ASTM B422-2006 Standard Specification for Copper-Aluminum-Silicon-Cobalt Alloy Copper-Nickel-Silicon-Magnesium Alloy Copper-Nickel-Silicon Alloy Copper-Nickel-Aluminum-Magnesium Al.pdf

1、Designation: B 422 06Standard Specification forCopper-Aluminum-Silicon-Cobalt Alloy, Copper-Nickel-Silicon-Magnesium Alloy, Copper-Nickel-Silicon Alloy,Copper-Nickel-Aluminum-Magnesium Alloy, and Copper-Nickel-Tin Alloy Sheet and Strip1This standard is issued under the fixed designation B 422; the n

2、umber immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.This

3、standard has been approved for use by agencies of the Department of Defense.1. Scope*1.1 This specification establishes the requirements for2Cop-per Alloy UNS Nos. C19010, C19020, C19025, C63800,C64725, C70250, C70260, and C70265 sheet and strip.1.2 The values stated in inch-pound units are to be re

4、gardedas the standard. The values given in SI units representmathematical conversions, which are provided for informationonly and are not considered standard.1.3 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user

5、of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Referenced Documents2.1 The following documents of the issue in effect on dateof material purchase form a part of this specification to theextent referenc

6、ed herein:2.2 ASTM Standards:3B 248 Specification for General Requirements for WroughtCopper and Copper-Alloy Plate, Sheet, Strip, and RolledBarB 248M Specification for General Requirements forWrought Copper and Copper-Alloy Plate, Sheet, Strip, andRolled Bar MetricB 846 Terminology for Copper and C

7、opper AlloysE 527 Practice for Numbering Metals and Alloys (UNS)3. General Requirements3.1 Material furnished to this specification shall be inaccordance with the applicable requirements of the currentedition of Specification B 248.4. Terminology4.1 DefinitionsFor definitions of terms related to cop

8、perand copper alloys, refer to Terminology B 846.5. Ordering Information5.1 Orders for material under this specification shouldinclude the following information:5.1.1 Quantity (of each size),5.1.2 Alloy: Copper Alloy UNS No. (Section 1),5.1.3 Form of material (sheet or strip),5.1.4 Temper (see 7.1),

9、5.1.5 Dimensions (thickness, width, length (if applicable),5.1.6 How furnished (rolls, specific lengths with or withoutends, stock lengths with or without ends),5.1.7 Type of edge, if required (slit, sheared, sawed, squarecorners, rounded corners, rounded edges, or full-rounded edges(see 10.6),5.1.8

10、 Type of width and straightness tolerances, if required(slit-metal tolerances, square sheared-metal tolerances, sawed-metal tolerances, straightened or edge-rolled-metal tolerances)(Section 10), and5.1.9 ASTM specification number and year of issue.5.2 In addition, when material is purchased for agen

11、cies ofthe U.S. government, it shall conform to the SupplementaryRequirements as defined in Specification B 248 when specifiedin the contract or purchase order.6. Chemical Composition6.1 The materials shall conform to the compositions pre-scribed in Table 1.1This specification is under the jurisdict

12、ion ofASTM Committee B05 on Copperand CopperAlloys and is the direct responsibility of Subcommittee B05.01 on Plate,Sheet, and Strip.Current edition approved Oct. 15, 2006. Published October 2006. Originallyapproved 1965. Last previous edition approved in 2005 as B 422 05.2The UNS system for copper

13、and copper alloys (see Practice E 527) is a simpleexpansion of the former standard designation system accomplished by the additionof a prefix “C” and a suffix “00.” The suffix can be used to accommodatecomposition variations of the base alloy.3For referenced ASTM standards, visit the ASTM website, w

14、ww.astm.org, orcontact 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

15、, PO Box C700, West Conshohocken, PA 19428-2959, United States.6.2 These specification limits do not preclude the presenceof other elements. Limits for unnamed elements may beestablished by agreement between manufacturer or supplierand purchaser.6.3 When copper is listed as remainder, copper may bet

16、aken as the difference between the sum of all the elementsanalyzed and 100 %. When all the elements in Table 1 forAlloys C 19010, C63800, C64725, C70250, C70260 andC70265 are analyzed, their sum shall be 99.5 % min. When allthe elements in Table 1 for Alloy C19025 are analyzed, theirsum shall be 99.

17、7 % min. When all the elements in Table 1 forAlloy C19020 are analyzed, their sum shall be 99.8 % min.7. Temper7.1 Tempers available under this specification are as desig-nated in Tables 2-7.8. Mechanical Properties8.1 Copper Alloy UNS No. C63800 is a dispersion-strengthened alloy which does not req

18、uire heat treatment. Theannealed and rolled tempers shall conform to the tensileproperty requirements prescribed in Table 2.8.2 Copper Alloy UNS No. C70250 is supplied in a mill-hardened, or cold-worked and precipitation heat-treated, orprecipitation heat-treated or spinodal heat-treated, 1/2 Hd and

19、stress-relieved tempers. The 0.2 % offset yield strength shall bethe standard tests for these tempers and shall conform to therequirements specified in Table 3.8.2.1 If ductility or formability requirements are desired,they shall be negotiated and agreed upon between manufac-turer and purchaser.8.3

20、Copper Alloys UNS No. C70260 and C70265 aresupplied in a mill-hardened temper. The 0.2 % offset yieldTABLE 1 Chemical Requirements Composition %Element C19010 C19020 C19025 C63800 C64725 C70250 C70260 C70265Nickel 0.81.8 0.503.0 0.801.2 0.20 max. 1.32.7A2.24.2B1.03.0B1.03.0BSilicon 0.150.35 . . . .

21、. . 1.52.1 0.200.8 0.251.2 0.200.7 0.200.7Lead, max . . . . . . . . . 0.05 0.01 0.05 . . . 0.05Iron, max . . . . 0.10 0.20 0.25 0.20 . . . . .Zinc, max . . . . . . 0.20 0.8 0.501.5 1.0 . . . 0.30Aluminum . . . . . . . . . 2.53.1 . . . . . . . . . . . .CopperAremainder remainder remainder remainder 9

22、5.0 min remainder remainder remainderCobalt . . . . . . . . . 0.250.55 . . . . . . . . . . . .Manganese, max . . . . . . . . . 0.10 . . . 0.10 . . . . . .Magnesium . . . . . . . . . . . . 0.20 max 0.050.30 . . . . . .Tin . . . 0.300.9 0.71.1 . . . 0.200.8 . . . . . . 0.050.8Phosphorus 0.010.05 0.010

23、.20 0.030.07 . . . . . . . . . 0.010 max 0.01 maxCalcium . . . . 0.01 . . .Chromium . . . . 0.20 . . .AIncluding silver.BIncluding cobalt.TABLE 2 Tensile Property Requirements and Approximate Hardness Values for Copper Alloy UNS No. C63800Temper Tensile StrengthElongation in 2 in.(50.8 mm), %Approxi

24、mate Rockwell HardnessADesignation Name ksiBMPaCRockwell B Superficial 30TO60 soft anneal 78 max 540 max 37 min . . . . . .O61 annealed 7787 530600 2740 . . . 7078H0114 hard 90102 620705 . . . 9296 7680H0212 hard 100112 690775 . . . 9598 7981H0334 hard 105117 720810 . . . 9799 8082H04 hard 114126 78

25、5870 . . . 98100 8183H06 extra hard 118130 815900 . . . 99101 8183H08 spring 123134 845925 . . . 99101 8284H10 extra spring 130 min 900 min . . . 100 min 83 minAHardness values shown apply only to direct determination, not converted values. They are for information only.Bksi = 1000 psi.CSee Appendix

26、 X1.TABLE 3 Yield Requirements for Copper Alloy UNS No. C70250Temper DesignationYield Strength at 0.2 % OffsetksiAMPaBTM00 6590 450620TM02 83110 585760TM03 95120 655825TR02 80 min 550 minTH03 6585 450585Aksi = 1000 psi.BSee Appendix X1.TABLE 4 Tensile and Yield Requirements forCopper Alloy UNS No. C

27、70260 and C70265Temper DesignationYield Strength at 0.2 % OffsetksiAMPaBTM00 6585 450585TM02 90100 620690TM03 95115 653790TM04 100120 687825Tensile StrengthTemperDesignationksiAMPaBTM01 90105 620720Aksi = 1000 psi.BSee Appendix X1.B422062strength shall be the standard test for the mill-hardened temp

28、ersTM00, TM02, TM03, and TM04 and shall conform to therequirements specified in Table 4. The tensile strength shall bethe standard test for the mill-hardened temper TM01 and shallconform to the requirements specified in Table 4.8.3.1 If ductility or formability requirements are desired,they shall be

29、 negotiated and agreed upon between manufac-turer and purchaser.8.4 Copper Alloy UNS Nos. C19020 and C19025 aresupplied in cold-worked, stress-relieved temper. These tempersshall conform to the tensile strength and elongation require-ments in Table 5. The 0.2 % offset yield strength shall be thestan

30、dard test for the mill-hardened tempers and shall conformto the requirements specified in Table 7 and Table 5, respec-tively.8.4.1 If ductility or formability requirements are desired,they shall be negotiated and agreed upon between manufac-turer and purchaser.8.5 Copper Alloy UNS No. C19010 is supp

31、lied in eitherprecipitation heat-treated (TM03 to TM08) tempers, or mill-hardened (H01 to H10) tempers. The 0.2 % offset yieldstrength shall be the standard test for the precipitation heat-treated and mill-hardened tempers and shall conform to therequirements specified in Table 6.8.5.1 If ductility

32、or formability requirements are desired,they shall be negotiated and agreed upon between manufac-turer and purchaser.8.6 Copper alloy C64725 is supplied in either mill-hardenedtemper (TM02TM08) temper, or cold-worked, stress relieved(HR04) temper. Tempers shall conform to the 0.2 % offsetyield requi

33、rements specified in Table 8.8.6.1 If ductility or formability requirements are desired,they shall be negotiated and agreed upon between manufac-turer and purchaser.9. Electrical Properties9.1 The electrical resistivity of Copper Alloys UNS Nos.C19010, C19025, C63800, C64725, C70250, C70260 andC7026

34、5 are listed in Table 9 for information only.10. Dimensions and Permissible Variations10.1 The dimensions and tolerances shall be as prescribed inthe current edition of Specifications B 248 and B 248M:10.2 Thickness:10.3 Width:10.3.1 Slit Metal and Slit Metal with Rolled Edges10.3.2 Square-Sheared M

35、etal10.3.3 Sawed Metal10.4 Length:10.4.1 Specific and Stock Lengths With and Without Ends10.4.2 Schedule of Lengths (Specific and Stock) With Ends10.4.3 Length Tolerances for Square-Metal10.4.4 Length Tolerances for Sawed Metal10.5 Straightness:10.5.1 Slit Metal or Slit Metal Either Straightened orE

36、dge-Rolled10.5.2 Square-Sheared Metal10.5.3 Sawed Metal10.6 Edges:10.6.1 Square Edges10.6.2 Rounded Corners10.6.3 Rounded Edges10.6.4 Full-Rounded Edges11. Keywords11.1 copper-aluminum-silicon-cobalt alloy; copper-nickel-aluminum magnesium alloy; copper-nickel-silicon alloy; cop-per nickel-silicon-m

37、agnesium alloy; copper-nickel-tin alloy;sheet; strip; UNS No. C19010; UNS No. C19020; UNS No.C19025; UNS No. C63800; UNS No. C64725; UNS No.C70250; UNS No. C70260; UNS No. C70265TABLE 5 Tensile Requirements forCopper Alloy UNS No. C19025DesignationTensile Strength Elongation in 2 in.ksiAMPaB(50.8 mm

38、) %HR02 6376 435525 925HR04 7283 495570 514HR06 78 min 540 min 412Aksi = 1000 psi.BSee Appendix X1.TABLE 6 Yield Requirements for Copper Alloy UNS No. C19010Temper Designation Yield Strength at 0.2 % OffsetksiAMPaBTM03 5065 340450TM04 6075 410515TM06 6479 440545TM08 7489 510610H01 4055 275380H02 546

39、9 370475H03 6277 410530H04 6681 435555H06 7287 460600H08 7893 520640H10 85100 585685Aksi = 1000 psi.BSee Appendix X1.TABLE 7 Tensile Requirements forCopper Alloy UNS No. C19020Designation Tensile Strength Elongation in 2 in.(50.8 mm), %ksi MPaHR02 58-70 400-485 5 minHR04 65-74 450-510 3 minHR06 71-8

40、0 490-550 3 minHR08 77 min 530 min 2 minTABLE 8 Yield Requirements forCopper Alloy UNS No. C64725Designation Yield StrengthksiAMPaBTM02 7090 480620TM04 85105 585720TM06 95115 655790TM08 100120 690825HR04 80105 550720Aksi = 1000 psi.BSee Appendix X1.B422063APPENDIX(Nonmandatory Information)X1. METRIC

41、 EQUIVALENTSX1.1 The SI unit for strength properties now shown is inaccordance with the International System of Units (SI). Thederived SI unit for force is the newton (N), which is defined asthat force which when applied to a body having a mass of onekilogram gives it an acceleration of one metre pe

42、r secondsquared (N = kg m/s2). The derived SI unit for pressure orstress is the newton per square metre (N/m2), which has beennamed the pascal (Pa) by the General Conference on Weightsand Measures. Since 1 ksi = 6 894 757 Pa, the metric equiva-lents are expressed as megapascal (MPa), which is the sa

43、me asMN/m2and N/mm2.SUMMARY OF CHANGESCommittee B05 has identified the location of selected changes to this standard since the last issue (B 422 05)that may impact the use of this standard. (Approved Oct. 15, 2006)(1) Added Copper UNS Alloy No. C64725 to 1.1.(2) Added 8.6 and 8.6.1.(3) Added C64725

44、to 9.1.(3) Eliminated references to sections and tables of Specifica-tion B 248 in Section 10.(4) Added C64725 to Keywords, Section 11.(5) Added C64725 to Table 1.(6) Corrected chemistry of Copper UNS Alloy No. C19025 inTable 1.(7) Added footnote to Table 1 to include silver in copper.(8) Changed Ta

45、ble 10 to call out specifications for UNS No.C64725.(9) Added Table 3.(10) Renumbered Electrical Resistivity and ConductivityEquivalent table to be Table 9.TABLE 9 Electrical Resistivity and Conductivity EquivalentCopper AlloyUNS No.TemperElectrical Resistivityat 20C (68F),V g/m2Equivalent Con-ducti

46、vity at 20C(68F), % IACSC63800 1.5328 10C64725 TM02 0.3832 40C64725 TM04, TM06, TM08,HR040.4143 37C70250 TR02, TM00, TM02 0.3832 40C70250 TM03 0.4258 36C70260 TM00, TM02, TM03,TM040.3832 40C70260 TM01 0.3066 50C70265 TM00, TM02, TM03,TM040.4379 35C70265 TM01 0.3406 45C19025 HR02, HR04, HR06 0.3832 4

47、0C70250 TH03 0.3066 50C19010 H08, H10 0.3193 48C19010 TM03, TM04, TM06,TM08, H03, H04,H060.3066 50C19010 H01, H02 0.2787 55 minC19020 HR02, HR04, HR06,HR080.3066 50B422064ASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedi

48、n this standard. Users of this standard are expressly advised that determination of the validity of any such patent rights, and the riskof infringement of such rights, are entirely their own responsibility.This standard is subject to revision at any time by the responsible technical committee and mu

49、st be reviewed every five years andif not revised, either reapproved or withdrawn. Your comments are invited either for revision of this standard or for additional standardsand should be addressed to ASTM International Headquarters. Your comments will receive careful consideration at a meeting of theresponsible technical committee, which you may attend. If you feel that your comments have not received a fair hearing you shouldmake your views known to the ASTM