ASTM B570-2006 Standard Specification for Copper-Beryllium Alloy (UNS Nos C17000 and C17200) Forgings and Extrusions《(UNS Nos C17000和C17200)铜-铍合金锻件和挤压件的标准规范》.pdf

《ASTM B570-2006 Standard Specification for Copper-Beryllium Alloy (UNS Nos C17000 and C17200) Forgings and Extrusions《(UNS Nos C17000和C17200)铜-铍合金锻件和挤压件的标准规范》.pdf》由会员分享，可在线阅读，更多相关《ASTM B570-2006 Standard Specification for Copper-Beryllium Alloy (UNS Nos C17000 and C17200) Forgings and Extrusions《(UNS Nos C17000和C17200)铜-铍合金锻件和挤压件的标准规范》.pdf（4页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: B 570 06Standard Specification forCopper-Beryllium Alloy (UNS Nos. C17000 and C17200)Forgings and Extrusions1This standard is issued under the fixed designation B 570; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, th

2、e 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.1. Scope*1.1 This specification establishes the requirements forcopper-beryllium alloy forgings and extrusions produced

3、 fromthe following alloys.Copper Alloy UNS No.Nominal % CompositionBerylliumC17000C172001.71.9NOTE 1Requirements for copper-beryllium alloy rod and bar appearin Specification B 196/B 196M (Section 2).1.2 Unless otherwise specified, Copper Alloy UNS No.C17200 shall be the alloy furnished whenever Spe

4、cificationB 570 is specified without any alloy designation.1.3 UnitsThe values stated in inch-pound units are to beregarded as standard. The values given in parentheses aremathematical conversions to SI units, which are for informa-tion only and are not considered standard.1.4 The following hazard s

5、tatement pertains only to the testmethod portions of the specification: This standard does notpurport to address all of the safety concerns, if any, associatedwith its use. It is the responsibility of the user of this standardto establish appropriate safety and health practices anddetermine the appl

6、icability of regulatory limitations prior touse.2. Referenced Documents2.1 ASTM Standards:2B 194 Specification for Copper-Beryllium Alloy Plate,Sheet, Strip, and Rolled BarB 196/B 196M Specification for Copper-Beryllium AlloyRod and BarB 249/B 249M Specification for General Requirements forWrought C

7、opper and Copper-Alloy Rod, Bar, Shapes andForgingsB 601 Classification for Temper Designations for Copperand Copper AlloysWrought and CastB 846 Terminology for Copper and Copper AlloysE8 Test Methods for Tension Testing of Metallic MaterialsE18 Test Methods for Rockwell Hardness and RockwellSuperfi

8、cial Hardness of Metallic MaterialsE112 Test Methods for Determining Average Grain Size3. General Requirements3.1 The following sections of Specification B 249/B 249Mform a part of this specification.3.1.1 Terminology,3.1.2 Materials and Manufacture,3.1.3 Sampling,3.1.4 Number of Tests and Retests,3

9、.1.5 Sample Preparation,3.1.6 Test Methods,3.1.7 Significance of Numerical Limits,3.1.8 Inspection,3.1.9 Rejection and Rehearing,3.1.10 Certification,3.1.11 Mill Test Report,3.1.12 Packaging, Marking, Shipping and Preservation.3.2 In addition, when a section with a title identical to thatreferenced

10、in 3.1, appears in this specification, it containsadditional requirements that supplement those appearing inSpecification B 249/B 249M.4. Terminology4.1 Definitions:4.1.1 For definitions of terms related to copper and copperalloys, refer to Terminology B 846.4.1.2 extrusion, na uniform metal shape,

11、long in relationto its cross-sectional dimensions, produced by forcing a suit-ably preheated billet or preformed piece through an orifice(die) of the desired cross section.1This specification is under the jurisdiction ofASTM Committee B05 on Copperand Copper Alloys and is the direct responsibility o

12、f Subcommittee B05.02 on Rod,Bar, Wire, Shapes, and Forgings.Current edition approved Oct. 1, 2006. Published October 2006. Originallyapproved in 1972. Last previous edition approved in 2005 as B 570 05a.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Se

13、rvice 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, West Conshohocken, PA 19

14、428-2959, United States.4.1.3 forging, na metal part worked to a predeterminedshape by one or more such processes as hammering, upsetting,pressing, rolling, and so forth.5. Ordering Information5.1 Include the following information in orders for prod-ucts:5.1.1 ASTM designation and year of issue,5.1.

15、2 Quantity: number of pieces or pounds,5.1.3 Copper Alloy UNS No. (Section 1),5.1.4 Temper (Section 8) or condition (Section 12),5.1.5 Drawing showing the shape, dimensions, and toler-ances, if required,5.1.6 If an extrusion: the length (or mass) required, straight-ness as required,5.2 The following

16、 are options and should be included in thecontract or purchase order, when required:5.2.1 Tension tests (Section 11),5.2.2 Special tests such as grain size,5.2.3 Finish (see Section 15),5.2.4 Grain size (see Section 9), and5.2.5 When material is ordered for agencies of the U.S.government.6. Material

17、 and Manufacture6.1 Material:6.1.1 The material of manufacture shall be cast or wroughtbillet of C17000 or C17200 of such purity and soundness as tobe suitable for processing into the products prescribed herein.6.1.2 The product heat number shall appear on the certifi-cation or test report.6.2 Manuf

18、actureThe product shall be manufactured byhot working and heat treating as may be necessary to meet theproperties specified herein.7. Chemical Composition7.1 The product composition shall conform to the chemicalrequirements shown in Table 1.7.2 These composition limits do not preclude the presenceof

19、 other elements. Limits may be established and analysisrequired for unnamed elements by agreement between themanufacturer and the purchaser.7.3 Copper, given as remainder, is the difference betweenthe sum of all elements analyzed and 100 %. When all theelements given in Table 1 are analyzed, the sum

20、 of the resultsshall be 99.5 % minimum.8. Temper8.1 The standard temper designations available under thisspecification and as prescribed in Classification B 601 aresolution heat-treated TB00 (A) and precipitation heat-treatedTF00 (AT).9. Grain Size9.1 The grain size, if required, shall be as agreed

21、uponbetween the purchaser and the manufacturer and shall bedetermined in accordance with Test Methods E112.10. Physical Property Requirements10.1 Microstructure:10.1.1 The product in the TF00 (precipitation-hardened(AT) condition shall have a microstructure with a minimum ofsecond phase (beta) const

22、ituents. When present, beta shall befine and well dispersed.11. Mechanical Property Requirements11.1 HardnessThe product furnished under this specifica-tion shall conform to the hardness requirements prescribed inTable 2 for the solution heat-treated condition and Table 3 afterprecipitation heat tre

23、atment, unless tensile properties are re-quired by the purchase order. Rockwell hardness shall bedetermined in accordance with Test Method E18.11.2 TensileWhen specified in the contract or purchaseorder, the tensile properties of the product furnished shallconform to the properties in Table 2 or Tab

24、le 3 depending upontemper required. Tensile properties shall be determined inaccordance with Test Methods E8.12. Heat Treatment12.1 Solution Heat TreatmentTemper TB00 (A)Theproduct shall be heated to a uniform temperature, nominally1450F (788C) and quenched commensurate with the requiredproperty and

25、 structural integrity of the configuration.12.2 Precipitation Heat TreatmentTemper TF00 (AT)The product shall be heat treated to a uniform temperature inthe range from 600 to 700F (316 to 370C) for a minimum of2 to 3 h and then air cooled. This is the heat treatment for theacceptance tests shown in

26、Table 3.12.3 Special combinations of properties may be obtained byspecial precipitation heat treatments. The requirements forthese special heat treatments shall be agreed upon by themanufacturer or supplier and purchaser.13. Purchases for the U.S. Government13.1 When specified in the contract or pur

27、chase order,product purchased for agencies of the U.S. government shallconform to the special government regulations specified in theSupplementary Requirements section.14. Dimensions and Permissible Variations14.1 The dimensions and tolerances for these product formsshall be those shown on the drawi

28、ng that forms a part of eachorder or as agreed upon between the manufacturer and thepurchaser.TABLE 1 Chemical RequirementsComposition, %ElementCopper AlloyUNS No.C17000Copper AlloyUNS No.C17200Beryllium 1.601.85 1.802.00Additive elements:Nickel + cobalt, min 0.20 0.20Nickel + cobalt + iron, max 0.6

29、 0.6Aluminum, max 0.20 0.20Silicon, max 0.20 0.20Copper remainder remainderB57006215. Workmanship, Finish, and Appearance15.1 The product shall be free of defects; however, blem-ishes that do not interfere with the intended application areacceptable.15.2 The purchaser shall specify in the order the

30、conditionor finish required, such as, hot-worked, hot-worked andcleaned by blasting, pickling, or machining.16. Test Methods16.1 Chemical Composition:16.2 The chemical composition shall, in case of disagree-ment, be determined in accordance with the applicable methodin the Annex of Specification B 1

31、94.16.3 Test method(s) for the determination of element(s)required by contractual agreement shall be as agreed uponbetween the manufacturer and the purchaser.17. Keywords17.1 copper beryllium; extrusions; forgings; UNS C17000;UNS C17200SUPPLEMENTARY REQUIREMENTSThe following supplementary requiremen

32、ts shall apply only when specified by the purchaser in theinquiry, contract, or order, for agencies of the U.S. government.S1. Referenced DocumentsS1.1 The following documents of the issue in effect on dateof material purchase form a part of this specification to theextent referenced herein:S1.1.1 A

33、STM Standard:B 900 Practice for Packaging of Copper and Copper-AlloyMill-Products for U.S. Government AgenciesS1.1.2 Federal Standards:3Fed. Std. No. 102 Preservation, Packaging and PackingLevelsFed. Std. No. 123 Marking for Shipment (Civil Agencies)Fed. Std. No. 185 Identification Marking of Copper

34、 andCopper-Base Alloy Mill ProductsS1.1.3 Military Standards:3MIL-STD-105 Sampling Procedures and Tables for Inspec-tion by AttributesMIL-STD-129 Marking for Shipment and StorageS2. Quality AssuranceS2.1 Responsibility for Inspection:S2.1.1 Unless otherwise specified in the contract or pur-chase ord

35、er, the manufacturer is responsible for the perfor-mance of all inspection and test requirements specified. Exceptas otherwise specified in the contract or purchase order, themanufacturer may use his own or any other suitable facilitiesfor the performance of the inspection and test requirements,unle

36、ss disapproved by the purchaser at the time the order isplaced. The purchaser shall have the right to perform any of theinspections or tests set forth, when such inspections and tests3Available from Standardization Documents Order Desk, Bldg. 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5094

37、, Attn: NPODS.TABLE 2 Mechanical Properties as Solution Heat TreatedTemper DesignationDiameter orThickness, in.(mm)Copper Alloy UNS No.C17000 C17200 C17000 C17200Standard Former Tensile Strength, ksi (MPa)A,B, max Rockwell Hardness, maxB ScaleTB00 solution heat-treated (A) all sizes 85 (590) 85 (590

38、) 85 85Aksi = 1000 psi.BSee Appendix X1.TABLE 3 Mechanical Properties After Precipitation Heat TreatmentTemper DesignationStandard Former In. mmCopper Alloy UNSNo.Tensile Strength,ksiA(MPa)B,CYield Strength, ksi(MPa), 0.2 % Offset,minElongation in43DD,min,%RockwellC ScaleTF00 precipitationhardened(A

39、T)UNS C17000 150190 (10301310) 120 (820) 3 32Up to 8, incl up to 200; 165200 (11401380) 130 (890) 3 36TF00 precipitationhardened(AT)Over 8 to 12, incl., over 200 to 300; UNS C17200 155190 (10701310) 130 (890) 3 34Over 12 over 300 145180 (10001240) 125 (860) 3 34Aksi = 1000 psi.BSee Appendix X1.CThe

40、upper limits in the tensile strength column are for design guidance only.D43D=43Diameter.B570063are deemed necessary to assure that the material conforms toprescribed requirements.S3. Identification MarkingS3.1 All material shall be properly marked for identificationin accordance with Fed. Std. No.

41、185 except that the ASTMspecification number and the alloy number shall be used.S4. Preparation for DeliveryS4.1 Preservation, Packaging, Packing:S4.1.1 Military AgenciesThe material shall be separatedby size, composition, grade or class, and shall be preserved andpackaged, Level A or C, packed Leve

42、l A, B, or C as specifiedin the contract or purchase order, in accordance with therequirements of Practice B 900.S4.1.2 Civil AgenciesThe requirements of Fed. Std. No.102 shall be referenced for definitions of the various levels ofpackaging protection.S4.2 Marking:S4.2.1 Military AgenciesIn addition

43、 to any special mark-ing required by the contract or purchase order, marking forshipment shall be in accordance with MIL-STD-129.S4.2.2 Civil AgenciesIn addition to any special markingrequired by the contract or purchase order, marking forshipment shall be in accordance with Fed. Std. No. 123.APPEND

44、IX(Nonmandatory Information)X1. METRIC 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 1 kggives it a

45、n acceleration of 1 m/s2(N = kgm/s2). The derived SIunit for pressure or stress is the newton per square metre(N/m2), which has been named the pascal (Pa) by the GeneralConference on Weights and Measures. Since 1 ksi = 6 894 757Pa, the metric equivalents are expressed as megapascal (MPa),which is th

46、e same as MN/m2and N/mm2.SUMMARY OF CHANGESCommittee B05 has identified the location of selected changes to this standard since the last issue(B 570 05a) that may impact the use of this standard. (Approved Oct. 1, 2006.)(1) Table 3 was revised.Committee B05 has identified the location of selected ch

47、anges to this standard since the last issue (B 570 05)that may impact the use of this standard. (Approved Oct. 1, 2005.)(1) Table 3 was revised.Committee B05 has identified the location of selected changes to this standard since the last issue (B 570 01)that may impact the use of this standard. (App

48、roved March 1, 2005.)(1) Document was revised to change Elongation in 2 in. toElongation in 43D. (See Table 3.)ASTM International takes no position respecting the validity of any patent rights asserted in connection with any item mentionedin this standard. Users of this standard are expressly advise

49、d 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 must 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 therespons