ASTM B265-2010 Standard Specification for Titanium and Titanium Alloy Strip Sheet and Plate《钛及钛合金带材、薄板材和厚板材的标准规范》.pdf

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1、Designation: B265 10Standard Specification forTitanium and Titanium Alloy Strip, Sheet, and Plate1This standard is issued under the fixed designation B265; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision.

2、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 Department of Defense.1. Scope*1.1 This specification2covers annealed titanium and tit

3、a-nium alloy strip, sheet, and plate as follows:1.1.1 Grade 1Unalloyed titanium,1.1.2 Grade 2Unalloyed titanium,1.1.2.1 Grade 2HUnalloyed titanium (Grade 2 with 58ksi minimum UTS),1.1.3 Grade 3Unalloyed titanium,1.1.4 Grade 4Unalloyed titanium,1.1.5 Grade 5Titanium alloy (6 % aluminum, 4 % vana-dium

4、),1.1.6 Grade 6Titanium alloy (5 % aluminum, 2.5 % tin),1.1.7 Grade 7Unalloyed titanium plus 0.12 to 0.25 %palladium,1.1.7.1 Grade 7HUnalloyed titanium plus 0.12 to 0.25 %palladium (Grade 7 with 58 ksi minimum UTS),1.1.8 Grade 9Titanium alloy (3.0 % aluminum, 2.5 %vanadium),1.1.9 Grade 11Unalloyed t

5、itanium plus 0.12 to 0.25 %palladium,1.1.10 Grade 12Titanium alloy (0.3 % molybdenum,0.8 % nickel),1.1.11 Grade 13Titanium alloy (0.5 % nickel, 0.05 %ruthenium),1.1.12 Grade 14Titanium alloy (0.5 % nickel, 0.05 %ruthenium),1.1.13 Grade 15Titanium alloy (0.5 % nickel, 0.05 %ruthenium),1.1.14 Grade 16

6、Unalloyed titanium plus 0.04 to 0.08 %palladium,1.1.14.1 Grade 16HUnalloyed titanium plus 0.04 to0.08 % palladium (Grade 16 with 58 ksi minimum UTS),1.1.15 Grade 17Unalloyed titanium plus 0.04 to 0.08 %palladium,1.1.16 Grade 18Titanium alloy (3 % aluminum, 2.5 %vanadium) plus 0.04 to 0.08 % palladiu

7、m,1.1.17 Grade 19Titanium alloy (3 % aluminum, 8 %vanadium, 6 % chromium, 4 % zirconium, 4 % molybdenum),1.1.18 Grade 20Titanium alloy (3 % aluminum, 8 %vanadium, 6 % chromium, 4 % zirconium, 4 % molybdenum)plus 0.04 % to 0.08 % palladium,1.1.19 Grade 21Titanium alloy (15 % molybdenum, 3 %aluminum,

8、2.7 % niobium, 0.25 % silicon),1.1.20 Grade 23Titanium alloy (6 % aluminum, 4 %vanadium with extra low interstitial elements, ELI),1.1.21 Grade 24Titanium alloy (6 % aluminum, 4 %vanadium) plus 0.04 % to 0.08 % palladium,1.1.22 Grade 25Titanium alloy (6 % aluminum, 4 %vanadium) plus 0.3 % to 0.8 % n

9、ickel and 0.04 % to 0.08 %palladium,1.1.23 Grade 26Unalloyed titanium plus 0.08 to 0.14 %ruthenium,1.1.23.1 Grade 26HUnalloyed titanium plus 0.08 to0.14 % ruthenium (Grade 26 with 58 ksi minimum UTS),1.1.24 Grade 27Unalloyed titanium plus 0.08 to 0.14 %ruthenium,1.1.25 Grade 28Titanium alloy (3 % al

10、uminum, 2.5 %vanadium) plus 0.08 to 0.14 % ruthenium,1.1.26 Grade 29Titanium alloy (6 % aluminum, 4 %vanadium with extra low interstitial elements, ELI) plus 0.08 to0.14 % ruthenium,1.1.27 Grade 30Titanium alloy (0.3 % cobalt, 0.05 %palladium),1.1.28 Grade 31Titanium alloy (0.3 % cobalt, 0.05 %palla

11、dium),1.1.29 Grade 32Titanium alloy (5 % aluminum, 1 % tin,1 % zirconium, 1 % vanadium, 0.8 % molybdenum),1.1.30 Grade 33Titanium alloy (0.4 % nickel, 0.015 %palladium, 0.02 5 % ruthenium, 0.15 % chromium),1.1.31 Grade 34Titanium alloy (0.4 % nickel, 0.015 %palladium, 0.025 % ruthenium, 0.15 % chrom

12、ium),1.1.32 Grade 35Titanium alloy (4.5 % aluminum, 2 %molybdenum, 1.6 % vanadium, 0.5 % iron, 0.3 % silicon),1This specification is under the jurisdiction of ASTM Committee B10 onReactive and Refractory Metals and Alloys and is the direct responsibility ofSubcommittee B10.01 on Titanium.Current edi

13、tion approved May 1, 2010. Published May 2010. Originallyapproved in 1952. Last previous edition approved in 2009 as B265 09a1. DOI:10.1520/B0265-10.2For ASME Boiler and Pressure Vessel Code applications see related Specifi-cations SB-265 in Section II of that Code.1*A Summary of Changes section app

14、ears at the end of this standard.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.1.1.33 Grade 36Titanium alloy (45 % niobium),1.1.34 Grade 37Titanium alloy (1.5 % aluminum), and1.1.35 Grade 38Titanium alloy (4 % aluminum, 2.5 %vanadiu

15、m, 1.5 % iron).NOTE 1H grade material is identical to the corresponding numericgrade (that is, Grade 2H = Grade 2) except for the higher guaranteedminimum UTS, and may always be certified as meeting the requirementsof its corresponding numeric grade. Grades 2H, 7H, 16H, and 26H areintended primarily

16、 for pressure vessel use.The H grades were added in response to a user association request basedon its study of over 5200 commercial Grade 2, 7, 16, and 26 test reports,where over 99 % met the 58 ksi minimum UTS.1.2 The values stated in inch-pound units are to be regardedas standard. The values give

17、n in parentheses are mathematicalconversions to SI units that are provided for information onlyand are not considered standard.2. Referenced Documents2.1 ASTM Standards:3E8 Test Methods for Tension Testing of Metallic MaterialsE29 Practice for Using Significant Digits in Test Data toDetermine Confor

18、mance with SpecificationsE290 Test Methods for Bend Testing of Material for Duc-tilityE539 Test Method for X-Ray Fluorescence SpectrometricAnalysis of 6Al-4V Titanium AlloyE1409 Test Method for Determination of Oxygen andNitrogen in Titanium and Titanium Alloys by the Inert GasFusion TechniqueE1447

19、Test Method for Determination of Hydrogen inTitanium and Titanium Alloys by Inert Gas Fusion Ther-mal Conductivity/Infrared Detection MethodE1941 Test Method for Determination of Carbon in Refrac-tory and Reactive Metals and Their AlloysE2371 Test Method for Analysis of Titanium and TitaniumAlloys b

20、y Atomic Emission Plasma SpectrometryE2626 Guide for Spectrometric Analysis of Reactive andRefractory Metals3. Terminology3.1 Definitions of Terms Specific to This Standard:3.1.1 Any product 0.187 in. (4.75 mm) and under inthickness and less than 24 in. (610 mm) in width is classifiedas strip; produ

21、cts 0.187 in. (4.75 mm) and under in thicknessand 24 in. (610 mm) or more in width are classified as sheet;any product over 0.187 in. (4.75 mm) in thickness and over 10in. (254 mm) in width is classified as plate.4. Ordering Information4.1 Orders for materials under this specification shall in-clude

22、 the following information as applicable:4.1.1 Grade number (Section 1),4.1.2 Product limitations (Section 3),4.1.3 Special mechanical properties (Table 1),4.1.4 Marking (Section 16),4.1.5 Finish (Section 8),4.1.6 Packaging (Section 16),4.1.7 Additional required reports (Section 15), and4.1.8 Dispos

23、ition of rejected material (Section 14).5. Chemical Composition5.1 The grades of titanium and titanium alloy metal coveredby this specification shall conform to the chemical compositionrequirements prescribed in Table 2.5.1.1 The elements listed in Table 2 are intentional alloyadditions or elements

24、which are inherent to the manufacture oftitanium sponge, ingot or mill product.5.1.1.1 Elements other than those listed in Table 2 aredeemed to be capable of occurring in the grades listed in Table2 by and only by way of unregulated or unanalyzed scrapadditions to the ingot melt. Therefore, product

25、analysis forelements not listed in Table 2 shall not be required unlessspecified and shall be considered to be in excess of the intentof this specification.5.1.2 Elements intentionally added to the melt must beidentified, analyzed, and reported in the chemical analysis.5.2 When agreed upon by produc

26、er and purchaser andrequested by the purchaser in his written purchase order,chemical analysis shall be completed for specific residualelements not listed in this specification.5.3 Product AnalysisProduct analysis tolerances do notbroaden the specified heat analysis requirements but covervariations

27、between laboratories in the measurement of chemi-cal content. The manufacturer shall not ship material that isoutside the limits specified in Table 2 for the applicable grade.Product analysis limits shall be as specified in Table 3.5.4 At least two samples for chemical analysis shall betested to det

28、ermine chemical composition. Samples shall betaken from the ingot or the extremes of the product to beanalyzed.6. Mechanical Properties6.1 Material supplied under this specification shall conformto the mechanical property requirements given in Table 1 forthe grade specified.6.2 Tension testing speci

29、mens are to 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./minthrough the specified yield strength, and then increasing therate so as to produce failure in approximately one additionalminute.6.3 For sheet

30、and strip, the bend test specimen shall with-stand being bent cold through an angle of 105 without fracturein the outside of the bent portion. The bend shall be made ona radius equal to that shown in Table 1 for the applicablegrade. The bends are to be made in accordance with TestMethod E290, using

31、Method 1, Guided Bend Test described inparagraph 3.6, bent through 105, and allowed to spring backnaturally. The surface of the specimen must include the originalmaterial surface with no material removal or surface condi-tioning, except corners may be rounded to a maximum radiusof 0.032 in. (0.8 mm)

32、. The width of the bend shall be at least3For 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 standards Document Summary page onthe ASTM website.B265 1025 times the

33、thickness. The test report shall, at minimum,indicate acceptable or unacceptable results.7. Permissible Variations in Dimensions7.1 Dimensional tolerances on titanium and titanium alloymaterial covered by this specification shall be as specified inTables 4-13, as applicable.8. Finish8.1 Titanium and

34、 titanium alloy sheet, strip, and plate shallbe free of injurious external and internal imperfections of anature that will interfere with the purpose for which it isintended. Annealed material may be furnished as descaled, assandblasted, or as ground, or both sandblasted and ground. Ifshipped as des

35、caled, sandblasted, or ground, the manufacturershall be permitted to remove minor surface imperfections byspot grinding if such grinding does not reduce the thickness ofthe material below the minimum permitted by the tolerance forthe thickness ordered.9. Sampling for Chemical Analysis9.1 Samples for

36、 chemical analysis shall be representative ofthe material being tested. The utmost care must be used insampling titanium for chemical analysis because of its greataffinity for elements such as oxygen, nitrogen, and hydrogen.Therefore, in cutting samples for analysis, the operation shouldTABLE 1 Tens

37、ile RequirementsAGradeTensile Strength, min Yield Strength, 0.2 % OffsetElongation in2 in. or 50 mm,min, %Bend Test (Radius of Mandrel)Bksi MPamin max Under 0.070 in.(1.8 mm) inThickness0.070 to 0.187 in.(1.84.75 mm) inThicknessksi MPa ksi MPa1 35 240 20 138 45 310 24 1.5T 2T2 50 345 40 275 65 450 2

38、0 2T 2.5T2HC,D58 400 40 275 65 450 20 2T 2T3 65 450 55 380 80 550 18 2T 2.5T4 80 550 70 483 95 655 15 2.5T 3T5 130 895 120 828 . . 10E4.5T 5T6 120 828 115 793 . . 10E4T 4.5T7 50 345 40 275 65 450 20 2T 2.5T7HC,D58 400 40 275 65 450 20 2T 2T9 90 620 70 483 . . 15F2.5T 3T11 35 240 20 138 45 310 24 1.5

39、T 2T12 70 483 50 345 . . 18 2T 2.5T13 40 275 25 170 . . 24 1.5T 2T14 60 410 40 275 . . 20 2T 2.5T15 70 483 55 380 . . 18 2T 2.5T16 50 345 40 275 65 450 20 2T 2.5T16HC,D58 400 40 275 65 450 20 2T 2T17 35 240 20 138 45 310 24 1.5T 2T18 90 620 70 483 . . 15F2.5T 3T19G,H115 793 110 759 . . 15 3T 3T20G,H

40、115 793 110 759 . . 15 3T 3T21G,H115 793 110 759 . . 15 3T 3T23G,H120 828 110 759 . . 10 4.5T 5T24 130 895 120 828 . . 10 4.5T 5T25 130 895 120 828 . . 10 4.5T 5T26 50 345 40 275 65 450 20 2T 2.5T26HC,D58 400 40 275 65 450 20 2T 4T27 35 240 20 138 45 310 24 1.5T 2T28 90 620 70 483 . . 15 2.5T 3T29 1

41、20 828 110 759 . . 10 4.5T 5T30 50 345 40 275 65 450 20 2T 2.5T31 65 450 55 380 80 550 18 2T 2.5T32 100 689 85 586 . . 10E3.5T 4.5T33 50 345 40 275 65 450 20 2T 2.5T34 65 450 55 380 80 550 18 2T 2.5T35 130 895 120 828 . . 5 8T 8T36 65 450 60 410 95 655 10 4.5T 5T37 50 345 31 215 65 450 20 2T 2.5T38

42、130 895 115 794 . . 10 4T 4.5TAMinimum and maximum limits apply to tests taken both longitudinal and transverse to the direction of rolling. Mechanical properties for conditions other than annealedor plate thickness over 1 in. (25 mm) may be established by agreement between the manufacturer and the

43、purchaser.BBend to Radius of Mandrel, T equals the thickness of the bend test specimen. Bend tests are not applicable to material over 0.187 in. (4.75 mm) in thickness.CMaterial is identical to the corresponding numeric grade (that is, Grade 2H = Grade 2) except for the higher guaranteed minimum UTS

44、, and may always be certifiedas meeting the requirements of its corresponding numeric grade. Grade 2H, 7H, 16H, and 26H are intended primarily for pressure vessel use.DThe H grades were added in response to a user association request based on its study of over 5200 commercial Grade 2, 7, 16, and 26

45、test reports, where over 99 %met the 58 ksi minimum UTS.EFor Grades 5, 6 and 32 the elongation on materials under 0.025 in. (0.635 mm) in thickness may be obtained only by negotiation.FElongation for continuous rolled and annealed (strip product from coil) for Grade 9 and Grade 18 shall be 12 % mini

46、mum in the longitudinal direction and 8 % minimumin the transverse direction.GProperties for material in the solution treated condition.HMaterial is normally purchased in the solution treated condition. Therefore, properties for aged material shall be negotiated between manufacturer and purchaser.B2

47、65 103TABLE 2 Chemical RequirementsComposition, Weight PercentA,B,C,D,EGradeCarbon,max.Oxygenrangeor max.Nitrogen,max.Hydrogen,max.Ironrangeor max. Aluminum Vanadium Palladium Ruthenium Nickel Molybdenum Chromium Cobalt Zirconium Niobium Tin SiliconOtherElements,max.eachOtherElements,max.total1 0.08

48、 0.18 0.03 0.015 0.20 - - - - - - - - - - - - 0.1 0.42 0.08 0.25 0.03 0.015 0.30 - - - - - - - - - - - - 0.1 0.42H 0.08 0.25 0.03 0.015 0.30 - - - - - - - - - - - - - - - - - - - - - - - - 0.1 0.43 0.08 0.35 0.05 0.015 0.30 - - - - - - - - - - - - 0.1 0.44 0.08 0.40 0.05 0.015 0.50 - - - - - - - - -

49、 - - - 0.1 0.45 0.08 0.20 0.05 0.015 0.40 5.5-6.75 3.5-4.5 - - - - - - - - - - - - - - - - - - - - 0.1 0.46 0.08 0.20 0.03 0.015 0.50 4.0-6.0 - - - - - - - - - - - - - - - - - - 2.0-3.0 - - 0.1 0.47 0.08 0.25 0.03 0.015 0.30 - - 0.12-0.25 - - - - - - - - - 0.1 0.47H 0.08 0.25 0.03 0.015 0.30 - - - - 0.12-0.25 - - - - - - - - - - - - - - - - - - 0.1 0.49 0.08 0.15 0.03 0.015 0.25 2.5-3.5 2.0-3.0 - - - - - - - - - - 0.1 0.411 0.08 0.18 0.03 0.015 0.20 - - - - 0.12-0.25 -

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