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本文(ASTM B209M-2010 Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate (Metric)《铝及铝合金板材的标准规范(米制)》.pdf)为本站会员(diecharacter305)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 B209M-2010 Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate (Metric)《铝及铝合金板材的标准规范(米制)》.pdf

1、Designation: B209M 10Standard Specification forAluminum and Aluminum-Alloy Sheet and Plate (Metric)1This standard is issued under the fixed designation B209M; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revisio

2、n. 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 specification covers aluminum and aluminum

3、alloyflat sheet, coiled sheet, and plate in the alloys (Note 1) andtempers shown in Tables 2 and 3, and in the following finishes:1.1.1 Plate in all alloys and sheet in heat-treatable alloys:mill finish.1.1.2 Sheet in nonheat-treatable alloys: mill finish, one-sidebright mill finish, standard one-si

4、de bright finish, and standardtwo-sides bright finish.1.2 Alloy and temper designations are in accordance withANSI H35.1/H35.1(M). The equivalent Unified NumberingSystem (UNS) alloy designations are those of Table 1 precededby A9, for example, A91100 for aluminum 1100 in accordancewith Practice E527

5、.NOTE 1Throughout this specification, use of the term alloy in thegeneral sense includes aluminum as well as aluminum alloy.NOTE 2See Specification B632/B632M for Tread Plate.NOTE 3See Specification B928/B928M for 5xxx-H116 and 5xxx-H321 aluminum alloys containing 3 % or more nominal magnesium andin

6、tended for marine service and similar environments. Other alloy-temperproducts listed in Specification B209, which do not require the additionalcorrosion testing/capability called out in Specification B928/B928M, maybe suitable for marine and similar environment applications.1.3 This specification i

7、s the SI companion to SpecificationB209.1.4 For acceptance criteria for inclusion of new aluminumand aluminum alloys in this specification, see Annex A2.2. Referenced Documents2.1 The following documents form a part of this specifica-tion to the extent referenced herein:2.2 ASTM Standards:2B209 Spec

8、ification for Aluminum and Aluminum-AlloySheet and PlateB548 Test Method for Ultrasonic Inspection of Aluminum-Alloy Plate for Pressure VesselsB557M Test Methods for Tension Testing Wrought and CastAluminum- and Magnesium-Alloy Products (Metric)B594 Practice for Ultrasonic Inspection of Aluminum-All

9、oy Wrought Products for Aerospace ApplicationsB632/B632M Specification for Aluminum-Alloy RolledTread PlateB660 Practices for Packaging/Packing of Aluminum andMagnesium ProductsB666/B666M Practice for Identification Marking of Alumi-num and Magnesium ProductsB881 Terminology Relating toAluminum- and

10、 Magnesium-Alloy ProductsB918 Practice for Heat Treatment of Wrought AluminumAlloysB928/B928M Specification for High MagnesiumAluminum-Alloy Sheet and Plate for Marine Service andSimilar EnvironmentsB947 Practice for Hot Rolling Mill Solution Heat Treatmentfor Aluminum Alloy PlateE29 Practice for Us

11、ing 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 for Duc-tilityE527 Practice for Numbering Metals and Alloys in theUnified Numbering System (UNS)E607

12、 Test Method for Atomic Emission SpectrometricAnalysis Aluminum Alloys by the Point to Plane Tech-nique Nitrogen AtmosphereE716 Practices for Sampling and Sample Preparation ofAluminum and Aluminum Alloys for Determination ofChemical Composition by Spectrochemical AnalysisE1004 Test Method for Deter

13、mining Electrical Conductiv-ity Using the Electromagnetic (Eddy-Current) MethodE1251 Test Method for Analysis of Aluminum and Alumi-num Alloys by Spark Atomic Emission Spectrometry1This specification is under the jurisdiction of ASTM Committee B07 on LightMetals and Alloys and is the direct responsi

14、bility of Subcommittee B07.03 onAluminum Alloy Wrought Products.Current edition approved Nov. 1, 2010. Published July 2011. Originally approvedin 1978. Last previous edition approved in 2007 as B209M 07. DOI: 10.1520/B0209M-10.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orc

15、ontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document 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, W

16、est Conshohocken, PA 19428-2959, United States.G34 Test Method for Exfoliation Corrosion Susceptibilityin 2XXX and 7XXX Series Aluminum Alloys (EXCOTest)G47 Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXXAluminumAlloyProducts2.3 ISO Standards:3ISO209-1 Wrough

17、t Aluminum and Aluminum Alloys-Chemical Composition and Forms of Product3Available from American National Standards Institute (ANSI), 25 W. 43rd St.,4th Floor, New York, NY 10036, http:/www.ansi.org.TABLE 1 Chemical Composition LimitsA,B,CNOTEIn case there is a discrepancy in the values listed in Ta

18、ble 1 with those listed in the “InternationalAlloy Designations and Chemical CompositionLimits for Wrought Aluminum and Wrought Aluminum Alloys” (known as the “Teal Sheets”), the composition limits registered with the AluminumAssociation and published in the “Teal Sheets” should be considered the co

19、ntrolling composition. The “Teal Sheets” are available at http:/www.aluminum.org/tealsheets.Alloy Silicon Iron Copper Manganese Magnesium Chromium Zinc TitaniumOther ElementsDAluminumEach 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

20、 0.15 99.00 minG1230H0.70 Si + Fe 0.10 0.05 0.05 . 0.10 0.03 0.03F. 99.30 minG2014 0.501.2 0.7 3.95.0 0.401.2 0.200.8 0.10 0.25 0.15 0.05 0.15 remainderAlclad 2014 2014 clad with 6003 alloy2024 0.50 0.50 3.84.9 0.300.9 1.21.8 0.10 0.25 0.15 0.05 0.15 remainderAlclad 2024 2024 clad with 1230 alloy212

21、4 0.20 0.30 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 0.05I0.15IremainderAlclad 2219 2219 clad with 7072 alloy3003 0.6 0.7 0.050.20 1.01.5 . . 0.10 . 0.05 0.15 remainderAlclad 3003 3003 clad with 7072 alloy3004 0.30 0.7 0.25 1.01.5 0.

22、81.3 . 0.25 . 0.05 0.15 remainderAlclad 3004 3004 clad with 7072 alloy3005 0.6 0.7 0.30 1.01.5 0.200.6 0.10 0.25 0.10 0.05 0.15 remainder3105 0.6 0.7 0.30 0.300.8 0.200.8 0.20 0.40 0.10 0.05 0.15 remainder500550100.300.400.70.70.200.250.200.100.300.501.10.200.60.100.150.250.30.0.100.050.050.150.15re

23、mainderremainder5050 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 remainder5059 0.45 0.50 0.25 0.61.2 5.06.0 0.25 0.400.9 0.20 0.05J0.15 remainder5083 0.40 0.40 0.10 0.401.0 4.04.9 0.050.25 0.25 0.15 0.05 0.15 remainder5086 0.40 0

24、.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 remainder5252 0.08 0.10 0.10 0.10 2.22.8 . 0.05 . 0.03F0.10Fremainder5254 0.45 Si + Fe 0.05 0.01 3.13.9 0.150.35 0.20 0.05 0.05 0.15 remainder5454 0.25 0.40 0.10 0.501.0 2.43.0

25、0.050.20 0.25 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 remainder5457 0.08 0.10 0.20 0.150.45 0.81.2 . 0.05 . 0.03F0.10Fremainder5657 0.08 0.10 0.10 0.03 0.61.0 . 0.05 . 0.02K0.05Kremainder5754 0.40 0.40 0.10 0.50L2.6-3.6 0.30L0.20 0.15 0.05 0.15 remaind

26、er6003H0.351.0 0.6 0.10 0.8 0.81.5 0.35 0.20 0.10 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 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 remainderAlclad 6061 6061 clad with 7072 alloy7072H0.7 Si + Fe 0.10 0.10 0.10 . 0.81.3 . 0.

27、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 remainderAlclad 7075 7075 clad with 7072 alloyALimits are in mass percent maximum unless shown as a range or stated otherwise.BAnalysis shall be made for the elements for which limits are shown in this table.CFor purpo

28、ses of determining conformance to these limits, an observed value or a calculated value attained from analysis shall be rounded to the nearestunitinthelast right hand place of figures used in expressing the specified limit, in accordance with the Rounding Method of Practice E29.DOthers includes list

29、ed 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. Should any analysis by the producer or

30、 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. The Total for Other Elements does not include elements shown in the footnotes with specific compositio

31、n limits.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. The total for other elements does not include vanadium.GThe aluminum content shall be calculated by subtracting from 100.00 %

32、the sum of all metallic elements present in amounts of 0.010 % or more each, roundedtothesecond decimal before determining the sum.HComposition of cladding alloy as applied during the course of manufacture. Samples from finished sheet or plate shall not be required to conform to these limits.IVanadi

33、um, 0.050.15, zirconium, 0.100.25.J0.050.25 Zr.KGallium 0.03 max, vanadium 0.05 max.L0.10-0.6 Mn + Cr.B209M 102TABLE 2 Mechanical Property Limits for Nonheat-Treatable AlloysA,BAlloy TemperSpecified Thickness,mmTensile Strength,MPaYield Strength(0.2 % offset), MPaElongation,min, %C BendDiameterFacto

34、r, Nover through min max min max in 50 mmin 53Diameter1060 O 0.15 0.32 55 95 15 . 15 . .1060 O 0.32 0.63 55 95 15 . 18 . .1060 O 0.63 1.20 55 95 15 . 23 . .1060 O 1.20 6.30 55 95 15 . 25 . .1060 O 6.30 80.00 55 95 15 . 25 22 .1060 H12Dor H22D0.40 0.63 75 110 60 . 6 . .1060 H12Dor H22D0.63 1.20 75 11

35、0 60 . 7 . .1060 H12Dor H22D1.20 6.30 75 110 60 . 12 . .1060 H12Dor H22D6.30 50.00 75 110 60 . 12 10 .1060 H14Dor H24D0.20 0.32 85 120 70 . 1 . .1060 H14Dor H24D0.32 0.63 85 120 70 . 2 . .1060 H14Dor H24D0.63 1.20 85 120 70 . 6 . .1060 H14Dor H24D1.20 6.30 85 120 70 . 10 . .1060 H14Dor H24D6.30 25.0

36、0 85 120 70 . 10 9 .1060 H16Dor H26D0.15 0.32 95 130 75 . 1 . .1060 H16Dor H26D0.32 0.63 95 130 75 . 2 . .1060 H16Dor H26D0.63 1.20 95 130 75 . 4 . .1060 H16Dor H26D1.20 4.00 95 130 75 . 5 . .1060 H18Dor H28D0.15 0.32 110 . 85 . 1 . .1060 H18Dor H28D0.32 0.63 110 . 85 . 2 . .1060 H18Dor H28D0.63 1.2

37、0 110 . 85 . 3 . .1060 H18Dor H28D1.20 3.20 110 . 85 . 4 . .1060 H112 6.30 12.50 75 . . . 10 . .1060 H112 12.50 40.00 70 . . . . 18 .1060 H112 40.00 80.00 60 . . . . 22 .1060 FE6.30 80.00 . . . . . . .1100 O 0.15 0.32 75 105 25 . 15 . 01100 O 0.32 0.63 75 105 25 . 17 . 01100 O 0.63 1.20 75 105 25 .

38、22 . 01100 O 1.20 6.30 75 105 25 . 30 . 01100 O 6.30 80.00 75 105 25 . 28 25 01100 H12Dor H22D0.40 0.63 95 130 75 . 3 . 01100 H12Dor H22D0.63 1.20 95 130 75 . 5 . 01100 H12Dor H22D1.20 6.30 95 130 75 . 8 . 01100 H12Dor H22D6.30 12.50 95 130 75 . 10 9 01100 H12Dor H22D12.50 50.00 95 130 75 . 10 9 .11

39、00 H14Dor H24D0.20 0.32 110 145 95 . 1 . 01100 H14Dor H24D0.32 0.63 110 145 95 . 2 . 01100 H14Dor H24D0.63 1.20 110 145 95 . 3 . 01100 H14Dor H24D1.20 6.30 110 145 95 . 5 . 01100 H14Dor H24D6.30 25.00 110 145 95 . 7 6 01100 H16Dor H26D0.15 0.32 130 165 115 . 1 . 41100 H16Dor H26D0.32 0.63 130 165 11

40、5 . 2 . 41100 H16Dor H26D0.63 1.20 130 165 115 . 3 . 41100 H16Dor H26D1.20 4.00 130 165 115 . 4 . 41100 H18Dor H28D0.15 0.32 150 . . . 1 . .1100 H18Dor H28D0.32 0.63 150 . . . 1 . .1100 H18Dor H28D0.63 1.20 150 . . . 2 . .1100 H18Dor H28D1.20 3.20 150 . . . 4 . .1100 H112 6.30 12.50 90 . 50 . 9 . .1

41、100 H112 12.50 40.00 85 . 40 . . 12 .1100 H112 40.00 80.00 80 . 30 . . 18 .1100 FE6.30 80.00 . . . . . . .3003 O 0.15 0.20 95 130 35 . 14 . 03003 O 0.20 0.32 95 130 35 . 18 . 03003 O 0.32 0.63 95 130 35 . 20 . 03003 O 0.63 1.20 95 130 35 . 23 . 03003 O 1.20 6.30 95 130 35 . 25 . 03003 O 6.30 80.00 9

42、5 130 35 . 23 21 .3003 H12Dor H22D0.40 0.63 120 160 85 . 3 . 03003 H12Dor H22D0.63 1.20 120 160 85 . 4 . 03003 H12Dor H22D1.20 6.30 120 160 85 . 6 . 03003 H12Dor H22D6.30 50.00 120 160 85 . 9 8 .3003 H14Dor H24D0.20 0.32 140 180 115 . 1 . 03003 H14Dor H24D0.32 0.63 140 180 115 . 2 . 03003 H14Dor H24

43、D0.63 1.20 140 180 115 . 3 . 0B209M 103TABLE 2 ContinuedAlloy TemperSpecified Thickness,mmTensile Strength,MPaYield Strength(0.2 % offset), MPaElongation,min, %C BendDiameterFactor, Nover through min max min max in 50 mmin 53Diameter3003 H14Dor H24D1.20 3.20 140 180 115 . 5 . 03003 H14Dor H24D3.20 6

44、.30 140 180 115 . 5 . 23003 H14Dor H24D6.30 25.00 140 180 115 . 8 7 .3003 H16Dor H26D0.15 0.32 165 205 145 . 1 . 43003 H16Dor H26D0.32 0.63 165 205 145 . 2 . 43003 H16Dor H26D0.63 1.20 165 205 145 . 3 . 43003 H16Dor H26D1.20 4.00 165 205 145 . 4 . 63003 H18Dor H28D0.15 0.32 185 . 165 . 1 . .3003 H18

45、Dor H28D0.32 0.63 185 . 165 . 1 . .3003 H18Dor H28D0.63 1.20 185 . 165 . 2 . .3003 H18Dor H28D1.20 3.20 185 . 165 . 4 . .3003 H112 6.30 12.50 115 . 70 . 8 . .3003 H112 12.50 40.00 105 . 40 . . 10 .3003 H112 40.00 80.00 100 . 40 . . 16 .3003 FF6.30 80.00 . . . . . . .Alclad 3003 O 0.15 0.32 90 125 30

46、 . 14 . .Alclad 3003 O 0.32 0.63 90 125 30 . 20 . .Alclad 3003 O 0.63 1.20 90 125 30 . 22 . .Alclad 3003 O 1.20 6.30 90 125 30 . 25 . .Alclad 3003 O 6.30 12.50 90 125 30 . 23 . .Alclad 3003 O 12.50 80.00 95F130F35F. . 21 .Alclad 3003 H12Dor H22D0.40 0.63 115 155 80 . 4 . .Alclad 3003 H12Dor H22D0.63

47、 1.20 115 155 80 . 5 . .Alclad 3003 H12Dor H22D1.20 6.30 115 155 80 . 6 . .Alclad 3003 H12Dor H22D6.30 12.50 115 155 80 . 9 . .Alclad 3003 H12Dor H22D12.50 50.00 120F160F85F. . 8 .Alclad 3003 H14Dor H24D0.20 0.32 135 175 110 . 1 . .Alclad 3003 H14Dor H24D0.32 0.63 135 175 110 . 2 . .Alclad 3003 H14D

48、or H24D0.63 1.20 135 175 110 . 3 . .Alclad 3003 H14Dor H24D1.20 6.30 135 175 110 . 5 . .Alclad 3003 H14Dor H24D6.30 12.50 135 175 110 . 8 . .Alclad 3003 H14Dor H24D12.50 25.00 140F180F115F. . 7 .Alclad 3003 H16Dor H26D0.15 0.32 160 200 140 . 1 . .Alclad 3003 H16Dor H26D0.32 0.63 160 200 140 . 2 . .A

49、lclad 3003 H16Dor H26D0.63 1.20 160 200 140 . 3 . .Alclad 3003 H16Dor H26D1.20 4.00 160 200 140 . 4 . .Alclad 3003 H18 0.15 0.32 180 . . . 1 . .Alclad 3003 H18 0.32 0.63 180 . . . 1 . .Alclad 3003 H18 0.63 1.20 180 . . . 2 . .Alclad 3003 H18 1.20 3.20 180 . . . 4 . .Alclad 3003 H112 6.30 12.50 110 . 65 . 8 . .Alclad 3003 H112 12.50 40.00 105F. 40F. . 10 .Alclad 3003 H112 40.00 80.00 100F. 40F. . 16 .Alclad 3003 FE6.30 80.00 . . . . . . .3004 O 0.15 0.32 150 200 60 . 9 . 03004 O 0.32 0.63 150 200 60 . 12 .

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