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本文(ASTM B221-2012 Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars Rods Wire Profiles and Tubes 《铝和铝合金挤压棒材杆材金属丝型材和管道的标准规格》.pdf)为本站会员(outsidejudge265)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

ASTM B221-2012 Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars Rods Wire Profiles and Tubes 《铝和铝合金挤压棒材杆材金属丝型材和管道的标准规格》.pdf

1、Designation:B22108 Designation: B221 12Standard Specification forAluminum and Aluminum-Alloy Extruded Bars, Rods, Wire,Profiles, and Tubes1This standard is issued under the fixed designation B221; the number immediately following the designation indicates the year oforiginal adoption or, in the case

2、 of revision, the year 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. NoteAppendix and Table

3、X1.1 updated and theyear date was changed on Aug. 8, 2008.1. Scope*1.1 This specification2covers aluminum and aluminum-alloy extruded bars, rods, wire, profiles, and tubes in the aluminumalloys (Note 1) and tempers shown in Table 2.NOTE 1Throughout this specification, the use of the term alloy in th

4、e general sense includes aluminum as well as aluminum alloy.NOTE 2For rolled or cold-finished bar and rod refer to Specification B211, for drawn seamless tube used in pressure applications, Specification B210,for structural pipe and tube, Specification B429/B429M, and for seamless pipe and tube used

5、 in pressure applications, Specification B241/B241M.NOTE 3Structural pipe and tube produced in accordance with B221 is not intended for fluid-carrying applications involving pressure. Refer to eitherSpecification B210 or B241/B241M, as appropriate, for seamless pipe and tube used in fluid-carrying a

6、pplications involving pressure.1.2 Alloy and temper designations are in accordance with ANSI H35.1/H35.1M. The equivalent Unified Numbering Systemalloy designations are those of Table 1 preceded by A9; for example, A91100 for Aluminum 1100 in accordance with PracticeE527.1.3 For acceptance criteria

7、for inclusion of new aluminum and aluminum alloys in this specification, see Annex A2.1.4 A complete metric companion to B221 has been developedB221M; therefore, no metric equivalents are presented in thisspecification.2. Referenced Documents2.1 The following documents of the issue in effect on the

8、date of material purchase, unless otherwise noted, form a part of thisspecification to the extent referenced herein:2.2 ASTM Standards:3B210 Specification for Aluminum and Aluminum-Alloy Drawn Seamless TubesB211 Specification for Aluminum and Aluminum-Alloy Rolled or Cold Finished Bar, Rod, and Wire

9、B241/B241M Specification for Aluminum and Aluminum-Alloy Seamless Pipe and Seamless Extruded TubeB429/B429M Specification for Aluminum-Alloy Extruded Structural Pipe and TubeB557 Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy ProductsB594 Practice for Ultrasonic Insp

10、ection of Aluminum-Alloy Wrought Products for Aerospace ApplicationsB660 Practices for Packaging/Packing of Aluminum and Magnesium ProductsB666/B666M Practice for Identification Marking of Aluminum and Magnesium ProductsB807/B807M Practice for Extrusion Press Solution Heat Treatment for Aluminum All

11、oysB881 Terminology Relating to Aluminum- and Magnesium-Alloy ProductsB918 Practice for Heat Treatment of Wrought Aluminum AlloysB945 Practice for Aluminum Alloy Extrusions Press Cooled from an Elevated Temperature Shaping Process for Production ofT1, T2, T5 and T10Type TempersE29 Practice for Using

12、 Significant Digits in Test Data to Determine Conformance with SpecificationsE34 Test Methods for Chemical Analysis of Aluminum and Aluminum-Base Alloys E55Practice for Sampling Wrought1This specification is under the jurisdiction of ASTM Committee B07 on Light Metals and Alloys and is the direct re

13、sponsibility of Subcommittee B07.03 on AluminumAlloy Wrought Products.Current edition approvedAug. 8, 2008. PublishedAugust 2008. Originally approved in 1947. Last previous edition approved in 2006 as B22106. DOI: 10.1520/B0221-08.Current edition approved Jan. 15, 2012. Published March 2012. Origina

14、lly approved in 1947. Last previous edition approved in 2008 as B221 08. DOI:10.1520/B0221-12.2For ASME Boiler and Pressure Vessel Code applications see related Specification SB-221 in Section 11II of this Code.3For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Cus

15、tomer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page on the ASTM website.1This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to

16、the previous version. Becauseit may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current versionof the standard as published by ASTM is to be considered the official document.*A Summar

17、y 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.TABLE 1 Chemical Composition LimitsA,B,CNOTE 1In case of a discrepancy between the values listed in Table 2 and those listed in t

18、he “International Alloy Designations and ChemicalComposition Limits for Wrought Aluminum and Wrought Aluminum Alloys” (known as the “Teal Sheets”), the composition limits registered with theAluminum Association and published in the “Teal Sheets” should be considered the controlling composition. The

19、“Teal Sheets” are available athttp:/www.aluminum.org/tealsheets.Alloy Silicon Iron CopperManga-neseMagne-siumChromium Zinc Titanium VanadiumOther ElementsDAluminumEach TotalE1060 0.25 0.35 0.05 0.03 0.03 . 0.05 0.03 0.05 0.03 . 99.60 minF1100 0.95 Si + Fe 0.050.20 0.05 . . 0.10 . . 0.05 0.15 99.00 m

20、inF1100 0.95 Si + Fe 0.050.20 0.05 . . 0.10 . . 0.05G0.15 99.00 minF2014 0.501.2 0.7 3.95.0 0.401.2 0.200.8 0.10 0.25 0.15G. 0.05G0.15 remainder2014 0.501.2 0.7 3.95.0 0.401.2 0.200.8 0.10 0.25 0.15H. 0.05H0.15 remainder2024 0.50 0.50 3.84.9 0.300.9 1.21.8 0.10 0.25 0.15G. 0.05G0.15 remainder2024 0.

21、50 0.50 3.84.9 0.300.9 1.21.8 0.10 0.25 0.15H. 0.05H0.15 remainder2219 0.20 0.30 5.86.8 0.200.40 0.02 . 0.10 0.020.10 0.050.15 0.05H0.15Hremainder2219 0.20 0.30 5.86.8 0.200.40 0.02 . 0.10 0.020.10 0.050.15 0.05I0.15Iremainder3003 0.6 0.7 0.050.20 1.01.5 . . 0.10 . . 0.05 0.15 remainderAlclad 3003 .

22、 3003 Clad with 7072 alloy . . . . . . . .3004 0.30 0.7 0.25 1.01.5 0.81.3 . 0.25 . . 0.05 0.15 remainder3102 0.40 0.7 0.10 0.050.40 . . 0.30 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 remainder5083 0.40 0.40 0.10 0.401.0 4.04.9 0.050.25 0.25 0.15 . 0.05 0.

23、15 remainder5086 0.40 0.50 0.10 0.200.7 3.54.5 0.050.25 0.25 0.15 . 0.05 0.15 remainder5154 0.25 0.40 0.10 0.10 3.13.9 0.150.35 0.20 0.20 . 0.05 0.15 remainder5154 0.25 0.40 0.10 0.10 3.13.9 0.150.35 0.20 0.20 . 0.05G0.15 remainder5454 0.25 0.40 0.10 0.501.0 2.43.0 0.050.20 0.25 0.20 . 0.05 0.15 rem

24、ainder5456 0.25 0.40 0.10 0.501.0 4.75.5 0.050.20 0.25 0.20 . 0.05 0.15 remainder6005 0.60.9 0.35 0.10 0.10 0.400.6 0.10 0.10 0.10 . 0.05 0.15 remainder6005A 0.500.9 0.35 0.30 0.50I0.400.7 0.30I0.20 0.10 . 0.05 0.15 remainder6005A 0.500.9 0.35 0.30 0.50J0.400.7 0.30J0.20 0.10 . 0.05 0.15 remainder60

25、20K0.40-0.9 0.50 0.30-0.9 0.35 0.6-1.2 0.15 0.20 0.15 0.05 0.15 remainder6041L0.50-0.9 0.15-0.7 0.15-0.6 0.05-0.20 0.8-1.2 0.05-0.15 0.25 0.15 0.05 0.15 remainder6042M0.50-1.2 0.7 0.20-0.6 0.40 0.7-1.2 0.04-0.35 0.25 0.15 0.05 0.15 remainder6060 0.300.6 0.100.30 0.10 0.10 0.350.6 0.5 0.15 0.10 . 0.0

26、5 0.15 remainder6061J0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.35 0.25 0.15 . 0.05 0.15 remainder6061N0.400.8 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 remainder6064O0.40-0.8 0.7 0.15-0.40 0.15 0.8-1.2 0.05-0.14 0.25

27、0.15 0.05 0.15 remainder6066 0.91.8 0.50 0.71.2 0.61.1 0.81.4 0.40 0.25 0.20 . 0.05 0.15 remainder6070 1.01.7 0.50 0.150.40 0.401.0 0.501.2 0.10 0.25 0.15 . 0.05 0.15 remainder6082 0.71.3 0.50 0.10 0.401.0 0.61.2 0.25 0.20 0.10 . 0.05 0.15 remainder6105 0.61.0 0.35 0.10 0.15 0.450.8 0.10 0.10 0.10 .

28、 0.05 0.15 remainder6162 0.400.8 0.50 0.20 0.10 0.71.1 0.10 0.25 0.10 . 0.05 0.15 remainder6262 0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.14 0.25 0.15 . 0.05K0.15Kremainder6262 0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.14 0.25 0.15 . 0.05P0.15Premainder6351 0.71.3 0.50 0.10 0.400.8 0.400.8 . 0.20 0.20 . 0

29、.05 0.15 remainder6360 0.35-0.8 0.10-0.30 0.15 0.02-0.15 0.25-0.45 0.05 0.10 0.10 . 0.05 0.15 remainder6463 0.200.6 0.15 0.20 0.05 0.450.9 . 0.05 . . 0.05 0.15 remainder6560 0.300.7 0.100.30 0.050.20 0.20 0.200.6 0.05 0.15 0.10 . 0.05 0.15 remainder7005 0.35 0.40 0.10 0.200.7 1.01.8 0.060.20 4.05.0

30、0.010.06 . 0.05L0.15Lremainder7005 0.35 0.40 0.10 0.200.7 1.01.8 0.060.20 4.05.0 0.010.06 . 0.05Q0.15Qremainder7072M0.7 Si + Fe 0.10 0.10 0.10 . 0.81.3 . . remainder7072R0.7 Si + Fe 0.10 0.10 0.10 . 0.81.3 . . remainder7075 0.40 0.50 1.22.0 0.30 2.12.9 0.180.28 5.16.1 0.20N. 0.05N0.15 remainder7075

31、0.40 0.50 1.22.0 0.30 2.12.9 0.180.28 5.16.1 0.20S. 0.05S0.15 remainder7116 0.15 0.30 0.501.1 0.05 0.81.4 . 4.25.2 0.05 0.05 0.05O0.15 remainder7116 0.15 0.30 0.501.1 0.05 0.81.4 . 4.25.2 0.05 0.05 0.05T0.15 remainder7129 0.15 0.30 0.500.9 0.10 1.32.0 0.10 4.25.2 0.05 0.05 0.05O0.15 remainder7129 0.

32、15 0.30 0.500.9 0.10 1.32.0 0.10 4.25.2 0.05 0.05 0.05T0.15 remainder7178 0.40 0.50 1.62.4 0.30 2.43.1 0.180.28 6.37.3 0.20 . 0.05 0.15 remainderALimits are in weight percent maximum unless shown as a range, or stated otherwise.BAnalysis shall be made for the elements for which limits are shown in t

33、his table.CFor the purpose of determining conformance to these limits, an observed value or a calculated value obtained from analysis shall be rounded to the nearest unit inthe last right-hand place of the figures used in expressing the specified limit, in accordance with the rounding-off method of

34、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 is not required and may not cover all metallic Others elements. Shou

35、ld 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 considerednonconforming.EOther ElementsTotal shall be the sum of unspecified metallic elements

36、 0.010 % or more, rounded to the second decimal before determining the sum.FThe 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 before determining the sum.GBe 0.0003 max for weld

37、ing electrode, welding rod, and filler wire.HUpon agreement between the purchaser and the producer or supplier, a Zr + Ti limit of 0.20 % max is permitted. Properties in Specification (Table 2) are not basedon the Zirconium and Titanium algorithm.HIZirconium, 0.100.25 %. The total for other elements

38、 does not include zirconium.IJManganese plus chromium shall total 0.120.50.JKLead 0.05 % max, Tin 0.9-1.5 %.LBismuth 0.30-0.9 %, Tin 0.35-1.2 %.MBismuth 0.20-0.8 % Lead 0.15-0.40 %.NIn 1965 the requirements for 6062 were combined with those for 6061 by revising the minimum chromium from “0.15 %” to“

39、 0.04 %.” This action cancelled alloy 6062.KOBismuth 0.50-0.7 %, Lead 0.20-0.40 %,PBismuth and lead shall be 0.400.7 % each.B221 122Nonferrous Metals and Alloys for De-termination of Chemical CompositionE527 Practice for Numbering Metals and Alloys in the Unified Numbering System (UNS)E607 Test Meth

40、od for Atomic Emission Spectrometric Analysis Aluminum Alloys by the Point to Plane Technique NitrogenAtmosphereTABLE 2 Mechanical Property LimitsA,BNOTE 1Strength values shown in parentheses are for information only.TemperSpecified Sectionor WallThickness, in.Area, in.2Tensile Strength,ksiYield Str

41、ength(0.2 % offset), ksiElongation in2 in. or 4 3Diameter,min, %C,Dmin max min maxAluminum 1060EAluminum 1060DO all all 8.5 14.0 2.5 . . . 25H112 all all 8.5 . . . 2.5 . . . 25Aluminum 1100EAluminum 1100DO all all 11.0 15.5 3.0 . . . 25H112 all all 11.0 . . . 3.0 . . . 25Alloy 2014EAlloy 2014DO all

42、all . . . 30.0 . . . 18.0 12T4JB0221-08_1T4JB0221-12_1T4510Fall all 50.0 . 35.0 . 12T4510Eall all 50.0 . 35.0 . 12T4511FT4511ET42Gall all 50.0 . 29.0 . 12T42Fall all 50.0 . 29.0 . 12T66B0221-08_25B0221-08_3up through 0.499 all 60.0 . 53.0 . 7T66B0221-12_25B0221-12_3up through0.499all 60.0 . 53.0 . 7

43、T6510F0.5000.749 all 64.0 . 58.0 . 7T6510E0.5000.749 all 64.0 . 58.0 . 7T6511FH B0221-08_4up through 25 68.0 . 60.0 . 7T6511EH B0221-12_4upthrough2568.0 . 60.0 . 70.750andoverover 25 through 32 68.0 . . . 58.0 . . . 6HB0221-08_5up through 0.749 all 60.0 . 53.0 . 7HB0221-12_5upthrough0.749all 60.0 .

44、53.0 . 7T62GHB0221-08_6up through2560.0 . 53.0 . 7T62FHB0221-12_6up through2560.0 . 53.0 . 70.750 and overover 25 through3260.0 . . . 53.0 . . . 6Alloy 2024EAlloy 2024DO all all . . . 35.0 . . . 19.0 125B0221-08_7up through 0.249 all 57.0 . 42.0 . 12H5B0221-12_7upthrough0.249all 57.0 . 42.0 . 12GT3J

45、B0221-08_80.2500.749 all 60.0 . 44.0 . 12HT3JB0221-12_80.2500.749 all 60.0 . 44.0 . 12GT3510F0.7501.499 all 65.0 . 46.0 . 10T3510E0.7501.499 all 65.0 . 46.0 . 10B221 123TABLE 2 ContinuedTemperSpecified Sectionor WallThickness, in.Area, in.2Tensile Strength,ksiYield Strength(0.2 % offset), ksiElongat

46、ion in2 in. or 4 3Diameter,min, %C,Dmin max min maxT3511FH B0221-08_9up through 25 70.0 . 52.0I. 10T3511EH B0221-12_9upthrough2570.0 . 52.0H. 101.500 and over over25through3268.0 . 48.0J. 81.500 and over over 25 through 3268.0 . 48.0I. 8HB0221-08_10up through 0.749 all 57.0 . 38.0 . 12HB0221-12_10up

47、through0.749all 57.0 . 38.0 . 120.7501.499 all 57.0 . . . 38.0 . . . 10T42G1.500 and overH B0221-08_11up through 25 57.0 . 38.0 . 10T42F1.500 and overH B0221-12_11up through 25 57.0 . 38.0 . 10over 25 through3257.0 . . . 38.0 . . . 8T81HB0221-08_120.0500.249 all 64.0 . 56.0 . 4T81HB0221-12_120.0500.

48、249 all 64.0 . 56.0 . 4T8510F0.2501.499 all 66.0 . 58.0 . 5T8510E0.2501.499 all 66.0 . 58.0 . 5T8511F1.500 and over upthrough3266.0 . 58.0 . 5T8511E1.500 and over upthrough3266.0 . 58.0 . 5Alloy 2219EAlloy 2219DO all all . . . 32.0 . . . 18.0 12T31T3510FH B0221-08_13up through 0.499 up through 25 42

49、.0 . 26.0 . 14T3510EH B0221-12_13upthrough0.499up through2542.0 . 26.0 . 14T3511F0.5002.999 up through 25 45.0 . 27.0 . 14T3511E0.5002.999 upthrough2545.0 . 27.0 . 14T62GH B0221-08_14up through 0.999 up through 25 54.0 . 36.0 . 6T62FH B0221-12_14upthrough0.999up through2554.0 . 36.0 . 61.000 and over up through 25 54.0 . . . 36.0 . . . 6T81JB0221-08_15T81JB0221-12_15T8510Fupthrough2.999up through2558.0 . 42.0 . 6T8

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