ASTM B211-2012 Standard Specification for Aluminum and Aluminum-Alloy Rolled or Cold Finished Bar Rod and Wire 《铝和铝合金轧制或冷加工棒材杆材金属丝的标准规格》.pdf

《ASTM B211-2012 Standard Specification for Aluminum and Aluminum-Alloy Rolled or Cold Finished Bar Rod and Wire 《铝和铝合金轧制或冷加工棒材杆材金属丝的标准规格》.pdf》由会员分享，可在线阅读，更多相关《ASTM B211-2012 Standard Specification for Aluminum and Aluminum-Alloy Rolled or Cold Finished Bar Rod and Wire 《铝和铝合金轧制或冷加工棒材杆材金属丝的标准规格》.pdf（10页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: B211 12Standard Specification forAluminum and Aluminum-Alloy Rolled or Cold Finished Bar,Rod, and Wire1This standard is issued under the fixed designation B211; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year

2、of last revision. A number in parentheses indicates 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 rolled

3、or cold-finished bar,rod, and wire in alloys (Note 1) and tempers as shown in Table2.NOTE 1Throughout this specification use of the term alloy in thegeneral sense includes aluminum as well as aluminum alloy.NOTE 2The term cold finished is used to indicate the type of surfacefinish, sharpness of angl

4、es, and dimensional tolerances produced bydrawing through a die.NOTE 3See Specification B221 for aluminum and aluminum-alloyextruded bars, rods, wire, shapes, and tubes; and Specification B316/B316M for aluminum and aluminum-alloy rivet and cold-heading wireand rods.1.2 Alloy and temper designations

5、 are in accordance withANSI H35.1. The equivalent UNS alloy designations are thoseof Table 1 preceded by A9, for example, A91100 for aluminum1100 in accordance with Practice E527.1.3 Acomplete metric companion to Specification B211 hasbeen developedB211M; therefore, no metric equivalents arepresente

6、d in this specification.1.4 For acceptance criteria for inclusion of new aluminumand aluminum alloys in this specification, see Annex A2.2. Referenced Documents2.1 The following documents of the issue in effect on dateof material purchase form a part of this specification to theextent referenced her

7、ein:2.2 ASTM Standards:3B221 Specification for Aluminum and Aluminum-AlloyExtruded Bars, Rods, Wire, Profiles, and TubesB316/B316M Specification for Aluminum and Aluminum-Alloy Rivet and Cold-Heading Wire and RodsB557 Test Methods for Tension Testing Wrought and CastAluminum- and Magnesium-Alloy Pro

8、ductsB594 Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace ApplicationsB660 Practices for Packaging/Packing of Aluminum andMagnesium ProductsB666/B666M Practice for Identification Marking of Alumi-num and Magnesium ProductsB881 Terminology Relating toAluminum- and

9、Magnesium-Alloy ProductsB918 Practice for Heat Treatment of Wrought AluminumAlloysE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE34 Test Methods for Chemical Analysis of Aluminum andAluminum-Base AlloysE290 Test Methods for Bend Testing of Material

10、 for Duc-tilityE527 Practice for Numbering Metals and Alloys in theUnified Numbering System (UNS)E607 Test Method for Atomic Emission SpectrometricAnalysis Aluminum Alloys by the Point to Plane Tech-nique Nitrogen Atmosphere4E716 Practices for Sampling and Sample Preparation ofAluminum and Aluminum

11、Alloys for Determination ofChemical Composition by Spectrochemical AnalysisE1004 Test Method for Determining Electrical Conductiv-ity Using the Electromagnetic (Eddy-Current) MethodE1251 Test Method for Analysis of Aluminum and Alumi-num Alloys by Spark Atomic Emission SpectrometryG47 Test Method fo

12、r Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXXAluminumAlloyProducts2.3 ANSI Standards:H35.1 Alloy and Temper Designation Systems for Alumi-num51This specification is under the jurisdiction of ASTM Committee B07 on LightMetals and Alloys and is the direct responsibility of

13、 Subcommittee B07.03 onAluminum Alloy Wrought Products.Current edition approved Jan. 15, 2012. Published March 2012. Originallyapproved in 1946. Last previous edition approved in 2003 as B21103. DOI:10.1520/B0211-12.2For ASME Boiler and Pressure Vessel Code applications see related Specifi-cation SB

14、-211 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.4Withdrawn. The last approved

15、 version of this historical standard is referencedon www.astm.org.5Available from American National Standards Institute (ANSI), 25 W. 43rd St.,4th Floor, New York, NY 10036, http:/www.ansi.org.1*A Summary of Changes section appears at the end of this standard.Copyright ASTM International, 100 Barr H

16、arbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.H35.2 Dimensional Tolerances for Aluminum Mill Prod-ucts52.4 Federal Standard:Fed. Std. No. 123 Marking for Shipment (Civil Agencies)62.5 Military Standard:MIL-STD-129 Marking for Shipment and Storage62.6 Aerospace Material Sp

17、ecification:AMS 2772 Heat Treatment of Aluminum Alloy Raw Mate-rials72.7 The Aluminum Association:International Alloy Designations and Chemical CompositionLimits for Wrought Aluminum and Wrought AluminumAlloys82.8 Other Standards:CEN EN 14242 Aluminium andAluminiumAlloysChemi-cal AnalysisInductively

18、 Coupled Plasma Optical Emis-sion Spectral Analysis93. Terminology3.1 Definitions:3.1.1 Refer to Terminology B881 for definitions of productterms in this specification.3.1.2 flattened and slit wireFlattened wire which has beenslit to obtain square edges.3.2 Definitions of Terms Specific to This Stan

19、dard:3.2.1 capable ofThe term capable of as 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

20、. Ordering Information4.1 Orders for material 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 pounds,4.1.3 Alloy (Section 7),4.1.4 Temper (Sectio

21、n 9),4.1.5 Product Form, Rolled or cold finished bar, rolled orcold finished rod, or wire,4.1.6 Geometry and Dimensions, Diameter for rounds; dis-tance across flats for square-cornered squares, hexagons, oroctagons; width and depth for square-cornered rectangles(orders for squares, hexagons, octagon

22、s, or rectangles withrounded corners usually require a drawing),4.1.7 Length, and6Available from Standardization Documents Order Desk, Bldg. 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5094, Attn: NPODS.7Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale,

23、PA 15096-0001.8Available from The Aluminum Association, Inc. 1525 Wilson Boulevard,Arlington, VA 22209, www.aluminum.org9Available from European Committee for Standardization, Central Secretariat(CEN), rue de Stassart 36, B1050 Brussels, Belgium. http:/www.cen.eu/esearchTABLE 1 Chemical Composition

24、LimitsA,B,C,DAlloy Si Fe Cu Mn Mg Cr Ni Zn Ti Bi Pb SnOther ElementsEAluminumEach TotalF1100 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 . 0.200.6 0.200.6 . 0.05 0.15 remainder2014 0.501.2 0.7 3.95.0 0.401.2 0.200.8 0.10 . 0.25 . . . 0.15 0.05

25、0.15 remainder2017 0.200.8 0.7 3.54.5 0.401.0 0.400.8 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 remainder2219 0.20 0.30 5.86.8 0.200.40 0.02 . . 0.10 . . . 0.020.10 0.05H0.15Hremainder3003 0.6 0.7 0.050.20 1.01.5 . . . 0.10 . . .

26、. 0.05 0.15 remainder4032 11.013.5 1.0 0.501.3 . 0.81.3 0.10 0.51.3 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 remainder5056 0.30 0.40 0.10 0.050.20 4.55.6 0.050.20 . 0.10 . . . . 0.05 0.15 remainder5154I0.25 0.40 0.10 0.10 3.13.9 0.150.35 . 0.2

27、0 . . . 0.20 0.05 0.15 remainder6013 0.61.0 0.50 0.61.1 0.200.8 0.81.2 0.10 . 0.25 0.10 . . . 0.05 0.15 remainder6020 0.400.9 0.50 0.300.9 0.35 0.61.2 0.15 . 0.20 0.15 . 0.05 0.91.5 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 remainder6110 0.71.5 0.8

28、 0.200.7 0.200.7 0.501.1 0.040.25 . 0.30 . . . 0.15 0.05 0.15 remainder6262 0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.14 . 0.25 . 0.400.7 0.400.7 0.15 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 mass percent maximum unless otherwis

29、e shown.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 expressi

30、ng the specified limit, in accordance with the rounding-off method of Practice E29.DIn case of any discrepancy in the values listed in Table 3 when compared with those listed in the “Teal Sheets” (International Alloy Designations and ChemicalComposition Limits for Wrought Aluminum and Wrought Alumin

31、um Alloys), the composition limits registered with The Aluminum Association and published in the “TealSheets” shall be considered the controlling composition.EOthers includes listed elements for which no specific limit is shown as well as unlisted metallic elements. The producer may analyze samples

32、for trace elements notspecified in the specification. However, such analysis 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

33、 exceeds the limit of Total, the material shall be considerednon-conforming.FOther elementsTotal shall be the sum of unspecified metallic elements 0.010 % or more each, rounded to the second decimal before determining the sum.GThe aluminum content is the difference between 100.00 % and the sum of al

34、l other metallic elements and silicon present in amounts of 0.010 % or more each, roundedto the second decimal before determining the sum.HVanadium 0.050.15 % zirconium 0.100.25 %. The total for other elements does not include vanadium and zirconium.IBeryllium 0.0003 maximum for welding electrode an

35、d welding rod only.B211 1224.1.8 Tensile property limits and dimensional tolerances forsized not covered in Table 2 and in ANSI H35.2, respectively.4.2 Additionally, orders for material to this specificationshall include the following information when required by thepurchaser:4.2.1 Whether heat trea

36、tment in accordance with PracticeB918 is required (8.2),4.2.2 Whether 7075-O material is required to develop re-quirements for T73 temper (see 10.1.2),4.2.3 Whether bend testing is required for 2017, 2024, or3003 (Section 12),4.2.4 When specified finish of bar and rod is not required(Section 15),4.2

37、.5 Whether marking for identification is required (Sec-tion 16),4.2.6 Whether ultrasonic inspection is required (Section 17,Table 3),4.2.7 Whether inspection or witness of inspection and testsby the purchasers representative is required prior to materialshipment (Section 19),4.2.8 Whether certificat

38、ion is required (Section 21), and4.2.9 Whether Practices B660 apply, and if so, the levels ofpreservation, packaging, and packing required (Section 22).5. Manufacture5.1 The products covered by this specification shall beproduced either by hot extruding and cold finishing or by hotrolling with or wi

39、thout cold finishing, at the option of theproducer.TABLE 2 Mechanical Property LimitsATemperSpecified Diameter orThickness, in.Tensile Strength, ksiYield StrengthB(0.2 % offset),min, ksiElonga-tionBin2in.or 4 3 Diam-eter, min, %min maxAluminum 1100O 0.124 and under 11.0 15.5 . .0.125 and over 11.0 1

40、5.5 3.0 25H12 0.374 and under 14.0 . . .H14 0.374 and under 16.0 . . .H16 0.374 and under 19.0 . . .H18 0.374 and under 22.0 . . .H112 all 11.0 . 3.0 .FalC.C.Alloy 2011T3 0.1251.500 45.0 . 38.0 101.5012.000 43.0 . 34.0 122.0013.500 42.0 . 30.0 12T4 and T451D0.1258.000 40.0 . 18.0 16T6 and T651 0.375

41、6.500 54.0 . 40.0 10T8 0.1253.250 54.0 . 40.0 10Alloy 2014EO 0.124 and under . 35.0 . .0.1258.000 . 35.0 . 12T4, T42F, and T451D0.124 and under 55.0 . . .0.1258.000G55.0 . 32.0 16T6, T62F, and T651D0.124 and under 65.0 . . .0.1258.000G65.0 . 55.0 8Alloy 2017EO 0.124 and under . 35.0 . .0.1258.000 .

42、35.0 . 16T4, T42F, and T451D0.124 and under 55.0 . . .0.1258.000H55.0 . 32.0 12Alloy 2024EO 0.124 and under . 35.0 . .0.1258.000 . 35.0 . 16T36 0.124 and under 69.0 . . .0.1250.375 69.0 . 52.0 10T4I0.124 and under 62.0 . . .0.1250.499 62.0 . 45.0I100.5004.500G62.0 . 42.0I104.5016.500J62.0 . 40.0 106

43、.5018.000J58.0 . 38.0 10T42F0.124 and under 62.0 . . .0.1251.000 62.0 . 40.0 101.0016.500G62.0 . 40.0 10T351D0.5006.500G62.0 . 45.0 106.5018.000 62.0 . 45.0 9T6 0.124 and under 62.0 . . .0.1256.500G62.0 . 50.0 5B211 123TABLE 2 ContinuedTemperSpecified Diameter orThickness, in.Tensile Strength, ksiYi

44、eld StrengthB(0.2 % offset),min, ksiElonga-tionBin2in.or 4 3 Diam-eter, min, %min maxT62F0.124 and under 60.0 . . .0.1256.500G60.0 . 46.0 5T851D0.5006.500G66.0 . 58.0 5Alloy 2219T851D0.5002.000 58.0 . 40.0 42.0014.000 57.0 . 39.0 4Alloy 3003O all 14.0 19.0 5.0 25H12 0.374 and under 17.0 . . .H14 0.3

45、74 and under 20.0 . . .H16 0.374 and under 24.0 . . .H18 0.374 and under 27.0 . . .H112 all 14.0 . 5.0 .FalC.C.Alloy 4032T86 0.3750.750 51.0 . 46.0 4Alloy 5052O 0.124 and under . 32.0 . .0.125 and over 25.0 32.0 9.5 25H32 0.124 and under 31.0 . . .0.1250.374 31.0 . 23.0 .H34 0.374 and under 34.0 . 2

46、6.0 .H36 0.124 and under 37.0 . . .0.1250.374 37.0 . 29.0 .H38 0.374 and under 39.0 . . .FalCC.Alloy 5056O 0.124 and under . 46.0 . .0.125 and over . 46.0 . 20H111 0.374 and under 44.0 . . .H12 0.374 and under 46.0 . . .H32 0.374 and under 44.0 . . .H14 0.374 and under 52.0 . . .H34 0.374 and under

47、50.0 . . .H18 0.374 and under 58.0 . . .H38 0.374 and under 55.0 . . .H192 0.374 and under 60.0 . . .H392 0.374 and under 58.0 . . .Alloy 5154O all 30.0 41.0 11.0 25H32 0.374 and under 36.0 . . .H34 0.374 and under 39.0 . . .H36 0.374 and under 42.0 . . .H38 0.374 and under 45.0 . . .H112 all 30.0 .

48、 11.0 .Alloy 6013T651 0.5004.000 56.0 . 52.0 7T8 0.7501.500 58.0 . 56.0 81.5015.500 57.0 . 55.0 7Alloy 6020T8 0.1870.375 43.0 . 40.0 120.3761.999 42.0 . 39.0 122.0003.250 39.0 . 36.0 12Alloy 6061EO 0.124 and under . 22.0 . .0.1258.000 . 22.0 . 18T4 and T451D0.124 and under 30.0 . . .0.1258.000H30.0

49、. 16.0 18T42F0.1258.000H30.0 . 14.0 18T6, T62F, and T651D0.124 and under 42.0 . . .0.1258.000H42.0 . 35.0 10T89 and T94 0.374 and under 54.0 . 47.0 .B211 124TABLE 2 ContinuedTemperSpecified Diameter orThickness, in.Tensile Strength, ksiYield StrengthB(0.2 % offset),min, ksiElonga-tionBin2in.or 4 3 Diam-eter, min, %min maxAlloy 6110T9 0.374 and under 65.0 . 63.0 2Alloy 6262T6 and T651D0.1258.000G42.0 . 35.0 10T8 0.7502.000 45.0 . 43.0 12T9 0.1252.000 52.0 . 48.0 52.001