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本文(ASTM B209M-2014 Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate (Metric)《铝和铝合金薄板材和厚板材的标准实施规程 (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-2014 Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate (Metric)《铝和铝合金薄板材和厚板材的标准实施规程 (米制)》.pdf

1、Designation: B209M 10B209M 14Standard 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

2、 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 U.S. Department of Defense.1. Scope*1.1 This specification covers aluminum

3、and aluminum alloy flat sheet, coiled sheet, and plate in the alloys (Note 1) and tempersshown in Tables 2 and 3, and Tables 2 and 4, 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-side

4、 bright mill finish, standard one-side bright finish, and standardtwo-sides bright finish.1.2 Alloy and temper designations are in accordance with ANSI H35.1/H35.1(M). The equivalent Unified Numbering System(UNS) alloy designations are those of Table 1Table 1 preceded byA9, for example,A91100 for al

5、uminum 1100 in accordance withPractice E527.NOTE 1Throughout this specification, use of the term alloy in the general 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 co

6、ntaining 3 % or more nominal magnesium and intendedfor marine service and similar environments. Other alloy-temper products listed in Specification B209, which do not require the additional corrosiontesting/capability called out in Specification B928/B928M, may be suitable for marine and similar env

7、ironment applications.1.3 This specification is the SI companion to Specification B209.1.3 For acceptance criteria for inclusion of new aluminum and aluminum alloys in this specification, see Annex A2.1.4 This specification is the SI companion to Specification B209.1.5 This standard does not purport

8、 to address all of the safety concerns, if any, associated with its use. It is the responsibilityof the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatorylimitations prior to use.2. Referenced Documents2.1 The following documents

9、form a part of this specification to the extent referenced herein:2.2 ASTM Standards:2B209 Specification for Aluminum and Aluminum-Alloy Sheet and PlateB548 Test Method for Ultrasonic Inspection of Aluminum-Alloy Plate for Pressure VesselsB557M Test Methods for Tension Testing Wrought and Cast Alumi

10、num- and Magnesium-Alloy Products (Metric)B594 Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought ProductsB632/B632M Specification for Aluminum-Alloy Rolled Tread PlateB660 Practices for Packaging/Packing of Aluminum and Magnesium ProductsB666/B666M Practice for Identification Marking of A

11、luminum and Magnesium ProductsB881 Terminology Relating to Aluminum- and Magnesium-Alloy ProductsB918 Practice for Heat Treatment of Wrought Aluminum AlloysB928/B928M Specification for High Magnesium Aluminum-Alloy Sheet and Plate for Marine Service and Similar Environ-ments1 This specification is u

12、nder the jurisdiction of ASTM Committee B07 on Light Metals and Alloys and is the direct responsibility of Subcommittee B07.03 on AluminumAlloy Wrought Products.Current edition approved Nov. 1, 2010Nov. 1, 2014. Published July 2011November 2014. Originally approved in 1978. Last previous edition app

13、roved in 20072010 asB209M 07.B209M 10. DOI: 10.1520/B0209M-10.10.1520/B0209M-14.2 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page o

14、n the ASTM website.This 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 the previous version. Becauseit may not be technically possible to adequately depict all changes accurately, ASTM recommends that user

15、s 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 Summary of Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshoh

16、ocken, PA 19428-2959. United States1B947 Practice for Hot Rolling Mill Solution Heat Treatment for Aluminum Alloy PlateB985 Practice for SamplingAluminum Ingots, Billets, Castings and Finished or Semi-Finished WroughtAluminum Products forCompositional AnalysisE29 Practice for Using Significant Digit

17、s in Test Data to Determine Conformance with SpecificationsE34 Test Methods for Chemical Analysis of Aluminum and Aluminum-Base AlloysE290 Test Methods for Bend Testing of Material for DuctilityTABLE 1 Chemical Composition LimitsA,B,C,MNOTE 1In case there is a discrepancy in the values listed in Tab

18、le 1 with those listed in the “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 co

19、ntrolling composition. The “Teal Sheets” are available athttp:/www.aluminum.org/tealsheets.Alloy Silicon 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 minG1100 0.95 Si + Fe 0.050.20 0.05 . . 0.10 . 0.0

20、5 0.15 99.00 minG1230H 0.70 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 alloy

21、2124 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 0.05I 0.15I remainderAlclad 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

22、.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 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

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

24、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 0.08 0.10 0.10 0.10 2.22.8 . 0.05 . 0.03F 0.10F remainder5254 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

25、 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 . 0.03F 0.10F remainder5657 0.08 0.10 0.10 0.03 0.61.0 . 0.05 . 0.02K 0.05K remainder5754 0.40 0.40 0.10 0.50L 2.6-3.6 0.30L 0.20 0.15 0.0

26、5 0.15 remainder6003H 0.351.0 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 alloy7072H 0.7 Si + Fe 0.10 0.10 0.

27、10 . 0.81.3 . 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 alloyA Limits are in mass percent maximum unless shown as a range or stated otherwise.B Analysis shall be made for the elements for which limits are shown in thi

28、s table.C For purposes of determining conformance to these limits, an observed value or a calculated value attained from analysis shall be rounded to the nearest unit in the lastright hand place of figures used in expressing the specified limit, in accordance with the Rounding Method of Practice E29

29、.D Others 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. Should any anal

30、ysis 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 considerednon-conforming. The Total for Other Elements does not include elements shown in the footnotes w

31、ith specific composition limits.E Other ElementsTotal shall be the sum of unspecified metallic elements 0.010 % or more, rounded to the second decimal before determining the sum.F Vanadium 0.05 max. The total for other elements does not include vanadium.G The aluminum content shall be calculated by

32、subtracting from 100.00 % the sum of all metallic elements present in amounts of 0.010 % or more each, rounded to thesecond decimal before determining the sum.H Composition of cladding alloy as applied during the course of manufacture. Samples from finished sheet or plate shall not be required to co

33、nform to these limits.I Vanadium, 0.050.15, zirconium, 0.100.25.J 0.050.25 Zr.K Gallium 0.03 max, vanadium 0.05 max.L 0.10-0.6 0.100.6 Mn + Cr.M In case there is a discrepancy in the values listed in Table 1 with those listed in the “International Alloy Designations and Chemical Composition Limits f

34、or WroughtAluminum and WroughtAluminumAlloys” (known as the “Teal Sheets”), the composition limits registered with theAluminumAssociation and published in the “Teal Sheets”shall be considered the controlling composition. The “Teal Sheets” are available at http:/www.aluminum.org/tealsheets.B209M 142T

35、ABLE 2 Mechanical Property Limits for Nonheat-Treatable AlloysA,BAlloy TemperSpecified Thickness,mmTensile Strength,MPaYield Strength(0.2 % offset), MPaElongation,min, %C BendDiameterFactor, Nover through min max min max in 50 mm in 5Diameter1060 O 0.15 0.32 55 95 15 . 15 . .1060 O 0.32 0.63 55 95 1

36、5 . 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 H12D or H22D 0.40 0.63 75 110 60 . 6 . .1060 H12D or H22D 0.63 1.20 75 110 60 . 7 . .1060 H12D or H22D 1.20 6.30 75 110 60 . 12 . .1060 H12D or H22D 6.30 50.00 75 110 60 . 12 10 .10

37、60 H14D or H24D 0.20 0.32 85 120 70 . 1 . .1060 H14D or H24D 0.32 0.63 85 120 70 . 2 . .1060 H14D or H24D 0.63 1.20 85 120 70 . 6 . .1060 H14D or H24D 1.20 6.30 85 120 70 . 10 . .1060 H14D or H24D 6.30 25.00 85 120 70 . 10 9 .1060 H16D or H26D 0.15 0.32 95 130 75 . 1 . .1060 H16D or H26D 0.32 0.63 9

38、5 130 75 . 2 . .1060 H16D or H26D 0.63 1.20 95 130 75 . 4 . .1060 H16D or H26D 1.20 4.00 95 130 75 . 5 . .1060 H18D or H28D 0.15 0.32 110 . 85 . 1 . .1060 H18D or H28D 0.32 0.63 110 . 85 . 2 . .1060 H18D or H28D 0.63 1.20 110 . 85 . 3 . .1060 H18D or H28D 1.20 3.20 110 . 85 . 4 . .1060 H112 6.30 12.

39、50 75 . . . 10 . .1060 H112 12.50 40.00 70 . . . . 18 .1060 H112 40.00 80.00 60 . . . . 22 .1060 FE 6.30 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 . 22 . 01100 O 1.20 6.30 75 105 25 . 30 . 01100 O 6.30 80.00 75 105 25 . 28 25

40、01100 H12D or H22D 0.40 0.63 95 130 75 . 3 . 01100 H12D or H22D 0.63 1.20 95 130 75 . 5 . 01100 H12D or H22D 1.20 6.30 95 130 75 . 8 . 01100 H12D or H22D 6.30 12.50 95 130 75 . 10 9 01100 H12D or H22D 12.50 50.00 95 130 75 . 10 9 .1100 H14D or H24D 0.20 0.32 110 145 95 . 1 . 01100 H14D or H24D 0.32

41、0.63 110 145 95 . 2 . 01100 H14D or H24D 0.63 1.20 110 145 95 . 3 . 01100 H14D or H24D 1.20 6.30 110 145 95 . 5 . 01100 H14D or H24D 6.30 25.00 110 145 95 . 7 6 01100 H16D or H26D 0.15 0.32 130 165 115 . 1 . 41100 H16D or H26D 0.32 0.63 130 165 115 . 2 . 41100 H16D or H26D 0.63 1.20 130 165 115 . 3

42、. 41100 H16D or H26D 1.20 4.00 130 165 115 . 4 . 41100 H18D or H28D 0.15 0.32 150 . . . 1 . .1100 H18D or H28D 0.32 0.63 150 . . . 1 . .1100 H18D or H28D 0.63 1.20 150 . . . 2 . .1100 H18D or H28D 1.20 3.20 150 . . . 4 . .1100 H112 6.30 12.50 90 . 50 . 9 . .1100 H112 12.50 40.00 85 . 40 . . 12 .1100

43、 H112 40.00 80.00 80 . 30 . . 18 .1100 FE 6.30 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 95 130 35 . 23 21 .3003 H12D or H22D 0.40

44、 0.63 120 160 85 . 3 . 03003 H12D or H22D 0.63 1.20 120 160 85 . 4 . 03003 H12D or H22D 1.20 6.30 120 160 85 . 6 . 03003 H12D or H22D 6.30 50.00 120 160 85 . 9 8 .3003 H14D or H24D 0.20 0.32 140 180 115 . 1 . 03003 H14D or H24D 0.32 0.63 140 180 115 . 2 . 03003 H14D or H24D 0.63 1.20 140 180 115 . 3

45、 . 03003 H14D or H24D 1.20 3.20 140 180 115 . 5 . 03003 H14D or H24D 3.20 6.30 140 180 115 . 5 . 2B209M 143TABLE 2 ContinuedAlloy TemperSpecified Thickness,mmTensile Strength,MPaYield Strength(0.2 % offset), MPaElongation,min, %C BendDiameterFactor, Nover through min max min max in 50 mm in 5Diamete

46、r3003 H14D or H24D 6.30 25.00 140 180 115 . 8 7 .3003 H16D or H26D 0.15 0.32 165 205 145 . 1 . 43003 H16D or H26D 0.32 0.63 165 205 145 . 2 . 43003 H16D or H26D 0.63 1.20 165 205 145 . 3 . 43003 H16D or H26D 1.20 4.00 165 205 145 . 4 . 63003 H18D or H28D 0.15 0.32 185 . 165 . 1 . .3003 H18D or H28D

47、0.32 0.63 185 . 165 . 1 . .3003 H18D or H28D 0.63 1.20 185 . 165 . 2 . .3003 H18D or H28D 1.20 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 FF 6.30 80.00 . . . . . . .Alclad 3003 O 0.15 0.32 90 125 30 .

48、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 95F 130F 35F . . 21 .Alclad 3003 H12D or H22D 0.40 0.63 115 155 80 . 4 . .Alclad 3003 H12D or H22D

49、0.63 1.20 115 155 80 . 5 . .Alclad 3003 H12D or H22D 1.20 6.30 115 155 80 . 6 . .Alclad 3003 H12D or H22D 6.30 12.50 115 155 80 . 9 . .Alclad 3003 H12D or H22D 12.50 50.00 120F 160F 85F . . 8 .Alclad 3003 H14D or H24D 0.20 0.32 135 175 110 . 1 . .Alclad 3003 H14D or H24D 0.32 0.63 135 175 110 . 2 . .Alclad 3003 H14D or H24D 0.63 1.20 135 175 110 . 3 . .Alclad 3003 H14D or H24D 1.20 6.30 135 175 110 . 5 . .Alclad 3003 H14D or H24D 6.30 12.50 135 175 110 . 8 . .Alclad 3003 H14D or H24D 12.50 25.00 140

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