ASTM B265-2011 Standard Specification for Titanium and Titanium Alloy Strip Sheet and Plate《钛及钛合金条板 薄板及中厚板标准规格》.pdf

1、Designation: B265 11Standard 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 Sept. 1, 2011. Published September 2011. Originallyapproved in 1952. Last previous edition approved in 2010 as B265 10. DOI:10.1520/B0265-11.2For ASME Boiler and Pressure Vessel Code applications see related Specifi-cations SB-265 in Section II of that Code.1*A Summary of Changes secti

14、on appears 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 %v

15、anadium, 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 pri

16、marily 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 value

17、s given 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

18、Conformance with SpecificationsE290 Test Methods for Bend Testing of Material for Duc-tilityE539 Test Method for Analysis of Titanium Alloys byX-Ray Fluorescence SpectrometryE1409 Test Method for Determination of Oxygen andNitrogen in Titanium and Titanium Alloys by the Inert GasFusion TechniqueE144

19、7 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 Alloys by CombustionAnalysisE2371 Test Method for Analysis of Titan

20、ium and TitaniumAlloys by 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 c

21、lassifiedas strip; products 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 spec

22、ification shall in-clude 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 (Sect

23、ion 15), and4.1.8 Disposition 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 all

24、oyadditions or elements 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 m

25、elt. Therefore, product 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 Wh

26、en agreed upon by producer 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 requireme

27、nts but covervariations 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 analys

28、is shall betested to determine 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

29、.2 Tension testing specimens 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 additio

30、nalminute.6.3 For sheet 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

31、 TestMethod E290, using 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 rad

32、iusof 0.032 in. (0.8 mm). 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 webs

33、ite.B265 1125 times the 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

34、. Finish8.1 Titanium and 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

35、ground. Ifshipped as descaled, 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

36、 Analysis9.1 Samples for 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 oper

37、ation shouldTABLE 1 Tensile 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 2T

38、2 50 345 40 275 65 450 20 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

39、240 20 138 45 310 24 1.5T 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 1

40、10 759 . . 15 3T 3T20G,H115 793 110 759 . . 15 3T 3T21G,H115 793 110 759 . . 15 3T 3T23 120 828 110 759 . . 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

41、483 . . 15 2.5T 3T29 120 828 110 759 . . 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 21

42、5 65 450 20 2T 2.5T38 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

43、 manufacturer and the 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

44、guaranteed minimum UTS, 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 G

45、rade 2, 7, 16, and 26 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

46、 18 shall be 12 % minimum 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 manufac

47、turer and purchaser.B265 113TABLE 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.eachOtherEl

48、ements,max.total1 0.08 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

49、0.50 - - - - - - - - - - - - 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 0.2