1、Designation: B 209 07Standard Specification forAluminum and Aluminum-Alloy Sheet and Plate1This standard is issued under the fixed designation B 209; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A numb
2、er 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 aluminum and aluminum-alloy fl
3、at sheet, coiled sheet, and plate in the alloys (Note 1)and tempers shown in Tables 2 and 3, and in the followingfinishes: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-side brigh
4、t finish, and standardtwo-sides bright finish.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 allo
5、ys containing 3 % or more nominal magnesium andintended for marine service and similar environments. Other alloy-temperproducts listed in this specification, which do not require the additionalcorrosion testing/capability called out in ASTM B 928/ B928M, may besuitable for marine and similar environ
6、ment applications.1.2 Alloy and temper designations are in accordance withANSI H35.1/H35.1(M). The equivalent Unified NumberingSystem alloy designations are those of Table 1 preceded byA9,for example, A91100 for aluminum 1100 in accordance withPractice E 527.1.3 A complete metric companion to Specif
7、ication B 209has been developedSpecification B 209M; therefore, nometric equivalents are presented 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 form a part of
8、this specifica-tion to the extent referenced herein:2.2 ASTM Standards:3B 548 Test Method for Ultrasonic Inspection of Aluminum-Alloy Plate for Pressure VesselsB 557 Test Methods for Tension Testing Wrought and CastAluminum- and Magnesium-Alloy ProductsB 594 Practice for Ultrasonic Inspection of Alu
9、minum-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 Terminology Relating
10、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 Aluminum Alloy Pla
11、teE29 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 Test Methods for Be
12、nd 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 Aluminum1This specification is under the ju
13、risdiction of ASTM Committee B07 on LightMetals and Alloys and is the direct responsibility of Subcommittee B07.03 onAluminum Alloy Wrought Products.Current edition approved Aug. 1, 2007. Published August 2007. Originallyapproved in 1946. Last previous edition approved in 2006 as B 209 06.2For ASME
14、Boiler and Pressure Vessel Code applications see related Specifi-cation SB-209 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 standa
15、rds 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.Alloys for Spectrochemical AnalysisE 1004 Practice for Determining Electri
16、cal ConductivityUsing the Electromagnetic (Eddy-Current) MethodE 1251 Test Method for Analysis of Aluminum and Alumi-num Alloys by Atomic Emission SpectrometryG34Test Method for Exfoliation Corrosion Susceptibilityin 2xxx and 7xxx Series Aluminum Alloys (EXCO Test)4G47 Test Method for Determining Su
17、sceptibility to Stress-Corrosion Cracking of 2xxx and 7xxx Aluminum AlloyProducts2.3 ANSI Standards:5H35.1/H35.1(M) Alloy and Temper Designation Systemsfor AluminumH35.2 Dimensional Tolerances forAluminum Mill Products2.4 AMS Specification:6AMS 2772 Heat Treatment of Aluminum Alloy Raw Mate-rials3.
18、Terminology3.1 DefinitionsRefer to Terminology B 881 for definitionsof product terms used in this specification.3.2 Definitions of Terms Specific to This Standard:3.2.1 capable ofThe term capable of, as used in thisspecification, means that the test need not be performed by theproducer of the materi
19、al. 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 information:4.1.1 This specification designation (which
20、includes thenumber, the year, and the revision letter, if applicable),4.1.2 Quantity in pieces or pounds,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,4.1.7 Dimensions (thickness, width, and length or coil s
21、ize),4.1.8 Tensile property limits and dimensional tolerances forsizes not covered in Table 2 or Table 3 of this specification andin ANSI H35.2, respectively.4.2 Additionally, orders for material meeting the require-ments of this specification shall include the following infor-mation when required b
22、y the purchaser: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 specificallyexcluded (Table 2, Footnote D),4.2.2 Whether heat treatment in accordance with PracticeB 918 is required (8.2),4.2.3 Whether bend tests are required (12.1),4.2.4
23、Whether testing for stress-corrosion cracking resis-tance of alloy 2124-T851 is required (13.1),4.2.5 Whether ultrasonic inspection 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
24、required prior to materialshipment (18.1),4.2.7 Whether certification is required (Section 22),4.2.8 Whether marking for 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 Qual
25、ity Assurance5.1 Responsibility for Inspection and TestsUnless other-wise specified in the contract or purchase order, the producer isresponsible for the performance of all inspection and testrequirements specified herein. The producer may use his ownor any other suitable facilities for the performa
26、nce of theinspection and test requirements specified herein, unless dis-approved by the purchaser in the order or at the 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 t
27、o ensure that materialconforms to prescribed requirements.5.2 Lot DefinitionAn inspection lot shall be defined asfollows: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-tre
28、at lotor lots, and subjected to inspection at one time.5.2.2 For nonheat-treated tempers, an inspection lot shallconsist 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
29、 material shall be sup-plied in the mill finish and shall be uniform as defined by therequirements of this specification and shall be commerciallysound. Any requirement not covered is subject to negotiationbetween producer and purchaser.6.2 Each sheet and plate shall be examined to determineconforma
30、nce to this specification with respect to generalquality and identification marking. On approval of the pur-chaser, 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 compositi
31、on limits specified in Table 1. Conformance shallbe determined by the producer by analyzing samples taken atthe time 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,
32、 additional sampling and analysis of the finishedproduct shall not be required.NOTE 4It is standard practice in the United States aluminum industry4The applicable edition in the use of this specification is G 3472formerlyavailable in the gray pages of the Annual Book of ASTM Standards , Vol 02.02.5A
33、vailable in the Related Materials section (gray pages) of the Annual Book ofASTM Standards, Vol 02.02.6Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001, http:/www.sae.org.B209072to determine conformance to the chemical composition limits prior tofu
34、rther 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 material.7.2 Number of SamplesThe number of samples taken forthe determination of chemical composition sh
35、all 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.7.2.2 When samples are taken from the finished or semifin-ished product, a sample shall be taken to repre
36、sent each 4000lb, or fraction thereof, of material in the lot, except that notmore than one sample shall be required per piece.7.3 Methods of SamplingSamples for determination ofchemical composition shall be taken in accordance with one ofthe following methods:TABLE 1 Chemical Composition LimitsA,B,
37、CAlloySilicon Iron Copper Manganese Magnesium Chromium Zinc Titanium Other ElementsDAluminumEach TotalE1060 0.25 0.35 0.05 0.03 0.03 . 0.05 0.03 0.03F. 99.60 minG11001230H0.95 Si + Fe0.70 Si + Fe0.050.200.100.050.05.0.05.0.100.10.0.030.050.03F0.15.99.00 minG99.30 minG2014 0.501.2 0.7 3.95.0 0.401.2
38、0.200.8 0.10 0.25 0.15 0.05 0.15 remainderAlclad 2014 2014 clad with 60032024 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 1230212422190.200.200.300.303.84.95.86.80.300.90.200.401.21.80.020.10.0.250.100.150.020.100.050.05I0.150.15IremainderremainderAlc
39、lad 2219 2219 clad with 70723003 0.6 0.7 0.050.20 1.01.5 . . 0.10 . 0.05 0.15 remainderAlclad 3003 3003 clad with 70723004 0.30 0.7 0.25 1.01.5 0.81.3 . 0.25 . 0.05 0.15 remainderAlclad 3004 3004 clad with 70723005 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
40、.8 0.200.8 0.20 0.40 0.10 0.05 0.15 remainder5005 0.30 0.7 0.20 0.20 0.501.1 0.10 0.25 . 0.05 0.15 remainder5010 0.40 0.7 0.25 0.100.30 0.200.6 0.15 0.30 0.10 0.05 0.15 remainder5050 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
41、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 remainder515452520.250.080.400.100.100.100.100.103.13.92.22.80.150.35.0.200.050.20.0.
42、050.03F0.150.10Fremainderremainder5254 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 0.150.45 0.81.2 . 0.05 . 0.
43、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 remainder6013 0.61.0 0.50 0.
44、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 70727008H0.10 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 . 0.05 0.15 remainder7075
45、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 70727008 Alclad 7075 7075 clad with 70087178 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 7072ALimits are in weight percent maximum unless shown as a ran
46、ge 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 nearestunitinthelast righthand place of figures us
47、ed 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 notspecified in the specification. However, su
48、ch 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 Total, the material shall be considerednonc
49、onforming.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 % 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 ma
