ASTM E1426-1998(2009)e1 Standard Test Method for Determining the Effective Elastic Parameter for X-Ray Diffraction Measurements of Residual Stress《残余应力X-射线缺陷测量效果弹性参数测定的标准试验方法》.pdf

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ASTM E1426-1998(2009)e1 Standard Test Method for Determining the Effective Elastic Parameter for X-Ray Diffraction Measurements of Residual Stress《残余应力X-射线缺陷测量效果弹性参数测定的标准试验方法》.pdf_第1页
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1、Designation: E 1426 98 (Reapproved 2009)1Standard Test Method forDetermining the Effective Elastic Parameter for X-RayDiffraction Measurements of Residual Stress1This standard is issued under the fixed designation E 1426; the number immediately following the designation indicates the year oforiginal

2、 adoption or, in the case of revision, 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.1NOTE9.7 was editorially revised in September 2009.INTRODUCTIONWhen a crystalli

3、ne material is strained the spacings between parallel planes of atoms, ions, ormolecules in the lattice change. X-ray diffraction techniques can measure these changes and, therefore,they constitute a powerful means for studying the residual stress state in a body. To calculatemacroscopic stresses fr

4、om lattice strains requires a material constant, Eeff, called the effective elasticparameter, that must be empirically determined by X-ray diffraction techniques as described in this testmethod.1. Scope1.1 This test method covers a procedure for experimentallydetermining the effective elastic parame

5、ter, Eeff, for the evalu-ation of residual and applied stresses by X-ray diffractiontechniques. The effective elastic parameter relates macroscopicstress to the strain measured in a particular crystallographicdirection in polycrystalline samples. Eeffshould not be con-fused with E, the modulus of el

6、asticity. Rather, it is nominallyequivalent to E/(1 + n) for the particular crystallographicdirection, where n is Poissons ratio. The effective elasticparameter is influenced by elastic anisotropy and preferredorientation of the sample material.1.2 This test method is applicable to all X-ray diffrac

7、tioninstruments intended for measurements of macroscopic re-sidual stress that use measurements of the positions of thediffraction peaks in the high back-reflection region to deter-mine changes in lattice spacing.1.3 This test method is applicable to all X-ray diffractiontechniques for residual stre

8、ss measurement, including single,double, and multiple exposure techniques.1.4 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.1.5 This st

9、andard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Referenced Documents2.1

10、 ASTM Standards:2E4 Practices for Force Verification of Testing MachinesE6 Terminology Relating to Methods of Mechanical Test-ingE7 Terminology Relating to MetallographyE 1237 Guide for Installing Bonded Resistance StrainGages3. Terminology3.1 Definitions:3.1.1 Many of the terms used in this test me

11、thod are definedin Terminology E6and E7.3.2 Definitions of Terms Specific to This Standard:3.2.1 interplanar spacingthe perpendicular distance be-tween adjacent parallel lattice planes.3.2.2 macrostressan average stress acting over a region ofthe test specimen containing many crystals.3.3 Symbols:3.

12、3.1 a = dummy parameter for Sum(a) and SD(a).3.3.2 c = ordinate intercept of a graph of Dd versus stress.3.3.3 d = interplanar spacing between crystallographicplanes; also called d-spacing.3.3.4 d0= interplanar spacing for unstressed material.3.3.5 Dd = change in interplanar spacing caused by stress

13、.1This test method is under the jurisdiction of ASTM Committee E28 onMechanical Testing and is the direct responsibility of Subcommittee E28.13 onResidual Stress Measurement.Current edition approved June 1, 2009. Published September 2009. Originallyapproved in 1991. Last previous edition approved in

14、 2003 as E 1426 98(2003).2For 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.1Copyright ASTM International, 100 B

15、arr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.3.3.6 E = modulus of elasticity.3.3.7 Eeff= effective elastic parameter for X-ray measure-ments.3.3.8 i = measurement index, 1 # i # n.3.3.9 m = slope of a graph of Dd versus stress.3.3.10 n = number of measurements used

16、to determineslope m.3.3.11 SD(a) = standard deviation of a set of quantities “a”.3.3.12 Sum(a) = sum of a set of quantities “a”.3.3.13 Ti=Ximinus mean of all Xivalues.3.3.14 Xi= i-th value of applied stress.3.3.15 Yi= measurement of Dd corresponding to Xi.3.3.16 n = Poissons ratio.3.3.17 c = angle b

17、etween the specimen surface normal andthe normal to the diffracting crystallographic planes.4. Summary of Test Method4.1 A test specimen is prepared from a material that isrepresentative of that of the object in which residual stressmeasurements are to be made.NOTE 1If a sample of the same material

18、is available it should be used.4.2 The test specimen is instrumented with an electricalresistance strain gage, mounted in a location that experiencesthe same stress as the region that will be subsequentlyirradiated with X-rays.4.3 The test specimen is calibrated by loading it in such amanner that th

19、e stress, where the strain gage is mounted, isdirectly calculable, and a calibration curve relating the straingage reading to the stress is developed.4.4 The test specimen is mounted in a loading fixture in anX-ray diffraction apparatus, and sequentially loaded to severalload levels.4.4.1 The change

20、 in interplanar spacing is measured foreach load level and related to the corresponding stress that isdetermined from the strain gage reading and the calibrationcurve.4.5 The effective elastic parameter and its standard devia-tion are calculated from the test results.5. Significance and Use5.1 This

21、test method provides standard procedures forexperimentally determining the effective elastic parameter forX-ray diffraction measurement of residual and applied stresses.It also provides a standard means of reporting the precision ofthe parameter.5.2 This test method is applicable to any crystalline

22、materialwhich exhibits a linear relationship between stress and strain inthe elastic range.5.3 This test method should be used whenever residualstresses are to be evaluated by an X-ray diffraction techniqueand the effective elastic parameter of the material is unknown.6. Apparatus6.1 Any X-ray diffr

23、action instrument intended for measure-ments of residual macrostress that employs measurements ofthe diffraction peaks in the high back-reflection region may beused, including film camera types, diffractometers, and por-table systems.6.2 A loading fixture is required to apply loads to the testspecim

24、en while it is being irradiated in the X-ray diffractioninstrument.6.2.1 The fixture shall be designed such that the surfacestress applied by the fixture shall be uniform over the irradiatedarea of the specimen.6.2.2 The fixture shall maintain the irradiated surface of thespecimen at the exact cente

25、r of rotation of the X-ray diffractioninstrument throughout the test with sufficient precision toprovide the desired levels of precision and bias in the mea-surements to be made.6.2.3 The fixture may be designed to apply tensile orbending loads. A four-point bending technique such as thatdescribed b

26、y Prevey3is most commonly used.6.3 Electrical resistance strain gages are mounted upon thetest specimen to enable it to be accurately stressed to knownlevels.7. Test Specimens7.1 Test specimens should be fabricated from material withmicrostructure as nearly the same as possible as that in themateria

27、l in which residual stresses are to be evaluated.7.2 For use in tensile or four-point bending fixtures, speci-mens should be rectangular in shape.7.2.1 The length of tensile specimens, between grips, shallbe not less than four times the width, and the width-to-thickness ratio shall not exceed eight.

28、7.2.2 For use in four-point bending fixtures, specimensshould have a length-to-width ratio of at least four. Thespecimen width should be sufficient to accommodate straingages (see 7.5) and the width-to-thickness ratio should begreater than one and consistent with the method used tocalculate the appl

29、ied stresses in 8.1.NOTE 2Nominal dimensions often used for specimens for four-pointbending fixtures are 4.0 3 0.75 3 0.06 in. (10.2 3 1.9 3 0.15 cm).7.3 Tapered specimens for use in cantilever bending fix-tures, and split-ring samples, are also acceptable.7.4 Specimen surfaces may be electropolishe

30、d or as-rolledsheet or plate.7.5 One or more electrical resistance strain gages is affixedto the test specimen in accordance with Guide E 1237. Thegage(s) should be aligned parallel to the longitudinal axis of thespecimen, and should be mounted on a region of the specimenthat experiences the same st

31、rain as the region that is to beirradiated. The gage(s) should be applied to the irradiatedsurface of the beam either adjacent to, or on either side of, theirradiated area in order to minimize errors due to the absenceof a pure tensile or bending load.NOTE 3In the case of four-point bending fixtures

32、 the gage(s) shouldbe placed well inside the inner span of the specimen in order to minimizethe stress concentration effects associated with the inner knife edges.3Prevey, P. S., “A Method of Determining the Elastic Properties of Alloys inSelected Crystallographic Directions for X-Ray Diffraction Re

33、sidual Stress Mea-surement,” Advances in X-Ray Analysis 20 , 1977, pp. 345354.E 1426 98 (2009)128. Calibration8.1 Calibrate the instrumented specimen using loads appliedby dead weights or by a testing machine that has been verifiedaccording to Practices E4. The loading configuration is suchthat the

34、applied stresses, in the region where the strain gagesare mounted and where X-ray diffraction measurements will bemade, are statically determinate (that is, may be calculatedfrom the applied loads and the dimensions of the specimen andthe fixture).8.2 Prestress the specimen by loading to a level of

35、approxi-mately 75 % of the load that is calculated to produce amaximum applied stress equal to the nominal yield strength ofthe material, then unload. This will minimize drift in the gagesand creep in the strain gage adhesive during the subsequenttesting procedure.8.3 Apply loads in increasing seque

36、nce at levels of approxi-mately 5, 15, and 25 % of the load that would produce amaximum applied stress equal to the nominal yield strength ofthe material.8.4 At each load level calculate the applied stress and takestrain gage readings.8.5 Apply loads in decreasing sequence at levels of approxi-matel

37、y 15 and 5 %, calculating the applied stress and takingstrain gage readings at each level.8.6 Repeat 8.3-8.5.8.7 Examine the data for repeatability and linearity. Devia-tions from either may indicate the failure of a strain gage bond,stressing beyond the proportional limit of the material, or animpe

38、rfect loading configuration. If the deviations exceed theacceptable degree of uncertainty in the subsequent measure-ments of residual stress, the source of the deviations should belocated and corrected before proceeding further.8.8 If the repeatability and the linearity of the data areacceptable, pl

39、ot a graph of applied stress versus strain gagereading, draw a straight line through the data, and extrapolateit down to zero applied stress and up to 75 % of the nominalyield strength of the material. This is the calibration curve. (SeeFig. 1.)NOTE 4For bending specimens, the strain indicated by th

40、e straingage(s) differs in magnitude from the strain in the specimen surfacebecause of the elevation of the strain gage grid above the surface. Thisdoes not affect the accuracy of the procedure.9. Procedure9.1 The X-ray diffraction technique, the crystallographicplanes, the c angle, and the instrume

41、ntation that are used todetermine the effective elastic parameter of the material shouldbe the same as those to be used subsequently to measureresidual stresses in objects of the same material.9.2 Mount the calibrated specimen in the loading fixture andmount the fixture in the X-ray diffraction inst

42、rument.9.2.1 When using a bending fixture the arrangement shouldbe such that the irradiated surface of the specimen is stressedin tension.9.3 Load the specimen with the loading fixture whilemonitoring the strain gage readings. Using the calibrationcurve to convert strain gage readings to applied str

43、esses, applystresses in increasing sequence at levels of approximately 5,20, 40, 60, and 70 % of the nominal yield strength of thematerial. The prestress level, 75 %, must not be exceeded.9.4 At each stress level calculate the change in interplanarspacing, Dd, between the c = 0 and c = c orientation

44、s for theparticular crystallographic planes and c angles used.9.5 Apply stresses in decreasing sequence at levels ofapproximately 60, 40, 20, and 5 %, measuring the change inthe interplanar spacing at each level.9.6 Repeat 9.3-9.5.9.7 Examine the data for repeatability and linearity, includ-ing the

45、difference in the strain data between plus and minus psiangles. Deviations from either may indicate the failure of astrain gage bond, failure of the fixture to apply the correctloading, or deviation from the proper X-ray geometry. Thelatter source of error, when present, is often caused by failureto

46、 maintain the irradiated area of the specimen surface at theexact center of the diffractometer while the specimen is underload. If the deviations exceed the acceptable degree of uncer-tainty in the subsequent measurements of residual stress, thesource of the deviations should be located and correcte

47、d beforeproceeding further.10. Calculation10.1 For each measurement described in Sections 9.3-9.6 ofthis test method, calculate the change in interplanar spacingand the corresponding applied stress.10.2 Plot the data on a graph of change in interplanarspacing vs. applied stress, and check for appare

48、nt errors. (SeeFig. 2.)FIG. 1 Calibration Curve for Instrumented Test SpecimenNOTE 1For clarity, only one point is shown for each applied stresslevelFIG. 2 Change in Interplanar Spacing Versus Applied StressE 1426 98 (2009)1310.3 Calculate the slope, m, of the best-fit straight line usingleast-squar

49、es linear regression. The following formulas4maybe used:SumX!5(i51nXiTi5 Xi2SumX!n(1)SumT2!5(i 51nTi2SumTY!5(TiYim 5SumTY!SumT2!In these equations, Xirepresents the i-th value of the appliedstress, and Yirepresents the measured value of Dd thatcorresponds to Xi.10.4 For the procedure described in 9.3-9.6 of this testmethod,n=18intheabove equations. This number corre-sponds to 2 repetitions of a sequence of 5 measurements atascending loads and 4 measurements at descending loads.NOTE 5There is no particular significance to using 18 data points.Any number equal

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