1、Designation: B 210M 05METRICStandard Specification forAluminum and Aluminum-Alloy Drawn Seamless TubesMetric1This standard is issued under the fixed designation B 210M; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of la
2、st 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 specification covers aluminum an
3、d aluminum-alloydrawn seamless tubes in straight lengths and coils for generalpurpose and pressure applications in alloys (Note 2), tempers,and thicknesses shown in Table 2. Coiled tubes are generallyavailable only as round tubes with a wall thickness notexceeding 2.00 mm and only in nonheat-treatab
4、le alloys.1.2 Alloy and temper designations are in accordance withANSI H35.1M. The equivalent Unified Numbering Systemalloy designations are those of Table 1 preceded by A9, forexample, A91100 for aluminum 1100 in accordance withPractice E 527.1.3 Preferred metric sizes are in accordance with ANSIB
5、32.5.NOTE 1See Specification B 483M for aluminum and aluminum-alloydrawn tubes for general purpose applications, Specification B 234M foraluminum-alloy drawn seamless tubes for condensers and heat exchang-ers, and Specification B 241/B 241M for aluminum-alloy seamless pipeand seamless extruded tube.
6、NOTE 2Throughout this specification use of the term alloy in thegeneral sense includes aluminum as well as aluminum alloy.1.4 This specification is the metric counterpart of Specifi-cation B 210.1.5 For acceptance criteria for inclusion of new aluminumand aluminum alloys in this specification, see A
7、nnex A2.1.6 The values stated in SI units are to be regarded asstandard. No other units of measure are included in thisstandard.1.7 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
8、appro-priate safety and health practices and determine the applica-bility of regulatory 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:2
9、B 234M Specification for Aluminum and Aluminum-AlloyDrawn Seamless Tubes for Condensers and Heat Exchang-ersB 241/B 241M Specification forAluminum andAluminum-Alloy Seamless Pipe and Seamless Extruded TubeB 483M Specification for Aluminum and Aluminum-AlloyDrawn Tubes for General Purpose Application
10、sB 557M Test Methods of Tension Testing Wrought and CastAluminum- and Magnesium-Alloy Products MetricB 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 Aluminium- and
11、Magnesium-Alloy ProductsB 918 Practice for Heat Treatment of Wrought AluminumAlloysE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE34 Test Methods for ChemicalAnalysis ofAluminum andAluminum-Base AlloysE55 Practice for Sampling Wrought Nonferrous Me
12、tals andAlloys for Determination of Chemical CompositionE 215 Practice for Standardizing Equipment 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
13、 Alloys by thePoint-to-Plane Technique, Nitrogen Atmosphere1This specification is under the jurisdiction of ASTM Committee B07 on LightMetals and Alloys and is the direct responsibility of Subcommittee B07.03 onAluminum Alloy Wrought Products.Current edition approved June 1, 2005. Published June 200
14、5. Originallyapproved in 1980. Last previous edition approved in 2002 as B 210M 02.2For 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 pa
15、ge 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.E 716 Practices for Sampling Aluminum and AluminumAlloys for Spectrochemical AnalysisE 1004 Pract
16、ice for Determining Electrical ConductivityUsing the Electromagnetic (Eddy-Current) MethodE 1251 Test Method for Optical Emission SpectrometricAnalysis ofAluminum andAluminumAlloys by theArgonAtmosphere, Point-to-Plane, Unipolar Self-Initiating Ca-pacitor Discharge2.3 ANSI Standards:3B 32.5 Preferre
17、d Metric Sizes For Tubular Metal ProductsOther Than PipeH35.1M Alloy and Temper Designation Systems for Alu-minumH35.2M Dimensional Tolerances for Aluminum Mill Prod-ucts2.4 Military Standard:4MIL-STD-129 Marking for Shipment and Storage2.5 AMS Specification:5AMS 2772 Heat Treatment of Aluminum Allo
18、y Raw Mate-rials2.6 Federal Standard:4Fed. Std. 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
19、used in thisspecification means that the test 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.4. Ordering Information4.1 Orders for materia
20、l to this specification shall include thefollowing information:4.1.1 This specification designation (which includes thenumber, the year, and the revision letter, if applicable),4.1.2 Quantity in pieces or kilograms,4.1.3 Alloy (Section 7),4.1.4 Temper (Section 8),3Available from American National St
21、andards Institute (ANSI), 25 W. 43rd St.,4th Floor, New York, NY 10036.4Available from Standardization Documents Order Desk, Bldg. 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5098.5Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001.TABLE 1 C
22、hemical Composition LimitsABCAlloy Silicon 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
23、 remainder2014 0.501.2 0.7 3.95.0 0.401.2 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 3102I5
24、005 0.30 0.7 0.20 0.20 0.501.1 0.10 0.25 . 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 remainder508350860.400.400.400.500.100.100.401.00.200.74.04.93.54.50.050.250.050.250.250.250.150.150.050.050.150.15rem
25、ainderremainder5154 0.25 0.40 0.10 0.10 3.13.9 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 remai
26、nder6262 0.400.8 0.7 0.150.40 0.15 0.81.2 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
27、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 observed value or a calculated value obtained from analysis shall be rounded to the nearestunitinthelast right-hand place of figures used in expressin
28、g the specified limit, in accordance with the rounding-off method of Practice E29.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
29、 is not 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 Total, the material shall be considerednon-conforming.
30、EOther elementsTotal shall be the sum of 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 %
31、or more each, roundedtothesecond decimal before determining the sum.HBismuth and lead each 0.20 0.6 %.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 confo
32、rm to these limits.B210M052TABLE 2 Tensile Property LimitsA,BTemperSpecified Wall ThicknessCTensile Strength, MPaYield StrengthD(0.2 % offset), MPaElongation,Emin, %Over Through Min Max Min MaxFull-SectionSpecimen in50 mmCut-Out Specimenin 50 mmin 5 3 Diam-eter(5.65 =A )Aluminum 1060FO 0.25 12.50 60
33、 95 15 . . . .H12 0.25 12.50 70 . 30 . . . .H14 0.25 12.50 85 . 70 . . . .H18 0.25 12.50 110 . 90 . . . .H113G0.25 12.50 60 . 15 . . . .F All . . . . . . .Aluminum 1100FO 0.32 12.50 75 105 25 . . . .H12 0.32 12.50 95 . 75 . . . .H14 0.32 12.50 110 . 95 . . . .H16 0.32 12.50 130 . 115 . . . .H18 0.32
34、 12.50 150 . 140 . . . .H113G0.32 12.50 75 . 25 . . . .F All . . . . . . .Alloy 2011T3 0.45 1.20 325 . 275 . . . .1.20 12.50 325 . 275 . 10 8 7T4511 0.45 1.20 305 . 170 . . . .1.20 6.30 305 . 170 . 20 18 166.30 12.50 305 . 170 . 20 20 18T8 0.45 12.50 400 . 315 . 10 8 7Alloy 2014O 0.45 12.50 . 220 .
35、110 . . .T4, T42H0.45 0.63 370 . 205 . 10 . .0.63 1.20 370 . 205 . 12 10 .1.20 6.30 370 . 205 . 14 10 .6.30 12.50 370 . 205 . 16 12 10T6, T62H0.45 0.63 450 . 380 . 7 . .0.63 1.20 450 . 380 . 7 6 .1.20 6.30 450 . 380 . 8 7 .6.30 12.50 450 . 380 . 9 8 7Alloy 2024O 0.45 12.50 . 220 . 100 . . .T3 0.45 0
36、.63 440 . 290 . 10 . .0.63 1.20 440 . 290 . 12 10 .1.20 6.30 440 . 290 . 14 10 .6.30 12.50 440 . 290 . 16 12 10T42H0.45 0.63 440 . 275 . 10 . .0.63 1.20 440 . 275 . 12 10 .1.20 6.30 440 . 275 . 14 10 .6.30 12.50 440 . 275 . 16 12 10Alloy 3003FO 0.25 0.63 95 130 35 . . . .0.63 1.20 95 130 35 . 30 20
37、.1.20 6.30 95 130 35 . 35 25 .6.30 12.50 95 130 35 . . 30 27H12 0.25 0.63 120 . 85 . . . .0.63 1.20 120 . 85 . . . .H14 . 0.63 140 . 115 . 3 . .0.63 1.20 140 . 115 . 5 3 .1.20 6.30 140 . 115 . 8 4 .6.30 12.50 140 . 115 . . . .H16 0.25 0.63 165 . 145 . . . .0.63 1.20 165 . 145 . 3 2 .1.20 6.30 165 .
38、145 . 5 4 .6.30 12.50 165 . 145 . . . .H18 . 0.63 185 . 165 . 2 . .0.63 1.20 185 . 165 . 3 2 .1.20 6.30 185 . 165 . 5 3 .6.30 12.50 185 . 165 . . . .H113G0.25 12.50 95 . 35 . . . .B210M053TABLE 2 ContinuedTemperSpecified Wall ThicknessCTensile Strength, MPaYield StrengthD(0.2 % offset), MPaElongatio
39、n,Emin, %Over Through Min Max Min MaxFull-SectionSpecimen in50 mmCut-Out Specimenin 50 mmin 5 3 Diam-eter(5.65 =A )F All . . . . . . .Alloy Alclad 3003FO 0.25 0.63 90 125 30 . . . .0.63 1.20 90 125 30 . 30 20 .1.20 6.30 90 125 30 . 35 25 .6.30 12.50 90 125 30 . . 30 27H14 0.25 0.63 135 . 110 . . . .
40、0.63 1.20 135 . 110 . 5 . .1.20 6.30 135 . 110 . 8 4 .6.30 12.50 135 . 110 . . . .H18 0.25 12.50 180 . 160 . . . .H113G0.25 12.50 90 . 30 . . . .F All . . . . . . .Alloy 3102FO 0.501.201.201.60858511511530D30D.30352025.Alloy Alclad 3102FO 0.501.201.201.6070701151152525.30352035.Alloy 5005FOF0.45All1
41、2.50 105.145.35.Alloy 5050FO 0.25 12.50 125 165 40 . . . .H32 0.25 12.50 150 . 110 . . . .H34 0.25 12.50 170 . 140 . . . .H36 0.25 12.50 185 . 150 . . . .H38 0.25 12.50 200 . 165 . . . .F All . . . . . . .Alloy 5052FO 0.25 11.50 170 240 70 . . . .H32 0.25 11.50 215 . 160 . . . .H34 0.25 11.50 235 .
42、180 . . . .H36 0.25 11.50 255 . 200 . . . .H38 0.25 11.50 270 . 215 . . . .F All . . . . . . .Alloy 5083FOF0.45All11.50 270.350.110.14.12.Alloy 5086FO 0.25 11.50 240 315 95 . . 14 12H32 0.25 11.50 275 . 195 . . . .H34 0.25 11.50 300 . 235 . . . .H36 0.25 11.50 325 . 260 . . . .F All . . . . . . .All
43、oy 5154FO 0.25 12.50 205 285 75 . 10 10 9H34 0.25 12.50 270 . 200 . 5 5 4H38 0.25 6.30 310 . 235 . . . .F All . . . . . . .Alloy 5456FOF0.45All11.50 285.365.130.14.12.Alloy 6061O 0.45 12.50 . 150 . 95 15 15 13T4 0.63 1.20 205 . 100 . 16 14 .1.20 6.30 205 . 110 . 18 16 .B210M054TABLE 2 ContinuedTempe
44、rSpecified Wall ThicknessCTensile Strength, MPaYield StrengthD(0.2 % offset), MPaElongation,Emin, %Over Through Min Max Min MaxFull-SectionSpecimen in50 mmCut-Out Specimenin 50 mmin 5 3 Diam-eter(5.65 =A )6.30 12.50 205 . 110 . 20 18 16T42H0.63 1.20 205 . 95 . 16 14 .1.20 6.30 205 . 95 . 18 16 .6.30
45、 12.50 205 . 95 . 20 18 16T6, T62H0.63 1.20 290 . 240 . 10 8 .1.20 6.30 290 . 240 . 12 10 .6.30 12.50 290 . 240 . 14 12 10Alloy 6063O 0.45 12.50 . 130 . . . . .T4, T42H0.63 1.20 150 . 70 . 16 14 .1.20 6.30 150 . 70 . 18 16 .6.30 12.50 150 . 70 . 20 18 16T6, T62H0.631.206.301.206.3012.50230230230.195
46、195195.12141681012.10T83 0.63 6.30 230 . 205 . 5 . .T831 0.63 6.30 195 . 170 . 5 . .T832 0.63 1.20 285 . 250 . 8 5 .1.20 6.30 275 . 240 8 5 .Alloy 6262T6, T62H0.63 1.20 290 . 240 . 10 8 .1.20 0.63 290 . 240 . 12 10 .6.30 12.50 290 . 240 . 14 12 10T9 0.63 10.00 330 . 305 . 5 4 3Alloy 7075O 0.631.201.
47、2012.50.275275.1451451012810.9T6, T62H0.63 6.30 530 . 455 . 8 7 .6.30 12.50 530 . 455 . 9 8 7T73I0.63 6.30 455 . 385 . 10 8 .6.30 12.50 455 . 385 . 12 10 9ASee Annex A1.BTo determine conformance to this specification, each value for tensile strength and for yield strength shall be rounded to the nea
48、rest 0.1 MPa and each value forelongation to the nearest 0.5 % both in accordance with the rounding method of Practice E29.CCoiled tube is generally available with a maximum wall thickness of 2.00 mm and only in nonheat-treatable alloys.DYield strength to be determined only on straight tube.EElongat
49、ion in 50 mm apply for tube tested in full-section, for sheet-type specimens, for tubes having a flat wall, and for similar curved specimens for tubes having acurved wall, up to a maximum wall thickness of 12.50 mm. Elongations in 5D (5.65 =A ), where D and A are diameter and cross-sectional area of the specimens,respectively, apply to round test specimens machined from wall thicknesses over 6.30 mm.FIn this alloy tube other than round is produced only in the F (as drawn) and O tempers. Properties for F
