Association and published in the “Teal Sheets” shall beconsidered the controlling compo

31、sition. The “Teal Sheets” are available at http:/www.aluminum.org/tealsheets.EOthers includes listed elements for which no specific limit is shown as well as unlisted metallic elements. The producer may analyze samples for trace elements notspecified in the specification. However, such analysis is n

32、ot required and may not cover all metallic Others elements. Should any analysis by the producer or the purchaserestablish that an Others element exceeds the limit of Each or that the aggregate of several Others elements exceeds the limit of Other Elements Total, the material shallbe considered non-c

33、onforming.FOther elementsTotal shall be the sum of unspecified metallic elements 0.010 % or more, rounded to the second decimal before determining the sum.GVanadium 0.05 % max.HThe aluminum content shall be calculated by subtracting from 100.00 % the sum of all metallic elements present in amounts o

34、f 0.010 % or more each, roundedtothesecond decimal before determining the sum.IAlloy clad with Alloy 7072.JComposition of cladding alloy as applied during the course of manufacture. The samples from finished tube shall not be required to conform to these limits.KA Zr + Ti limit of 0.25 percent maxim

35、um may be used with this alloy designation for extruded and forged products only, but only when the supplier or producer and thepurchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr +Ti limi

36、t.B210/B210M 192TABLE 2 Tensile Property Limits (US Customary)A,BTemperSpecified WallThickness,Cin.Tensile Strength, ksiYield StrengthD(0.2 % offset), min,ksiElongation in 2 in. or 4 Diameter,Emin, %min maxFull-SectionSpecimenCut-Out SpecimenAluminum 1060FO 0.0140.500 8.5 13.5 2.5 . . . . . .H12 10.

37、0 . 4.0 . .H14 12.0 . . . 10.0 . . . . . .H18 16.0 . . . 13.0 . . . . . .H113G8.5 . 2.5 . .Aluminum 1100FO 0.0100.500 11.0 15.5 3.5 . . . . . .H12 14.0 . 11.0 . .H14 16.0 . . . 14.0 . . . . . .H16 19.0 . . . 17.0 . . . . . .H18 22.0 . . . 20.0 . . . . . .H113G11.0 . 3.5 . .Alloy 2011T3 0.0180.049 47

38、.0 . . . 40.0 . . . . . .0.0500.500 47.0 . . . 40.0 10 8T4511 0.0180.049 44.0 . . . 25.0 . . . . . .0.0500.259 44.0 . . . 25.0 20 180.2600.500 44.0 . . . 25.0 20 20T8 0.0180.500 58.0 . . . 46.0 10 8Alloy 2014O 0.0180.500 . . . 32.0 16.0 max . . . . . .T4, T42H0.0180.024 54.0 . . . 30.0 10 . . .0.025

39、0.049 54.0 . . . 30.0 12 100.0500.259 54.0 . . . 30.0 14 100.2600.500 54.0 . . . 30.0 16 12T6, T62H0.0180.024 65.0 . . . 55.0 7 . . .0.0250.049 65.0 . . . 55.0 7 60.0500.259 65.0 . . . 55.0 8 70.2600.500 65.0 . . . 55.0 9 8Alloy 2024O 0.0180.500 . . . 32.0 15.0 max . . . . . .T3 0.0180.024 64.0 . .

40、. 42.0 10 . . .0.0250.049 64.0 . . . 42.0 12 100.0500.259 64.0 . . . 42.0 14 100.2600.500 64.0 . . . 42.0 16 12T42H0.0180.024 64.0 . . . 40.0 10 . . .0.0250.049 64.0 . . . 40.0 12 100.0500.259 64.0 . . . 40.0 14 100.2600.500 64.0 . . . 40.0 16 12Alloy 3003FO 0.0100.024 14.0 19.0 5.0 . . . . . .0.025

41、0.049 14.0 19.0 5.0 30 200.0500.259 14.0 19.0 5.0 35 250.2600.500 14.0 19.0 5.0 . . . 30H12 0.0100.500 17.0 . . . 12.0 . . . . . .H14 0.0100.024 20.0 . . . 17.0 3 . . .0.0250.049 20.0 . . . 17.0 5 30.0500.259 20.0 . . . 17.0 8 40.2600.500 20.0 . . . 17.0 . . . . . .H16 0.0100.024 24.0 . . . 21.0 . .

42、 . . . .0.0250.049 24.0 . . . 21.0 3 20.0500.259 24.0 . . . 21.0 5 40.2600.500 24.0 . . . 21.0 . . . . . .H18 0.0100.024 27.0 . . . 24.0 2 . . .0.0250.049 27.0 . . . 24.0 3 20.0500.259 27.0 . . . 24.0 5 30.2600.500 27.0 . . . 24.0 . . . . . .H113G0.0100.500 14.0 . . . 5.0 . . . . . .Alloy Alclad 300

43、3FO 0.0100.024 13.0 19.0 4.5 . . . . . .0.0250.049 13.0 19.0 4.5 30 200.0500.259 13.0 19.0 4.5 35 250.2600.500 13.0 19.0 4.5 . . . 30H14 0.0100.024 19.0 . . . 16.0 . . . . . .0.0250.049 19.0 . . . 16.0 5 30.0500.259 19.0 . . . 16.0 8 40.2600.500 19.0 . . . 16.0 . . . . . .H18 0.0100.500 26.0 . . . 2

44、3.0 . . . . . .H113G0.0100.500 13.0 . . . 4.5 . . . . . .Alloy 3102FO 0.0180.049 12.0 17.0 4.0 30I20I0.0500.065 12.0 17.0 4.0 35 25B210/B210M 193TABLE 2 ContinuedTemperSpecified WallThickness,Cin.Tensile Strength, ksiYield StrengthD(0.2 % offset), min,ksiElongation in 2 in. or 4 Diameter,Emin, %min

45、maxFull-SectionSpecimenCut-Out SpecimenAlloy Alclad 3102FO 0.0180.049 10.0 17.0 3.5 30I20I0.0500.065 10.0 17.0 3.5 35 25Alloy 5005FO 0.0180.500 15.0 21.0 5.0 . . . . . .Alloy 5050FO 0.0100.500 18.0 24.0 6.0 . . . . . .H32 0.0100.500 22.0 . . . 16.0 . . . . . .H34 0.0100.500 25.0 . . . 20.0 . . . . .

46、 .H36 0.0100.500 27.0 . . . 22.0 . . . . . .H38 0.0100.500 29.0 . . . 24.0 . . . . . .Alloy 5052FO 0.0100.450 25.0 35.0 10.0 . . . . . .H32 0.0100.450 31.0 . . . 23.0 . . . . . .H34 0.0100.450 34.0 . . . 26.0 . . . . . .H36 0.0100.450 37.0 . . . 29.0 . . . . . .H38 0.0100.450 39.0 . . . 24.0 . . . .

47、 . .Alloy 5083FO 0.0180.450 39.0 51.0 16.0 . . . 14Alloy 5086FO 0.0100.450 35.0 46.0 14.0 . . . . . .H32 0.0100.450 40.0 . . . 28.0 . . . . . .H34 0.0100.450 44.0 . . . 34.0 . . . . . .H36 0.0100.450 47.0 . . . 38.0 . . . . . .Alloy 5154FO 0.0100.500 30.0 41.0 11.0 10 10H34 0.0100.500 39.0 . . . 29.

48、0 5 5H38 0.0100.250 45.0 . . . 34.0 . . . . . .Alloy 5456FO 0.0180.450 41.0 53.0 19.0 . . . 14Alloy 6061O 0.0180.500 . . . 22.0 14.0 max 15 15T4 0.0250.049 30.0 . . . 16.0 16 140.0500.259 30.0 . . . 16.0 18 160.2600.500 30.0 . . . 16.0 20 18T42H0.0250.049 30.0 . . . 14.0 16 140.0500.259 30.0 . . . 1

49、4.0 18 160.2600.500 30.0 . . . 14.0 20 18T6, T62H0.0250.049 42.0 . . . 35.0 10 80.0500.259 42.0 . . . 35.0 12 100.2600.500 42.0 . . . 35.0 14 12T8 0.0350.350 45.0 . . . 40.0 8 . . .Alloy 6063O 0.0180.500 . . . 19.0 . . . . . . . . .T4, T42H0.0250.049 22.0 . . . 10.0 16 140.0500.259 22.0 . . . 10.0 18 160.2600.500 22.0 . . . 10.0 20 18T6, T62H0.0250.049 33.0 . . . 28.0 12 80.0500.259 33.0 . . . 28.0 14 100.2600.500 33.0 . .