ASTM F2066-2011 Standard Specification for Wrought Titanium-15 Molybdenum Alloy for Surgical Implant Applications (UNS R58150)《外壳植入应用(UNS R58150)锻造钛-15钼合金的标准规范》.pdf

《ASTM F2066-2011 Standard Specification for Wrought Titanium-15 Molybdenum Alloy for Surgical Implant Applications (UNS R58150)《外壳植入应用(UNS R58150)锻造钛-15钼合金的标准规范》.pdf》由会员分享，可在线阅读，更多相关《ASTM F2066-2011 Standard Specification for Wrought Titanium-15 Molybdenum Alloy for Surgical Implant Applications (UNS R58150)《外壳植入应用(UNS R58150)锻造钛-15钼合金的标准规范》.pdf（5页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: F2066 11Standard Specification forWrought Titanium-15 Molybdenum Alloy for Surgical ImplantApplications (UNS R58150)1This standard is issued under the fixed designation F2066; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revi

2、sion, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope*1.1 This specification covers the chemical, mechanical, andmetallurgical requirements for wrought titan

3、ium-15 molybde-num alloy to be used in the manufacture of surgical implants(1).21.2 The values stated in inch-pound units are to be regardedas standard. The values given in parentheses are mathematicalconversions to SI units that are provided for information onlyand are not considered standard.2. Re

4、ferenced Documents2.1 ASTM Standards:3E8 Test Methods for Tension Testing of Metallic MaterialsE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE112 Test Methods for Determining Average Grain SizeE290 Test Methods for Bend Testing of Material for Duc-

5、tilityE1409 Test Method for Determination of Oxygen andNitrogen in Titanium and Titanium Alloys by the Inert GasFusion TechniqueE1447 Test Method for Determination of Hydrogen inTitanium and Titanium Alloys by Inert Gas Fusion Ther-mal Conductivity/Infrared Detection MethodE2371 Test Method for Anal

6、ysis of Titanium and TitaniumAlloys by Atomic Emission Plasma SpectrometryF67 Specification for Unalloyed Titanium, for SurgicalImplant Applications (UNS R50250, UNS R50400, UNSR50550, UNS R50700)F748 Practice for Selecting Generic Biological Test Meth-ods for Materials and DevicesF981 Practice for

7、Assessment of Compatibility of Biomate-rials for Surgical Implants with Respect to Effect ofMaterials on Muscle and BoneF1408 Practice for Subcutaneous Screening Test for Im-plant Materials2.2 Aerospace Material Specification:AMS 2249 Chemical Check Analysis Limits, Titanium andTitanium Alloys42.3 I

8、SO Standards:5ISO 6892 Metallic Materials Tensile TestingISO 9001 Quality Management Systems2.4 American Society for Quality Standard:ASQ C1 Specification of General Requirements for a Qual-ity Program63. Terminology3.1 Definitions of Terms Specific to This Standard:3.1.1 beta annealed, nthe conditi

9、on of the material that isobtained if, following the final hot-working or cold-workingoperation, the mill product is rapidly quenched, for example,by water quenching or pressurized helium gas quench, from atemperature above the beta transus of approximately 1382F(750C).3.1.2 beta transus, nthe minim

10、um temperature at whichthe alpha plus beta phase can transform to 100 % beta phase.4. Product Classification4.1 StripAny product under 0.1875 in. (4.76 mm) inthickness and under 24 in. (610 mm) wide.4.2 SheetAny product under 0.1875 in. (4.76 mm) inthickness and 24 in. (610 mm) or more in width.4.3

11、PlateAny product 0.1875 in. (4.76 mm) thick andover and 10 in. (254 mm) wide and over, with widths greaterthan five times the thickness. Any plate up to 4 in. (101.60mm), thick inclusive, is covered by this specification.4.4 BarRounds, flats, or other shapes from 0.1875 in.(4.76 mm) to 4 in. (101.60

12、 mm) in diameter or thickness.(Other sizes and shapes by special order.)1This specification is under the jurisdiction of ASTM Committee F04 onMedical and Surgical Materials and Devices and is the direct responsibility ofSubcommittee F04.12 on Metallurgical Materials.Current edition approved Dec. 1,

13、2011. Published December 2011. Originallyapproved in 2001. Last previous edition approved in 2008 as F2066 08. DOI:10.1520/F206611.2The boldface numbers in parentheses refer to the list of references at the end ofthis standard.3For referenced ASTM standards, visit the ASTM website, www.astm.org, orc

14、ontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.4Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001, http:/www.sae.org.5Available fr

15、om American National Standards Institute (ANSI), 25 W. 43rd St.,4th Floor, New York, NY 10036, http:/www.ansi.org.6Available from American Society for Quality (ASQ), 600 N. Plankinton Ave.,Milwaukee, WI 53203, http:/www.asq.org.1*A Summary of Changes section appears at the end of this standard.Copyr

16、ight ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.4.5 WireRounds, flats, or other shapes less than316 in.(4.76 mm) in diameter or thickness.5. Ordering Information5.1 Include with inquiries and orders for material under thisspecification the

17、 following information.5.1.1 Quantity,5.1.2 Applicable ASTM designation and date of issue,5.1.3 Form (strip, sheet, plate, bar, or wire),5.1.4 Condition (see Section 3 and 6.1),5.1.5 Mechanical properties (if applicable for special con-ditions),5.1.6 Finish (see 6.2),5.1.7 Applicable dimensions incl

18、uding size, thickness,width, length, or drawing number,5.1.8 Special tests, if any, and5.1.9 Special requirements.6. Materials and Manufacture6.1 FinishThe mill product may be furnished to theimplant manufacturer as descaled or pickled, abrasive-blasted,chemically milled, ground, machined, peeled, p

19、olished, or asspecified by the purchaser. On billets, bars, plates, and forg-ings, it is permissible to remove minor surface imperfectionsby grinding if the resultant area meets the dimensional andsurface finish requirements of this section.6.2 Condition:6.2.1 Beta AnnealedMaterial shall be furnishe

20、d in thebeta annealed condition. Two classes of beta annealed sheet,strip, and plate are available. If no class is chosen, Class 1product shall be provided.6.2.2 Alpha + BetaMaterial may be furnished in theannealed, aged, coldworked, hot-rolled, or any combination ofthese conditions.7. Chemical Requ

21、irements7.1 The heat analysis shall conform to the chemical com-position of Table 1. Ingot analysis may be used for reporting allchemical requirements, except hydrogen. Samples for hydro-gen shall be taken from the finished mill product, and thesupplier shall not ship material with chemistry outside

22、 therequirements specified in Table 1.7.1.1 Requirements for the major and minor elementalconstituents are listed in Table 1. Also listed are importantresidual elements.Analysis for elements not listed in Table 1 isnot required to verify compliance with this specification.7.2 Product Analysis:7.2.1

23、Product analysis tolerances do not broaden the speci-fied heat analysis requirements but cover variations betweenlaboratories in the measurement of chemical content. Themanufacturer shall not ship material that is outside the limitsspecified in Table 1. The product analysis tolerances shallconform t

24、o the product tolerances in Table 2.7.2.2 The product analysis is either for the purpose ofverifying the composition of a heat or manufacturing lot or todetermine variations in the composition within the heat.7.2.3 Acceptance or rejection of a heat or manufacturing lotof material may be made by the

25、purchaser on the basis of thisproduct analysis. Product analyses outside the tolerance limitsallowed in Table 2 are cause for rejection of the product. Areferee analysis may be used if agreed upon by the supplier andpurchaser.7.2.4 For referee purposes, use Test Methods, E1409,E1447, and E2371 or ot

26、her analytical methods agreed uponbetween the purchaser and the supplier.7.3 Samples for chemical analysis are representative of thematerial being tested. The utmost care must be used insampling titanium for chemical analysis because of its affinityfor elements such as oxygen, nitrogen, and hydrogen

27、. Incutting samples for analysis, therefore, the operation should becarried out insofar as possible in a dust-free atmosphere.Cutting tools should be clean and sharp. Samples for analysisshould be stored in suitable containers.8. Mechanical Requirements8.1 The material supplied under this specificat

28、ion shallconform to the mechanical property requirements in Table 3 orTable 4.8.2 Specimens for tension tests shall be machined and testedin accordance with Test Methods E8. Tensile properties shallbe determined using a strain rate of 0.003 to 0.007 in./in./min(mm/mm/min) through the specified yield

29、 and then the cross-head speed shall be increased so as to produce fracture inapproximately one additional minute.8.3 For sheet and strip, the bend test specimen shall with-stand being bent cold through an angle of 105 without fracturein the outside surface of the bend portion. The bend shall bemade

30、 over a mandrel with a diameter equal to that shown inTable 4. Test conditions shall conform to Test Method E290.8.4 Number of Tests:8.4.1 Bar, Forging Bar, Shapes, and WirePerform at leastone tension test from each lot in the longitudinal direction.Should this test result not meet the specified req

31、uirements, testtwo additional test pieces representative of the same lot, in theTABLE 1 Chemical RequirementsElement Composition, %, (Mass/Mass)Nitrogen, max 0.05Carbon, max 0.10Hydrogen, max 0.015Iron, max 0.10Oxygen, max 0.20Molybdenum 14.00-16.00TitaniumAbalanceAThe percentage of titanium is dete

32、rmined by difference and need not bedetermined or certified.TABLE 2 Product Analysis TolerancesAElementTolerance Under the Minimum or Over theMaximum LimitB, %, (Mass/Mass)Nitrogen 0.02Carbon 0.02Hydrogen 0.0020Iron 0.10Oxygen 0.02Molybdenum 0.25ARefer to AMS 2249.BUnder the minimum limit not applic

33、able for elements in which only a maximumpercentage is indicated.F2066 112same manner, for each failed test piece. The lot shall beconsidered in compliance only if all additional test pieces meetthe specified requirements.8.4.2 Tensile test results for which any specimen fracturesoutside the gage le

34、ngth shall be considered acceptable, if boththe elongation and the reduction of area meet the minimumrequirements specified. Refer to sections 7.11.4 and 7.12.5 ofTest Methods E8. If either the elongation or reduction of areais less than the minimum requirement, discard the test andretest. Retest on

35、e specimen for each specimen that did not meetthe minimum requirements.8.4.3 Sheet, Strip, and PlatePerform at least one tensiontest from each lot in the longitudinal direction. Perform at leastone bend test from each lot in both the longitudinal andtransverse directions. Tests in the transverse dir

36、ection need bemade only on product from which a specimen not less than 8.0in. (200 mm) in length for sheet, and 2.50 in. (64 mm) in lengthfor plate can be taken. Should any of these test pieces not meetthe specified requirements, test two additional test piecesrepresentative of the same lot, in the

37、same manner, for eachfailed test pieces. The lot shall be considered in complianceonly if all additional test pieces meet the specified require-ments.9. Special Requirements9.1 Microstructure:9.1.1 Beta AnnealedThe microstructure shall consist of afully recrystallized beta phase structure. Primary a

38、lpha andalpha prime (also known as martensitic alpha) are not permit-ted in the microstructure when viewed at 1003 magnification.The grain size in the annealed condition shall be 5 or finer, inaccordance with Test Methods E112.9.1.2 Alpha + BetaThe microstructure shall be a finedispersion of the alp

39、ha and beta phases resulting from process-ing in the alpha plus beta field. There shall be no continuousalpha network at prior beta grain boundaries. There shall be nocoarse, elongated alpha platelets.9.2 Determine the beta transus temperature for each heat bya suitable method and report on the mate

40、rial certification ifrequired by the purchaser.9.3 Alpha case is not permitted for products supplied with amachined, ground, or chemically milled surface finish. Forother products, there will be no continuous layer of alpha casewhen examined at 1003 magnification.10. Significance of Numerical Limits

41、10.1 The following applies to all specified numerical limitsin this specification. To determine conformance to these limits,an observed or calculated value shall be rounded to the nearestunit in the last right-hand digit used in expressing the specifi-cation limit, in accordance with the rounding me

42、thod ofPractice E29.11. Certification11.1 The supplier shall provide a certification that thematerial was tested in accordance with this specification andmet all requirements. A report of the test results shall befurnished to the purchaser at the time of shipment.12. Quality Program Requirements12.1

43、 The supplier shall maintain a quality program such asdefined in ASQ C1 or ISO 9001.13. Keywords13.1 metals (for surgical implants); orthopaedic medicaldevices; titanium alloys; titanium alloys (for surgical implants)TABLE 3 Mechanical PropertiesBar and WireConditionAUltimateTensile Strength,min, ps

44、i (MPa)Yield Strength(0.2 % Offset),min, psi (MPa)ElongationBin2 in. (50 mm)4D or 4W,min, %Reduction ofArea, min, %Beta annealed 100 000 (690) 70 000 (483) 20 60Alpha + BetaC,D130 500 (900) 116 000 (800) 10 25AMechanical properties for conditions other than those listed in this table may be establis

45、hed by agreement between the supplier and purchaser.BElongation of material 0.063 in. (1.6 mm) or greater in diameter (D) or width (W) shall be measured using a gage length of 2 in. or 4D or 4W. The gage length mustbe reported with the test results. The method for determining elongation of material

46、under 0.063 in. (1.6 mm) in diameter or thickness may be negotiated. Alternatively,a gage length corresponding to ISO 6892 may be used when agreed upon between supplier and purchaser. (5.65 times the square root of So, where So is the originalcross sectional area.) Gage length will be reported with

47、the elongation value.CMechanical properties for the hot rolled condition may be established by agreement between the supplier and purchaser.DUp to 4.00-in. (101.60-mm) diameter or thickness.TABLE 4 Mechanical PropertiesSheet, Strip, and PlateABend Test Mandrel DiameterBConditionAUltimateTensile Stre

48、ngth,min, psi (MPa)Yield Strength(0.2 % Offset),min, psi (MPa)ElongationCin2in.(50 mm), min, %Under 0.070 in.(1.78 mm)in Thickness0.070 to 0.1875 in.(1.78 to 4.76 mm)in ThicknessBeta annealed, Class 1 105 000 (724) 80 000 (552) 12 5T 6TBeta annealed, Class 2 100 000 (690) 70 000 (483) 20 5T 6TAMecha

49、nical properties for conditions other than those listed in this table may be established by agreement between the supplier and purchaser.BT equals the thickness of the bend test specimen. Bend tests are not applicable to material over 0.1875 in. (4.76 mm) in thickness. The limits listed apply to tests takenboth longitudinally and transversely to the direction of rolling.CElongation of material 0.063 in. (1.6 mm) or greater in diameter (D) or width (W) shall be measured using a gage length of 2 in. or 4D or 4W. The gage length mustbe reported with the test r