ASTM B265-2013a Standard Specification for Titanium and Titanium Alloy Strip Sheet and Plate《钛及钛合金带材、薄板材及板材标准规格》.pdf

1、Designation: B265 13aStandard 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 ti

3、ta-nium alloy strip, sheet, and plate as follows:1.1.1 Grade 1UNS R50250. Unalloyed titanium,1.1.2 Grade 2UNS R50400. Unalloyed titanium,1.1.2.1 Grade 2HUNS R50400. Unalloyed titanium(Grade 2 with 58 ksi (400 MPa) minimum UTS),1.1.3 Grade 3UNS R50550. Unalloyed titanium,1.1.4 Grade 4UNS R50700. Unal

4、loyed titanium,1.1.5 Grade 5UNS R56400. Titanium alloy (6 %aluminum, 4 % vanadium),1.1.6 Grade 6UNS R54520. Titanium alloy (5 %aluminum, 2.5 % tin),1.1.7 Grade 7UNS R52400. Unalloyed titanium plus 0.12to 0.25 % palladium,1.1.7.1 Grade 7HUNS R52400. Unalloyed titanium plus0.12 to 0.25 % palladium (Gr

5、ade 7 with 58 ksi (400 MPa)minimum UTS),1.1.8 Grade 9UNS R56320. Titanium alloy (3.0 %aluminum, 2.5 % vanadium),1.1.9 Grade 11UNS R52250. Unalloyed titanium plus0.12 to 0.25 % palladium,1.1.10 Grade 12UNS R53400. Titanium alloy (0.3 %molybdenum, 0.8 % nickel),1.1.11 Grade 13UNS R53413. Titanium allo

6、y (0.5 %nickel, 0.05 % ruthenium),1.1.12 Grade 14UNS R53414. Titanium alloy (0.5 %nickel, 0.05 % ruthenium),1.1.13 Grade 15UNS R53415. Titanium alloy (0.5 %nickel, 0.05 % ruthenium),1.1.14 Grade 16UNS R52402. Unalloyed titanium plus0.04 to 0.08 % palladium,1.1.14.1 Grade 16HUNS R52402. Unalloyed tit

7、aniumplus 0.04 to 0.08 % palladium (Grade 16 with 58 ksi (400MPa) minimum UTS),1.1.15 Grade 17UNS R52252. Unalloyed titanium plus0.04 to 0.08 % palladium,1.1.16 Grade 18UNS R56322. Titanium alloy (3 %aluminum, 2.5 % vanadium) plus 0.04 to 0.08 % palladium,1.1.17 Grade 19UNS R58640. Titanium alloy (3

8、 %aluminum, 8 % vanadium, 6 % chromium, 4 % zirconium, 4 %molybdenum),1.1.18 Grade 20UNS R58645. Titanium alloy (3 %aluminum, 8 % vanadium, 6 % chromium, 4 % zirconium, 4 %molybdenum) plus 0.04 % to 0.08 % palladium,1.1.19 Grade 21UNS R58210. Titanium alloy (15 %molybdenum, 3 % aluminum, 2.7 % niobi

9、um, 0.25 % silicon),1.1.20 Grade 23UNS R56407. Titanium alloy (6 %aluminum, 4 % vanadium with extra low interstitial elements,ELI),1.1.21 Grade 24UNS R56405. Titanium alloy (6 %aluminum, 4 % vanadium) plus 0.04 % to 0.08 % palladium,1.1.22 Grade 25UNS R56403. Titanium alloy (6 %aluminum, 4 % vanadiu

10、m) plus 0.3 % to 0.8 % nickel and0.04 % to 0.08 % palladium,1.1.23 Grade 26UNS R52404. Unalloyed titanium plus0.08 to 0.14 % ruthenium,1.1.23.1 Grade 26HUNS R52404. Unalloyed titaniumplus 0.08 to 0.14 % ruthenium (Grade 26 with 58 ksi (400MPa) minimum UTS),1.1.24 Grade 27UNS R52254. Unalloyed titani

11、um plus0.08 to 0.14 % ruthenium,1.1.25 Grade 28UNS R56323. Titanium alloy (3 %aluminum, 2.5 % vanadium) plus 0.08 to 0.14 % ruthenium,1.1.26 Grade 29UNS R56404. Titanium alloy (6 %aluminum, 4 % vanadium with extra low interstitial elements,ELI) plus 0.08 to 0.14 % ruthenium,1.1.27 Grade 30UNS R53530

12、. Titanium alloy (0.3 %cobalt, 0.05 % palladium),1.1.28 Grade 31UNS R53532. Titanium alloy (0.3 %cobalt, 0.05 % palladium),1.1.29 Grade 32UNS R55111. Titanium alloy (5 %aluminum, 1 % tin, 1 % zirconium, 1 % vanadium, 0.8 %molybdenum),1.1.30 Grade 33UNS R53442. Titanium alloy (0.4 %nickel, 0.015 % pa

13、lladium, 0.02 5 % ruthenium, 0.15 %chromium),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 edition approved July 1, 2013. Published August 2013. Originallyappr

14、oved in 1952. Last previous edition approved in 2013 as B265 13. DOI:10.1520/B0265-13A.2For ASME Boiler and Pressure Vessel Code applications see related Specifi-cations SB-265 in Section II of that Code.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 1

15、00 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States11.1.31 Grade 34UNS R53445. Titanium alloy (0.4 %nickel, 0.015 % palladium, 0.025 % ruthenium, 0.15 %chromium),1.1.32 Grade 35UNS R56340. Titanium alloy (4.5 %aluminum, 2 % molybdenum, 1.6 % vanadium, 0.5 % iron,0.3 %

16、silicon),1.1.33 Grade 36UNS R58450. Titanium alloy (45 %niobium),1.1.34 Grade 37UNS R52815. Titanium alloy (1.5 %aluminum),1.1.35 Grade 38UNS R54250. Titanium alloy (4 %aluminum, 2.5 % vanadium, 1.5 % iron), and1.1.36 Grade 39UNS R53390. Titanium alloy (0.25 %iron, 0.4 % silicon).NOTE 1H grade mater

17、ial 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 for pressure vessel use.1.2 The v

18、alues 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. Referenced Documents2.1 ASTM Standards:3E8 Test Methods for Tension Testing of Metallic Mat

19、erialsE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with SpecificationsE290 Test Methods for Bend Testing of Material for Ductil-ityE539 Test Method forAnalysis of TitaniumAlloys by X-RayFluorescence SpectrometryE1409 Test Method for Determination of Oxygen and Nitro

20、-gen in Titanium and Titanium Alloys by the Inert GasFusion TechniqueE1447 Test Method for Determination of Hydrogen in Tita-nium and Titanium Alloys by Inert Gas Fusion ThermalConductivity/Infrared Detection MethodE1941 Test Method for Determination of Carbon in Refrac-tory and Reactive Metals and

21、TheirAlloys by CombustionAnalysisE2371 Test Method for Analysis of Titanium and TitaniumAlloys by Direct Current Plasma and Inductively CoupledPlasma Atomic Emission Spectrometry (Performance-Based Test Methodology)E2626 Guide for Spectrometric Analysis of Reactive andRefractory Metals3. Terminology

22、3.1 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; 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 ove

23、r 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 the following information as applicable:4.1.1 Grade number (Section 1),4.1.2 Product limitations (Section 3),4.1.3 Specia

24、l 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 Disposition of rejected material (Section 14).5. Chemical Composition5.1 The grades of titanium and titanium alloy metal covered

25、by 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 which are inherent to the manufacture oftitanium sponge, ingot or mill product.5.1.1.1 Elements other than those listed in

26、 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 analysis forelements not listed in Table 2 shall not be required unlessspecified and shall be considered to be in excess o

27、f 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 producer and purchaser andrequested by the purchaser in his written purchase order,chemical analysis shall be completed for spec

28、ific residualelements not listed in this specification.5.3 Product AnalysisProduct analysis tolerances do notbroaden the specified heat analysis requirements but covervariations between laboratories in the measurement of chemi-cal content. The manufacturer shall not ship material that isoutside the

29、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 determine chemical composition. Samples shall betaken from the ingot or the extremes of the product to beanalyzed.6. Mechanic

30、al Properties6.1 Material supplied under this specification shall conformto the mechanical property requirements given in Table 1 forthe grade specified.6.2 Tension testing specimens are to be machined and testedin accordance with Test Methods E8. Tensile properties shallbe determined using a strain

31、 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.3For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Boo

32、k of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.B265 13a26.3 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 radi

33、us equal to that shown in Table 1 for the applicablegrade. The bends are to be made in accordance with 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 sur

34、face with no material removal or surfaceconditioning, except corners may be rounded to a maximumradius of 0.032 in. (0.8 mm). The width of the bend shall be atleast 5 times the thickness. The test report shall, at minimum,indicate acceptable or unacceptable results.7. Permissible Variations in Dimen

35、sions7.1 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 titanium alloy sheet, strip, and plate shallbe free of injurious external and internal imperfections of anature that will

36、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 descaled, sandblasted, or ground, the manufacturerTABLE 1 Tensile RequirementsAGradeTensile Strength, min Yield Strength, 0.2

37、% 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 20 2T 2.5T2HC,D58 400 40 275 65 450 20 2T 2T3 65 450 55 380 80 55

38、0 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 1.5T 2T12 70 483 50 345 . . 18 2T 2.5T13 40 275 25 170 . . 24 1.5T

39、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,H115 793 110 759 . . 15 3T 3T21G,H115 793 110 759 . . 15 3T 3T23

40、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 70 483 . . 15 2.5T 3T29 120 828 110 759 . . 10 4.5T 5T30 50 345 40 275 65 450 20 2T 2.5T31

41、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 130 895 115 794 . . 10 4T 4.5T39 75 515 60 410 90 620 20 2T 2.5TAM

42、inimum 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 purchaser.BBend to Radius of Man

43、drel, 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, and may always be certified as

44、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 test reports, where over 99 %met

45、 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 % minimum in the longitudinal directio

46、n 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.B265 13a3TABLE2ChemicalRequirement

47、sComposition,WeightPercentA,B,C,D,EGradeUNSNumberCarbon,max.Oxygenrangeormax.Nitrogen,max.Hydrogen,max.Ironrangeormax.AluminumVanadiumPalladiumRutheniumNickelMolybdenumChromiumCobaltZirconiumNiobiumTinSiliconOtherElements,max. eachOtherElements,max.total1R502500.080.180.030.0150.20-0.10.42/2HR504000

48、.080.250.030.0150.30-0.10.43R505500.080.350.050.0150.30-0.10.44R507000.080.400.050.0150.50-0.10.45R564000.080.200.050.0150.405.5- 6.753.5-4.5-0.10.46R545200.080.200.030.0150.504.0-6.0-2.0-3.0-0.10.47/7HR524000.080.250.030.0150.30-0.12-0.25-0.10.49R563200.080.150.030.0150.252.5-3.52.0-3.0-0.10.411R522500.080.180.030.0150.20-0.12-0.25-0.10.412R534000.080.250.030.0150.30-0.6-0.90.2-0.4-0.10.413R534130.080.100.030.0150.20-0.04-0.060.4-0.6-0.10.414R534140.080.150.030.0150.30-0.04-0.060.4-0.6-0.10.415R534150.080.250.050.0150.30-0.04-0.060.4-0.6-0.10.416/16HR524020.080.250.030.0150.