ASTM E466-2007 809 Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials《金属材料受力控制的恒定振幅轴向疲劳试验的操作用标准实施规程》.pdf

《ASTM E466-2007 809 Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials《金属材料受力控制的恒定振幅轴向疲劳试验的操作用标准实施规程》.pdf》由会员分享，可在线阅读，更多相关《ASTM E466-2007 809 Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials《金属材料受力控制的恒定振幅轴向疲劳试验的操作用标准实施规程》.pdf（5页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: E 466 07Standard Practice forConducting Force Controlled Constant Amplitude AxialFatigue Tests of Metallic Materials1This standard is issued under the fixed designation E 466; 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 (e) indicates an editorial change since the last revision or reapproval.1. Scope1.1 This practice covers the procedure for the performanceof axial force controlled fatigue tests to ob

3、tain the fatiguestrength of metallic materials in the fatigue regime where thestrains are predominately elastic, both upon initial loading andthroughout the test. This practice is limited to the fatiguetesting of axial unnotched and notched specimens subjected toa constant amplitude, periodic forcin

4、g function in air at roomtemperature. This practice is not intended for application inaxial fatigue tests of components or parts.NOTE 1The following documents, although not directly referenced inthe text, are considered important enough to be listed in this practice:E 739 Practice for Statistical An

5、alysis of Linear or Linearized Stress-Life (S-N) and Strain-Life (e-N) Fatigue DataSTP 566 Handbook of Fatigue Testing2STP 588 Manual on Statistical Planning and Analysis for FatigueExperiments3STP 731 Tables for Estimating Median Fatigue Limits42. Referenced Documents2.1 ASTM Standards:5E3 Guide fo

6、r Preparation of Metallographic SpecimensE 467 Practice for Verification of Constant Amplitude Dy-namic Forces in an Axial Fatigue Testing SystemE 468 Practice for Presentation of Constant Amplitude Fa-tigue Test Results for Metallic MaterialsE 606 Practice for Strain-Controlled Fatigue TestingE 739

7、 Practice for Statistical Analysis of Linear or Linear-ized Stress-Life ( S-N) and Strain-Life (e-N) Fatigue DataE 1012 Practice for Verification of Test Frame and Speci-men Alignment Under Tensile and Compressive AxialForce ApplicationE 1823 Terminology Relating to Fatigue and Fracture Test-ing3. T

8、erminology3.1 Definitions:3.1.1 The terms used in this practice shall be as defined inTerminology E 1823.4. Significance and Use4.1 The axial force fatigue test is used to determine theeffect of variations in material, geometry, surface condition,stress, and so forth, on the fatigue resistance of me

9、tallicmaterials subjected to direct stress for relatively large numbersof cycles. The results may also be used as a guide for theselection of metallic materials for service under conditions ofrepeated direct stress.4.2 In order to verify that such basic fatigue data generatedusing this practice is c

10、omparable, reproducible, and correlatedamong laboratories, it may be advantageous to conduct around-robin-type test program from a statisticians point ofview. To do so would require the control or balance of what areoften deemed nuisance variables; for example, hardness, clean-liness, grain size, co

11、mposition, directionality, surface residualstress, surface finish, and so forth. Thus, when embarking on aprogram of this nature it is essential to define and maintain1This practice is under the jurisdiction ofASTM Committee E08 on Fatigue andFracture and is the direct responsibility of Subcommittee

12、 E08.05 on CyclicDeformation and Fatigue Crack Formation.Current edition approved Nov. 1, 2007. Published November 2007. Originallyapproved in 1972. Last previous edition approved in 2002 as E 466 96(2002)e1.2Handbook of Fatigue Testing, ASTM STP 566, ASTM, 1974.3Little, R. E., Manual on Statistical

13、 Planning and Analysis, ASTM STP 588,ASTM, 1975.4Little, R. E., Tables for Estimating Median Fatigue Limits, ASTM STP 731,ASTM, 1981.5For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume infor

14、mation, refer to the standards Document Summary page onthe ASTM website.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.Copyright by ASTM Intl (all rights reserved); Thu Jun 5 01:55:41 EDT 2008Downloaded/printed byGuo Dehua (CNIS) pu

15、rsuant to License Agreement. No further reproductions authorized.consistency a priori, as many variables as reasonably possible,with as much economy as prudent. All material variables,testing information, and procedures used should be reported sothat correlation and reproducibility of results may be

16、 attemptedin a fashion that is considered reasonably good current testpractice.4.3 The results of the axial force fatigue test are suitable forapplication to design only when the specimen test conditionsrealistically simulate service conditions or some methodologyof accounting for service conditions

17、 is available and clearlydefined.5. Specimen Design5.1 The type of specimen used will depend on the objectiveof the test program, the type of equipment, the equipmentcapacity, and the form in which the material is available.However, the design should meet certain general criteriaoutlined below:5.1.1

18、 The design of the specimen should be such that failureoccurs in the test section (reduced area as shown in Fig. 1 andFig. 2). The acceptable ratio of the areas (test section to gripsection) to ensure a test section failure is dependent on thespecimen gripping method. Threaded end specimens mayprove

19、 difficult to align and failure often initiates at these stressconcentrations when testing in the life regime of interest in thispractice. A caveat is given regarding the gage section withsharp edges (that is, square or rectangular cross section) sincethese are inherent weaknesses because the slip o

20、f the grains atsharp edges is not confined by neighboring grains on two sides.Because of this, a circular cross section may be preferred ifmaterial form lends itself to this configuration. The size of thegripped end relative to the gage section, and the blend radiusfrom gage section into the grip se

21、ction, may cause prematurefailure particularly if fretting occurs in the grip section or if theradius is too small. Readers are referred to Ref (1) should thisoccur.5.1.2 For the purpose of calculating the force to be appliedto obtain the required stress, the dimensions from which thearea is calcula

22、ted should be measured to the nearest 0.001 in.(0.03 mm) for dimensions equal to or greater than 0.200 in.(5.08 mm) and to the nearest 0.0005 in. (0.013 mm) fordimensions less than 0.200 in. (5.08 mm). Surfaces intended tobe parallel and straight should be in a manner consistent with8.2.NOTE 2Measur

23、ements of dimensions presume smooth surface fin-ishes for the specimens. In the case of surfaces that are not smooth, dueto the fact that some surface treatment or condition is being studied, thedimensions should be measured as above and the average, maximum, andminimum values reported.5.2 Specimen

24、Dimensions:5.2.1 Circular Cross SectionsSpecimens with circularcross sections may be either of two types:5.2.1.1 Specimens with tangentially blended fillets betweenthe test section and the ends (Fig. 1)The diameter of the testsection should preferably be between 0.200 in. (5.08 mm) and1.000 in. (25.

25、4 mm). To ensure test section failure, the gripcross-sectional area should be at least 1.5 times but, preferablyfor most materials and specimens, at least four times the testsection area. The blending fillet radius should be at least eighttimes the test section diameter to minimize the theoreticalst

26、ress concentration factor, Ktof the specimen. The test sectionlength should be approximately two to three times the testsection diameter. For tests run in compression, the length of thetest section should be approximately two times the test sectiondiameter to minimize buckling.5.2.1.2 Specimens with

27、 a continuous radius between ends(Fig. 3) The radius of curvature should be no less than eighttimes the minimum diameter of the test section to minimize Kt. The reduced section length should be greater than three timesthe minimum test section diameter. Otherwise, the samedimensional relationships sh

28、ould apply, as in the case of thespecimens described in 5.2.1.1.5.2.2 Rectangular Cross SectionsSpecimens with rectan-gular cross sections may be made from sheet or plate materialand may have a reduced test cross section along one dimen-sion, generally the width, or they may be made from materialreq

29、uiring dimensional reductions in both width and thickness.In view of this, no maximum ratio of area (grip to test section)should apply. The value of 1.5 given in 5.2.1.1 may beconsidered as a guideline. Otherwise, the sections may beeither of two types:5.2.2.1 Specimens with tangentially blended fil

30、lets betweenthe uniform test section and the ends (Fig. 4) The radius ofthe blending fillets should be at least eight times the specimentest section width to minimize Ktof the specimen. The ratio ofspecimen test section width to thickness should be between twoand six, and the reduced area should pre

31、ferably be between0.030 in.2(19.4 mm2) and 1.000 in.2(645 mm2), except inextreme cases where the necessity of sampling a product withan unchanged surface makes the above restrictions impractical.The test section length should be approximately two to threetimes the test section width of the specimen.

32、 For specimensthat are less than 0.100 in. (2.54 mm) thick, special precautionsare necessary particularly in reversed loading, such as R = 1.For example, specimen alignment is of utmost importance andFIG. 1 Specimens with Tangentially Blending Fillets Between the Test Section and the EndsE466072Copy

33、right by ASTM Intl (all rights reserved); Thu Jun 5 01:55:41 EDT 2008Downloaded/printed byGuo Dehua (CNIS) pursuant to License Agreement. No further reproductions authorized.the procedure outlined in Practice E 606 would be advanta-geous. Also, Refs (2-5), although they pertain to strain-controlled

34、testing, may prove of interest since they deal withsheet specimens approximately 0.05 in. (1.25 mm) thick.5.2.2.2 Specimens with continuous radius between ends(Fig. 2)The same restrictions should apply in the case of thistype of specimen as for the specimen described in 5.2.1.2. Thearea restrictions

35、 should be the same as for the specimendescribed in 5.2.2.1.5.2.3 Notched SpecimensIn view of the specialized natureof the test programs involving notched specimens, no restric-tions are placed on the design of the notched specimen, otherthan that it must be consistent with the objectives of theprog

36、ram. Also, specific notched geometry, notch tip radius,information on the associated Ktfor the notch, and the methodand source of its determination should be reported.6. Specimen Preparation6.1 The condition of the test specimen and the method ofspecimen preparation are of the utmost importance. Imp

37、ropermethods of preparation can greatly bias the test results. In viewof this fact, the method of preparation should be agreed uponprior to the beginning of the test program by both the originatorand the user of the fatigue data to be generated. Since specimenpreparation can strongly influence the r

38、esulting fatigue data,the application or end use of that data, or both, should beconsidered when selecting the method of preparation. Appen-dix X1 presents an example of a machining procedure that hasbeen employed on some metals in an attempt to minimize thevariability of machining and heat treatmen

39、t upon fatigue life.6.2 Once a technique has been established and approved fora specific material and test specimen configuration, changeshould not be made because of potential bias that may beintroduced by the changed technique. Regardless of the ma-chining, grinding, or polishing method used, the

40、final metalremoval should be in a direction approximately parallel to thelong axis of the specimen. This entire procedure should beclearly explained in the reporting since it is known to influencefatigue behavior in the long life regime.6.3 The effects to be most avoided are fillet undercuttingand r

41、esidual stresses introduced by specimen machining prac-tices. One exception may be where these parameters are understudy. Fillet undercutting can be readily determined by inspec-tion.Assurance that surface residual stresses are minimized canbe achieved by careful control of the machining procedures.

42、 Itis advisable to determine these surface residual stresses withX-ray diffraction peak shift or similar techniques, and that thevalue of the surface residual stress be reported along with thedirection of determination (that is, longitudinal, transverse,radial, and so forth).FIG. 2 Specimens with Co

43、ntinuous Radius Between EndsFIG. 3 Specimens with a Continuous Radius Between EndsFIG. 4 Specimens with Tangentially Blending Fillets Between the Uniform Test Section and the EndsE466073Copyright by ASTM Intl (all rights reserved); Thu Jun 5 01:55:41 EDT 2008Downloaded/printed byGuo Dehua (CNIS) pur

44、suant to License Agreement. No further reproductions authorized.6.4 StorageSpecimens that are subject to corrosion inroom temperature air should be accordingly protected, prefer-ably in an inert medium. The storage medium should generallybe removed before testing using appropriate solvents, if nec-e

45、ssary, without adverse effects upon the life of the specimens.6.5 InspectionVisual inspections with unaided eyes orwith low power magnification up to 203 should be conductedon all specimens. Obvious abnormalities, such as cracks,machining marks, gouges, undercuts, and so forth, are notacceptable. Sp

46、ecimens should be cleaned prior to testing withsolvent(s) non-injurious and non-detrimental to the mechanicalproperties of the material in order to remove any surface oilfilms, fingerprints, and so forth. Dimensional analysis andinspection should be conducted in a manner that will notvisibly mark, s

47、cratch, gouge, score, or alter the surface of thespecimen.7. Equipment Characteristics7.1 Generally, the tests will be performed on one of thefollowing types of fatigue testing machines:7.1.1 Mechanical (eccentric crank, power screws, rotatingmasses),7.1.2 Electromechanical or magnetically driven, o

48、r7.1.3 Hydraulic or electrohydraulic.7.2 The action of the machine should be analyzed to ensurethat the desired form and magnitude of loading is maintainedfor the duration of the test.7.3 The test machines should have a force-monitoringsystem, such as a transducer mounted in series with thespecimen,

49、 or mounted on the specimen itself, unless the use ofsuch a system is impractical due to space or other limitations.The test forces should be monitored continuously in the earlystage of the test and periodically, thereafter, to ensure that thedesired force cycle is maintained. The varying stress ampli-tude, as determined by a suitable dynamic verification (seePractice E 467), should be maintained at all times within 2 %of the desired test value.7.4 Test FrequencyThe range of frequencies for whichfatigue results may be influenced by rate effects varies frommaterial to