ASTM B209M-2007 Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate [Metric]《铝和铝合金薄板材和板材(米制)的标准规范》.pdf

《ASTM B209M-2007 Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate [Metric]《铝和铝合金薄板材和板材(米制)的标准规范》.pdf》由会员分享，可在线阅读，更多相关《ASTM B209M-2007 Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate [Metric]《铝和铝合金薄板材和板材(米制)的标准规范》.pdf（31页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: B 209M 07METRICStandard Specification forAluminum and Aluminum-Alloy Sheet and Plate Metric1This standard is issued under the fixed designation B 209M; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last r

2、evision. 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 and al

3、uminum 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

4、 one-side 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 Practi

5、ce E 527.NOTE 1Throughout this specification, use of the term alloy in thegeneral sense includes aluminum as well as aluminum alloy.NOTE 2See Specification B 632/B 632M for Tread Plate.NOTE 3See Specification B 928/B 928M for 5xxx-H116 and 5xxx-H321 aluminum alloys containing 3 % or more nominal mag

6、nesium andintended for marine service and similar environments. Other alloy-temperproducts listed in Specification B 209, which do not require the additionalcorrosion testing/capability called out in Specification B 928/B 928M,may be suitable for marine and similar environment applications.1.3 This

7、specification is the metric counterpart of Specifi-cation B 209.1.4 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 A

8、STM Standards:2B 209 Specification for Aluminum and Aluminum-AlloySheet and PlateB 548 Test Method for Ultrasonic Inspection of Aluminum-Alloy Plate for Pressure VesselsB 557M Test Methods for Tension Testing Wrought andCast Aluminum- and Magnesium-Alloy Products MetricB 594 Practice for Ultrasonic

9、Inspection of Aluminum-Alloy Wrought Products for Aerospace ApplicationsB 632/B 632M Specification for Aluminum-Alloy RolledTread PlateB 660 Practices for Packaging/Packing of Aluminum andMagnesium ProductsB 666/B 666M Practice for Identification Marking of Alu-minum and Magnesium ProductsB 881 Term

10、inology Relating to Aluminum- andMagnesium-Alloy ProductsB 918 Practice for Heat Treatment of Wrought AluminumAlloysB 928/B 928M Specification for High MagnesiumAluminum-Alloy Sheet and Plate for Marine Service andSimilar EnvironmentsB 947 Practice for Hot Rolling Mill Solution Heat Treat-ment for A

11、luminum Alloy PlateE29 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 Metals andAlloys for Determination of Chemical CompositionE 290 Te

12、st Methods for Bend Testing of Material forDuctilityE 527 Practice for Numbering Metals and Alloys (UNS)E 607 Test Method for Atomic Emission SpectrometricAnalysis Aluminum Alloys by the Point to Plane Tech-nique Nitrogen AtmosphereE 716 Practices for Sampling Aluminum and AluminumAlloys for Spectro

13、chemical AnalysisE 1004 Practice for Determining Electrical ConductivityUsing the Electromagnetic (Eddy-Current) Method1This 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 Produc

14、ts.Current edition approved Aug. 1, 2007. Published August 2007. Originallyapproved in 1978. Last previous edition approved in 2006 as B 209M 06.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards

15、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, West Conshohocken, PA 19428-2959, United States.E 1251 Test Method for Analysis of

16、Aluminum and Alumi-num Alloys by Atomic Emission SpectrometryG34Test Method for Exfoliation Corrosion Susceptibilityin 2xxx and 7xxx Series Aluminum Alloys (EXCO Test)G47Test Method for Determining Susceptibilioty toStress-Corrosion Cracking of 2xxx and 7xxx AluminumAlloy Products2.3 ISO Standards:3

17、ISO209-1 Wrought 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,CAlloy Silicon Iron CopperManga-neseMagne-siumC

18、hro-miumZincTita-niumOther ElementsDAlumi-numEach 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 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

19、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 alloy2124 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 0.05I0.15Iremainde

20、rAlclad 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 0.81.3 . 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 remainder3

21、105 0.6 0.7 0.30 0.300.8 0.200.8 0.20 0.40 0.10 0.05 0.15 remainder500550100.300.400.70.70.200.250.200.100.300.501.10.200.60.100.150.250.30.0.100.050.050.150.15remainderremainder5050 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 re

22、mainder5059 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 0.50 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

23、.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 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 0.150.4

24、5 0.81.2 . 0.05 . 0.03F0.10Fremainder5652 0.40 Si + Fe 0.04 0.01 2.22.8 0.150.35 0.10 . 0.05 0.15 remainder5657 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 remainder6003H0.351.0 0.6 0.10 0.8 0.81.5 0.35 0.20 0.10 0.05 0.15 remainde

25、r6013 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 alloy7008H0.10 0.10 0.05 0.05 0.71.4 0.120.25 4.55.5 0.05 0.05 0.10 remainder7072H0.7 Si + Fe 0.10 0.10 0.10 . 0.81.3

26、. 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 remainderAlclad 7075 7075 clad with 7072 alloy7008 Alclad 7075 7075 clad with 7008 alloy7178 0.40 0.50 1.62.4 0.30 2.43.1 0.180.28 6.37.3 0.20 0.05 0.15 remainderAlclad 7178 7178 clad with 7072 alloyALimits are in

27、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 purposes of determining conformance to these limits, an observed value or a calculated value attained from analysis shall be rounded to the nearestu

28、nitinthelast righthand place of figures used in expressing the specified limit, in accordance with the Rounding 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 nots

29、pecified 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 exceeds the limit of T

30、otal, the material shall be considerednon-conforming.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

31、 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.HComposition of cladding alloy as applied during the course of manufacture. Samples from finished sheet or plate shall not be

32、 required to conform to these limits.IVanadium, 0.050.15, zirconium, 0.100.25. The total for other elements does not include vanadium and zirconium.J0.050.25 Zr.KGallium 0.03 max, vanadium 0.05 max. The total for other elements does not include vanadium and gallium.L0.10-0.6 Mn + Cr.B209M072ISO2107

33、Aluminum, Magnesium and their Alloys-TemperDesignationISO6361-2 Wrought Aluminum and Aluminum Alloys,Sheets, Strips, and Plates2.4 ANSI Standards:4H35.1/H35.1(M) Alloy and Temper Designation Systemsfor AluminumH35.2M Dimensional Tolerances for Aluminum Mill Prod-ucts2.5 AMS Specification:5AMS 2772 H

34、eat Treatment of Aluminum Alloy Raw Mate-rials3. Terminology3.1 Definitions:3.2 Refer to Terminology B 881 for definitions of productterms used in this specification.3.3 Definitions of Terms Specific to This Standard:3.3.1 capable ofThe term capable of as used in thisspecification means that the tes

35、t need not be performed by theproducer of the material. However, should testing by thepurchaser establish that the material does not meet theserequirements, the material shall be subject to rejection.4. Ordering Information4.1 Orders for material to this specification shall include thefollowing info

36、rmation: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 (7.1),4.1.4 Temper (9.1),4.1.5 Finish for sheet in nonheat-treatable alloys (Section1),4.1.6 For sheet, whether flat or coiled,4

37、.1.7 Dimensions (thickness, width, and length or coil size),4.2 Additionally, orders for material to this specificationshall include the following information when required by thepurchaser:4.2.1 Whether a supply of one of the pairs of tempers whereshown in Table 2, (H14 or H24) or (H34 or H24), is s

38、pecificallyexcluded (Table 2, Footnote E),4.2.2 Whether bend tests are required (12.1),4.2.3 Whether heat treatment in accordance with PracticeB 918 is required (8.2),4.2.4 Whether testing for stress-corrosion cracking resis-tance of alloy 2124-T851 is required (13.1),4.2.5 Whether ultrasonic inspec

39、tion for aerospace or pres-sure vessels applications is required (Section 17),4.2.6 Whether inspection or witness of inspection and testsby the purchasers representative is required prior to materialshipment (Section 18),4.2.7 Whether certification is required (Section 22),4.2.8 Whether marking for

40、identification is required (20.1),and4.2.9 Whether Practices B 660 applies and, if so, the levelsof preservation, packaging, and packing required (21.3).5. Responsibility for Quality Assurance5.1 Responsibility for Inspection and TestsUnless other-wise specified in the contract or purchase order, th

41、e producer isresponsible for the performance of all inspection and testrequirements specified herein. The producer may use his ownor any other suitable facilities for the performance of theinspection and test requirements specified herein, unless dis-approved by the purchaser in the order or at the

42、time of contractsigning. The purchaser shall have the right to perform any ofthe inspections and tests set forth in this specification wheresuch inspections are deemed necessary to assure that materialconforms to prescribed requirements.5.2 Lot DefinitionAn inspection lot shall be defined asfollows:

43、5.2.1 For heat-treated tempers, an inspection lot shall con-sist of an identifiable quantity of material of the same millform, alloy, temper, and thickness traceable to a heat-treat lotor lots, and subjected to inspection at one time.5.2.2 For nonheat-treated tempers, an inspection lot shallconsist

44、of an identifiable quantity of material of the same millform, alloy, temper, and thickness subjected to inspection atone time.6. General Quality6.1 Unless otherwise specified, the material shall be sup-plied in the mill finish and shall be uniform as defined by therequirements of this specification

45、and shall be commerciallysound. Any requirement not so covered is subject to negotia-tion between producer and purchaser.6.2 Each sheet and plate shall be examined to determineconformance to this specification with respect to generalquality and identification marking. On approval of the pur-chaser,

46、however, the producer may use a system of statisticalquality control for such examinations.7. Chemical Composition7.1 LimitsThe sheet and plate shall conform to the chemi-cal composition limits specified in Table 1. Conformance shallbe determined by the producer by analyzing samples taken atthe time

47、 the ingots are cast, or samples taken from the finishedor semifinished product. If the producer has determined thechemical composition of the material during the course ofmanufacture, additional sampling and analysis of the finishedproduct shall not be required.NOTE 4It is standard practice in the

48、United States aluminum industryto determine conformance to the chemical composition limits prior tofurther processing of ingots into wrought products. Due to the continuousnature of the process, it is not practical to keep a specific ingot analysisidentified with a specific quantity of finished mate

49、rial.7.2 Number of SamplesThe number of samples taken fordetermination of chemical composition shall be as follows:7.2.1 When samples are taken at the time the ingots are cast,at least one sample shall be taken for each group of ingots castsimultaneously from the same source of molten metal.4Available in the Related Materials section (gray pages) of the Annual Book ofASTM Standards, Vol 02.02.5Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001