1、Designation: B 211 03Standard Specification forAluminum and Aluminum-Alloy Bar, Rod, and Wire1This standard is issued under the fixed designation B 211; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A n
2、umber 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 specification2covers rolled or cold-finished bar
3、,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 angles, and dimensional
4、tolerances produced bydrawing through a die.NOTE 3See Specification B 221 for aluminum and aluminum-alloyextruded bars, rods, wire, shapes, and tubes; and Specification B 316/B 316M for aluminum and aluminum-alloy rivet and cold-heading wireand rods.1.2 Alloy and temper designations are in accordanc
5、e withANSI H35.1. The equivalent UNS alloy designations are thoseof Table 1 preceded by A9, for example, A91100 for aluminum1100 in accordance with Practice E 527.1.3 A complete metric companion to Specification B 211has been developedB 211M; therefore, no metric equivalentsare presented in this spe
6、cification.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 herein:2.2 ASTM
7、Standards:3B 221 Specification for Aluminum and Aluminum-AlloyExtruded Bars, Rods, Wire, Profiles, and TubesB 316/B 316M Specification for Aluminum and Aluminum-Alloy Rivet and Cold-Heading Wire and RodsB 557 Test Methods of Tension Testing Wrought and CastAluminum- and Magnesium-Alloy ProductsB 594
8、 Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace ApplicationsB 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 and Magne
9、siumAlloy ProductsB 918 Practice for Heat Treatment of Wrought AluminumAlloysE 29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE 34 Test Methods for Chemical Analysis of Aluminum andAluminum-Base AlloysE 55 Practice for Sampling Wrought Nonferrous Met
10、als andAlloys for Determination of Chemical CompositionE 290 Test Methods for Bend Testing of Material forDuctilityE 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
11、 AtmosphereE 716 Practices for Sampling Aluminum and AluminumAlloys for Spectrochemical AnalysisE 1004 Practice for Determining Electrical ConductivityUsing the Electromagnetic (Eddy-Current) MethodE 1251 Test Method for Optical Emission SpectrometricAnalysis of Aluminum and Aluminum Alloys by the A
12、rgonAtmosphere, Point-to-Plane, Unipolar Self Initiating Ca-pacitor DischargeG 47 Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum-Alloy Products2.3 ANSI Standards:H35.1 Alloy and Temper Designation Systems for Alumi-numH35.2 Dimensional Tolerances fo
13、r Aluminum Mill Products2.4 Federal Standard:Fed. Std. No. 123 Marking for Shipment (Civil Agencies)41This 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
14、 approved Nov. 1, 2003. Published November 2003. Originallyapproved in 1946. Last previous edition approved in 2002 as B 21102.2For ASME Boiler and Pressure Vessel Code applications see related Specifi-cation SB-211 in Section II of that Code.3For referenced ASTM standards, visit the ASTM website, w
15、ww.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.4Available from Standardization Documents Order Desk, Bldg. 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5094,
16、 Attn: NPODS.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.2.5 Military Standard:MIL-STD-129 Marking for Shipment and Storage42.6 Aerospace Material Specification:AM
17、S 2772 Heat Treatment of Aluminum Alloy Raw Mate-rials53. Terminology3.1 Definitions: Refer to Terminology B 881 for definitionsof product terms in this specification.3.1.1 flatten and slit wireFlatten wire which has been slitto obtain square edges.3.2 Definitions of Terms Specific to This Standard:
18、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. Ord
19、ering 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 (Section 9),
20、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, octagons, or
21、 rectangles withrounded corners usually require a drawing),4.1.7 Length, and4.1.8 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
22、 required by thepurchaser:4.2.1 Whether heat treatment in accordance with PracticeB 918 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 fin
23、ish of bar and rod is not required(Section 15),4.2.5 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 mate
24、rialshipment (Section 19),4.2.8 Whether certification is required (Section 21), and4.2.9 Whether Practices B 660 apply, and if so, the levels ofpreservation, packaging, and packing required (Section 22).5Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-
25、0001.TABLE 1 Chemical Composition LimitsA,B,CAlloy Silicon Iron Copper Manganese Magnesium Chromium Zinc Bismuth Lead TitaniumOtherElementsDAluminumEach 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
26、.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 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
27、.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 . . . 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 remainder5154 0.25 0.40 0.10 0.10 3.
28、13.9 0.150.35 0.20 . . 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 remainder6110 0.71.5 0.8 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 remainde
29、r7075 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 otherwise 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
30、 calculated value obtained from analysis shall be rounded to the nearest unit in thelast right-hand place of figures used in expressing the specified limit, in accordance with the rounding-off method of Practice E 29.DOthers includes listed elements for which no specific limit is shown as well as un
31、listed 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 metallic Others elements. Should any analysis by the producer or the purchaserestablish that an Others element exceeds the lim
32、it 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 unspecified metallic elements 0.010 % or more each, rounded to the second decimal before determining the sum.FVanadium 0.05
33、% max.GThe aluminum content is the difference between 100.00 % and the sum of all 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 i
34、nclude vanadium and zirconium.B2110325. Manufacture5.1 The products covered by this specification shall beproduced either by hot extruding and cold finishing or by hotrolling with or without cold finishing, at the option of theproducer.TABLE 2 Mechanical Property LimitsATemperSpecified Diameter orTh
35、ickness, in.Tensile Strength, ksiYield StrengthB(0.2 % offset),min, ksiElonga-tionBin 2 in.or 4 3 Diam-eter, min, %min maxAluminum 1060O 0.124 and under 8.0 . . .0.125 and over 8.0 . 2.5 25H14 0.374 and under 12.0 . 10.0 .H18 0.374 and under 16.0 . 13.0 .Aluminum 1100O 0.124 and under 11.0 15.5 . .0
36、.125 and over 11.0 15.5 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 .F allC.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
37、.0 16T6 and T651 0.3756.500 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 .
38、 35.0 . .0.1258.000 . 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 . 42.0I104.50
39、16.500J62.0 . 40.0 106.5018.000J58.0 . 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 5T62F0.124 and under 60.0 . . .0.1256.500G60.0 . 46.0 5T851D0.5006.5
40、00G66.0 . 58.0 5Alloy 2219T851D0.5002.000 58.0 . 40.0 42.0014.000 57.0 . 39.0 4B211033TABLE 2 ContinuedTemperSpecified Diameter orThickness, in.Tensile Strength, ksiYield StrengthB(0.2 % offset),min, ksiElonga-tionBin 2 in.or 4 3 Diam-eter, min, %min maxAlloy 3003O all 14.0 19.0 5.0 25H12 0.374 and
41、under 17.0 . . .H14 0.374 and under 20.0 . . .H16 0.374 and under 24.0 . . .H18 0.374 and under 27.0 . . .H112 all 14.0 . 5.0 .F allC.C.Alloy 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 . 26.0 .H36 0.12
42、4 and under 37.0 . . .0.1250.374 37.0 . 29.0 .H38 0.374 and under 39.0 . . .F allCC.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 50.0 . . .H
43、18 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 . 11.0 .Allo
44、y 6061EO 0.124 and under . 22.0 . .0.1258.000 . 22.0 . 18T4 and T451D0.124 and under 30.0 . . .0.1258.000H30.0 . 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 .Alloy 6110T9 0.374 and under 65.0 . 63.0
45、 2Alloy 6262T6 and T651D0.1258.000G42.0 . 35.0 10T9 0.1252.000 52.0 . 48.0 52.0013.000 50.0 . 46.0 5Alloy 7075EO 0.124 and under . 40.0 . .0.1258.000 . 40.0 . 10T6, T62 0.124 and under 77.0 . 66.0 .0.1254.000K77.0 . 66.0 7T651 0.124 and under 77.0 . 66.0 .0.1254.000K77.0 . 66.0 74.0016.000 75.0 . 64
46、.0 76.0017.000 73.0 . 62.0 7T73 and T7351D0.124 and under 68.0 . . .0.1254.000 68.0 . 56.0 104.0015.000 66.0 55.0 8B211034TABLE 2 ContinuedTemperSpecified Diameter orThickness, in.Tensile Strength, ksiYield StrengthB(0.2 % offset),min, ksiElonga-tionBin 2 in.or 4 3 Diam-eter, min, %min max5.0016.000
47、 64.0 52.0 8Temper Specified Diameter or Thickness, in. Bend Diameter Factor, NAlloy 2017T4, T42, and T451 0.124 and under 3L0.1258.000H6LAlloy 2024O 0.124 and under 1T351, T4, T42 0.124 and under 30.1256.500 6Alloy 3003O all 0H12 0.374 and under 2H14 0.374 and under 2H16 0.374 and under 8ATo determ
48、ine 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-off method of Practice E 29. The basis for establishment of tensile property l
49、imits is shown in AnnexA1.BThe measurement of yield strength and elongation is not required for wire less than 0.125 in. in thickness or diameter.CThere are no tensile requirements for material in the F temper but it usually can be expected that material 112 in. or less in thickness or diameter (except sections over4 in. in width) will have a strength about equivalent to the H14 or H34 temper. As size increases the strength decreases to nearly that of the O temper.DFor stress-relieve
