ASTM B210-2004 Standard Specification for Aluminum and Aluminum-Alloy Drawn Seamless Tubes《拉制无缝铝和铝合金管的标准规范》.pdf

1、Designation: B 210 04Used in USNRC-NDT standardsStandard Specification forAluminum and Aluminum-Alloy Drawn Seamless Tubes1This standard is issued under the fixed designation B 210; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, t

2、he year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) 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 specification2cover

3、s aluminum and aluminum-alloy drawn seamless tubes in straight lengths and coils forgeneral purpose and pressure applications in alloys (Note 2),tempers, and thicknesses shown in Table 2. Coiled tubes aregenerally available only as round tubes with a wall thicknessnot exceeding 0.083 in. and only in

4、 nonheat-treatable alloys.1.2 Alloy and temper designations are in accordance withANSI H35.1. The equivalent Unified Numbering System alloydesignations are those of Table 1 preceded by A9, for example,A91100 for aluminum designation 1100 in accordance withPractice E 527.NOTE 1See Specification B 483

5、 for aluminum-alloy drawn tubes forgeneral purpose applications; Specification B 234 for aluminum-alloydrawn seamless tubes for condensers and heat exchangers; and Specifi-cation B 241/B 241M for aluminum-alloy seamless pipe and seamlessextruded tube.NOTE 2Throughout this specification, use of the t

6、erm alloy in thegeneral sense includes aluminum as well as aluminum alloy.1.3 A complete metric companion to Specification B 210has been developedSpecification B 210M; therefore, nometric equivalents are presented in this specification.1.4 For acceptance criteria for inclusion of new aluminumand alu

7、minum alloys in this specification, see Annex A2.1.5 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 establish appro-priate safety and health practices and determine the applica-bility of re

8、gulatory limitations prior to use.2. Referenced Documents2.1 The following documents of the issue in effect on dateof material purchase form a part of this specification to theextent referenced herein:2.2 ASTM Standards:3B 234 Specification for Aluminum and Aluminum-AlloyDrawn Seamless Tubes for Con

9、densers and Heat Exchang-ersB 241/B 241M Specification forAluminum andAluminum-Alloy Seamless Pipe and Seamless Extruded TubeB 483 Specification for Aluminum and Aluminum-AlloyDrawn Tubes for General Purpose ApplicationsB 557 Test Methods of Tension Testing Wrought and CastAluminum- and Magnesium-Al

10、loy ProductsB 660 Practices for Packaging/Packing of Aluminum andMagnesium ProductsB 666/B 666M Practice for Identification Marking of Alu-minum and Magnesium ProductsB 881 Terminology Relating to Aluminum- andMagnesium-Alloy ProductsB 918 Practice for Heat Treatment of Wrought AluminumAlloysE29 Pra

11、ctice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE34 Test Methods for ChemicalAnalysis ofAluminum andAluminum-Base AlloysE55 Practice for Sampling Wrought Nonferrous Metals andAlloys for Determination of Chemical CompositionE 215 Practice for Standardizing E

12、quipment for Electro-magnetic Examination of Seamless Aluminum-Alloy TubeE 527 Practice for Numbering Metals and Alloys (UNS)E 607 Test Method for Optical Emission SpectrometricAnalysis of Aluminum and Aluminum Alloys by thePoint-to-Plane Technique, Nitrogen AtmosphereE 716 Practices for Sampling Al

13、uminum and AluminumAlloys for Spectrochemical AnalysisE 1004 Practice for Determining Electrical ConductivityUsing the Electromagnetic (Eddy-Current) MethodE 1251 Test Method for Optical Emission SpectrometricAnalysis ofAluminum andAluminumAlloys by theArgon1This specification is under the jurisdict

14、ion of ASTM Committee B07 on LightMetals and Alloys and is the direct responsibility of Subcommittee B07.03 onAluminum Alloy Wrought Products.Current edition approved Dec. 1, 2004. Published December 2004. Originallyapproved in 1946. Last previous edition approved in 2002 as B 210 02.2For ASME Boile

15、r and Pressure Vessel Code applications see related 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 D

16、ocument Summary page onthe ASTM website.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 19428-2959, United States.Atmosphere, Point-to-Plane, Unipolar Self-Initiating Ca-pacitor Discharge2.3 AN

17、SI Standards:4H35.1 Alloy and Temper Designation Systems for Alumi-numH35.2 Dimensional Tolerances forAluminum Mill Products2.4 Military Standard:5MIL-STD-129 Marking for Shipment and Storage2.5 AMS Specification:6AMS 2772 Heat Treatment of Aluminum Alloy Raw Mate-rials2.6 Federal Standard:5Fed. Std

18、. No. 123 Marking for Shipment (Civil Agencies)3. Terminology3.1 Definitions: Refer to Terminology B 881 for definitionsof product terms used in this specification.3.2 Definitions of Terms Specific to This Standard:3.2.1 capable ofThe term capable of as used in thisspecification means that the test

19、need not be performed by theproducer of the material. However, should subsequent testingby the purchaser establish that the material does not meet theserequirements, the material shall be subject to rejection.TABLE 2 Tensile Property LimitsA,BTemperSpecified WallThickness,Cin.Tensile Strength, ksiYi

20、eld StrengthD(0.2 % offset),min, ksiElongation in 2 in. or 4 3 Diameter,Emin, %min maxFull-SectionSpecimenCut-OutSpecimenAluminum 1060FO 0.0140.500 8.5 13.5 2.5 . .H12 10.0 . 4.0 . .H14 12.0 . 10.0 . .H18 16.0 . 13.0 . .4Available from American National Standards Institute (ANSI), 25 W. 43rd St.,4th

21、 Floor, New York, NY 10036.5Available from Standardization Documents Order Desk, Bldg. 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5098.6Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001.TABLE 1 Chemical Composition LimitsA,B,CAlloy Silicon

22、 Iron Copper Manganese Magnesium Chromium Zinc TitaniumOther ElementsDAluminum,minEach TotalE1060 0.25 0.35 0.05 0.03 0.03 . 0.05 0.03 0.03F. 99.60 minG1100 0.95 Si + Fe 0.050.20 0.05 . . 0.10 . 0.05 0.15 99.00 minG2011 0.40 0.7 5.06.0 . . . 0.30 . 0.05H0.15 remainder2014 0.501.2 0.7 3.95.0 0.401.2

23、0.200.8 0.10 0.25 0.15 0.05 0.15 remainder2024 0.50 0.50 3.84.9 0.300.9 1.21.8 0.10 0.25 0.15 0.05 0.15 remainder3003 0.6 0.7 0.050.20 1.01.5 . . 0.10 . 0.05 0.15 remainderAlclad 3003I3102 0.40 0.7 0.10 0.050.40 . . 0.30 0.10 0.05 0.15 remainderAlclad 3102I5005 0.30 0.7 0.20 0.20 0.501.1 0.10 0.25 .

24、 0.05 0.15 remainder5050 0.40 0.7 0.20 0.10 1.11.8 0.10 0.25 . 0.05 0.15 remainder5052 0.25 0.40 0.10 0.10 2.22.8 0.150.35 0.10 . 0.05 0.15 remainder508350860.400.400.400.500.100.100.401.00.200.74.04.93.54.50.050.250.050.250.250.250.150.150.050.050.150.15remainderremainder5154 0.25 0.40 0.10 0.10 3.

25、13.9 0.150.35 0.20 0.20 0.05 0.15 remainder5456 0.25 0.40 0.10 0.501.0 4.75.5 0.050.20 0.25 0.20 0.05 0.15 remainder6061 0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.35 0.25 0.15 0.05 0.15 remainder6063 0.200.6 0.35 0.10 0.10 0.450.9 0.10 0.10 0.10 0.05 0.15 remainder6262 0.400.8 0.7 0.150.40 0.15 0.81.2

26、0.040.14 0.25 0.15 0.05J0.15 remainder7072 claddingK0.7 Si + Fe 0.10 0.10 0.10 . 0.81.3 . 0.05 0.15 remainder7075 0.40 0.50 1.22.0 0.30 2.12.9 0.180.28 5.16.1 0.20 0.05 0.15 remainderALimits are in weight percent maximum unless shown as a range or otherwise stated.BAnalysis shall be made for the ele

27、ments for which limits are shown in this table.CFor purposes of determining conformance to these limits, an observed value or a calculated value obtained from analysis shall be rounded to the nearestunitinthelast right-hand place of figures used in expressing the specified limit, in accordance with

28、the rounding-off method of Practice E 29.DOthers 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 not required and may not cover all me

29、tallic 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 Total, the material shall be considerednon-conforming.EOther elementsTotal shall be the sum of

30、unspecified metallic elements 0.010 % or more, rounded to the second decimal before determining the sum.FVanadium 0.05 % max.GThe aluminum content shall be calculated by subtracting from 100.00 % the sum of all metallic elements present in amounts of 0.010 % or more each, roundedtothesecond decimal

31、before determining the sum.HBismuth and lead each 0.200.6 %.IAlloy clad with Alloy 7072.JBismuth and lead each 0.400.7 %.KComposition of cladding alloy as applied during the course of manufacture. The samples from finished tube shall not be required to conform to these limits.B210042TABLE 2 Continue

32、dTemperSpecified WallThickness,Cin.Tensile Strength, ksiYield StrengthD(0.2 % offset),min, ksiElongation in 2 in. or 4 3 Diameter,Emin, %min maxFull-SectionSpecimenCut-OutSpecimenH113G8.5 . 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 . .H1

33、8 22.0 . 20.0 . .H113G11.0 3.5Alloy 2011T3 0.0180.049 47.0 . 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 .0.0250.049

34、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 . .T3H0.0180.024 64.0 . 42.0 10 .0.0250.049 64.0 . 42.0 12 100.0500.259 64.0

35、 . 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 . .0.0250.049 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

36、 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 . .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 2

37、7.0 . 24.0 5 30.2600.500 27.0 . 24.0 . .H113G0.0100.500 14.0 . 5.0 . .Alloy Alclad 3003O 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 .0.0500.259 19.0 . 16.0 8 40.2600.500 1

38、9.0 . 16.0 . .H18 0.0100.500 26.0 . 23.0 . .B210043TABLE 2 ContinuedTemperSpecified WallThickness,Cin.Tensile Strength, ksiYield StrengthD(0.2 % offset),min, ksiElongation in 2 in. or 4 3 Diameter,Emin, %min maxFull-SectionSpecimenCut-OutSpecimenH113G0.0100.500 13.0 . 4.5 . .Alloy 3102FO 0.0180.049

39、12.0 17.0 4.0 30I20I0.0500.065 12.0 17.0 4.0 35 25Alloy Alclad 3102FO 0.0180.049 10.0 17.0 3.5 30I20I250.0500.065 10.0 17.0 3.5 35Alloy 5005FOF0.0180.500 15.0 21.0 5.0 . .Alloy 5050FOF0.0100.500 18.0 24.0 6.0 . .H32 22.0 . 16.0 . .H34 25.0 . 20.0 . .H36 27.0 . 22.0 . .H38 29.0 . 24.0 . .Alloy 5052FO

40、F0.0100.450 25.0 35.0 10.0 . .H32 31.0 . 23.0 . .H34 34.0 . 26.0 . .H36 37.0 . 29.0 . .H38 39.0 . 24.0 . .Alloy 5083FOF0.0180.450 39.0 51.0 16.0 . 14Alloy 5086FOF0.0100.450 35.0 46.0 14.0 . .H32 40.0 . 28.0 . .H34 44.0 . 34.0 . .H36 47.0 . 38.0 . .Alloy 5154FO 0.0100.500 30.0 41.0 11.0 10 10H34 39.0

41、 . 29.0 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 0.0250.0490.0500.25930.0 . 16.0 16 140.2600.500 30.0 . 16.0 18 1630.0 . 16.0 20 18T42H0.0250.049 30.0 . 14.0 16 140.0500.259 30.0 . 14.0 18 160.2600.500 30.0 . 14.0 20 1

42、8T6, T62H0.0250.049 42.0 . 35.0 10 80.0500.259 42.0 . 35.0 12 100.2600.500 42.0 . 35.0 14 12Alloy 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 .

43、28.0 16 12T83 0.0250.259 33.0 . 30.0 5 .B210044TABLE 2 ContinuedTemperSpecified WallThickness,Cin.Tensile Strength, ksiYield StrengthD(0.2 % offset),min, ksiElongation in 2 in. or 4 3 Diameter,Emin, %min maxFull-SectionSpecimenCut-OutSpecimenT831 0.0250.259 28.0 . 25.0 5 .T832 0.0250.049 41.0 . 36.0

44、 8 50.0500.259 40.0 . 35.0 8 5Alloy 6262T6, T62H0.0250.049 42.0 . 35.0 10 80.0500.259 42.0 . 35.0 12 100.2600.500 42.0 . 35.0 14 12T9 0.0250.375 48.0 . 44.0 5 4Alloy 7075O 0.0250.049 . 40.0 21.0 max 10 80.0500.500 . 40.0 21.0 max 12 10T6, T62H0.0250.259 77.0 . 66.0 8 70.2600.500 77.0 . 66.0 9 8T73J0

45、.0250.259 66.0 . 56.0 10 80.2600.500 66.0 . 56.0 12 10ASee Annex A1.BTo determine conformance to this specification, each value for tensile strength and for yield strength shall be rounded to the nearest 0.1 ksi and each value forelongation to the nearest 0.5 % both in accordance with the rounding-o

46、ff method of Practice E29.CCoiled tube is generally available with a maximum wall thickness of 0.083 in. and only in nonheat-treatable alloys.DYield strength to be determined only on straight tube.EElongation of full-section and cut-out sheet-type specimens is measured in 2 in. of cut-out round spec

47、imens, in 43 specimen diameter.FIn this alloy tube other than round is produced only in the F (as drawn) and O tempers. Properties for F temper are not specified or guaranteed.GBeginning with the 1982 issue the requirements for the H112 tempers were replaced by the H113 temper, applicable to other t

48、han round tube, which is fabricated bycold-forming annealed round tube and acquires some temper in this forming operation.HMaterial in the T42 or T62 tempers is not available from the material producers.IFor specified wall thickness under 0.025 in., elongation is not required.JMaterial in this tempe

49、r exhibits improved resistance to stress corrosion compared to that of the T6 temper. The stress-corrosion resistance capability of individual lotsis determined by testing the previously selected tension-test samples in accordance with the applicable electrical conductivity acceptance criteria of Table 3.4. Ordering Information4.1 Orders for material to this specification shall include thefollowing information:4.1.1 This specification d