ASTM G142-1998(2011) Standard Test Method for Determination of Susceptibility of Metals to Embrittlement in Hydrogen Containing Environments at High Pressure High Temperature or Bo.pdf

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1、Designation: G142 98 (Reapproved 2011)Standard Test Method forDetermination of Susceptibility of Metals to Embrittlement inHydrogen Containing Environments at High Pressure, HighTemperature, or Both1This standard is issued under the fixed designation G142; the number immediately following the design

2、ation indicates the year oforiginal 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.1. Scope1.1 This test method covers a proced

3、ure for determinationof tensile properties of metals in high pressure or hightemperature, or both, gaseous hydrogen-containing environ-ments. It includes accommodations for the testing of eithersmooth or notched specimens.1.2 This test method applies to all materials and productforms including, but

4、not restricted to, wrought and castmaterials.1.3 The values stated in SI units are to be regarded asstandard. The values given in parentheses are for informationonly.1.4 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of t

5、he 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 ASTM Standards:2D1193 Specification for Reagent WaterE4 Practices for Force Verification of Testing MachinesE8 Test Method

6、s for Tension Testing of Metallic MaterialsE691 Practice for Conducting an Interlaboratory Study toDetermine the Precision of a Test MethodG15 Terminology Relating to Corrosion and CorrosionTesting3G111 Guide for Corrosion Tests in High Temperature orHigh Pressure Environment, or BothG129 Practice f

7、or Slow Strain Rate Testing to Evaluate theSusceptibility of Metallic Materials to EnvironmentallyAssisted Cracking2.2 Military Standard:4MIL-P-27201B Propellant, Hydrogen3. Terminology3.1 Definitions:3.1.1 control test, na mechanical test conducted in anenvironment that does not produce embrittleme

8、nt of a testmaterial.3.1.2 hydrogen embrittlement, nhydrogen induced crack-ing or severe loss of ductility caused by the presence ofhydrogen in the metal.3.1.3 Other definitions and terminology related to testingcan be found in Terminology G15.4. Summary of Test Method4.1 Specimens of selected mater

9、ials are exposed to a gas-eous hydrogen containing environment at high pressure or hightemperature, or both, while being pulled to failure in uniaxialtension. The susceptibility to hydrogen embrittlement is evalu-ated through the determination of standard mechanical prop-erties in tension (that is,

10、yield strength, ultimate tensilestrength, notched tensile strength, reduction in area or elonga-tion, or both). Comparison of these mechanical propertiesdetermined in a hydrogen-containing environment to thosedetermined in a non-embrittling environment (control test)provides a general index of susce

11、ptibility to cracking versus thematerials normal mechanical behavior.5. Significance and Use5.1 This test method provides a reliable prediction of theresistance or susceptibility, or both, to loss of material strengthand ductility as a result of exposure to hydrogen-containinggaseous environments. T

12、his test method is applicable over abroad range of pressures, temperatures, and gaseous environ-ments. The results from this test method can be used toevaluate the effects of material composition, processing, andheat treatment as well as the effects of changes in environment1This test method is unde

13、r the jurisdiction of ASTM Committee G01 onCorrosion of Metals and is the direct responsibility of Subcommittee G01.06 onEnvironmentally Assisted Cracking.Current edition approved March 1, 2011. Published April 2011. Originallyapproved in 1996. Last previous edition approved in 2004 as G14298(2004).

14、 DOI:10.1520/G0142-98R11.2For 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.3Withdrawn. The last approved versio

15、n of this historical standard is referencedon www.astm.org.4Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,Section D, 700 Robbins Ave., Philadelphia, PA 19111-50981Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United Spositi

16、on, temperature, and pressure. These results may ormay not correlate with service experience for particular appli-cations. Furthermore, this test method may not be suitable forthe evaluation of high temperature hydrogen attack in steelsunless suitable exposure time at the test conditions has takenpl

17、ace prior to the initiation of tensile testing to allow for thedevelopment of internal blistering, decarburization or cracking,or both.6. Apparatus6.1 Since this test method is intended to be conducted athigh pressures and may also involve high temperatures, theapparatus must be constructed to safel

18、y contain the testenvironment while being resistant to the embrittling effects ofhydrogen. Secondly, the test apparatus must be capable ofallowing introduction of the test gas, removal of air from thetest cell, and accurate performance of the tension test on thetest specimen. In cases where the test

19、s are conducted atelevated temperatures, the apparatus must provide for heatingof the specimen and the test environment in direct contact withthe specimen.6.2 Fig. 1 shows a schematic representation of a typical testcell designed to conduct HP/HT gaseous hydrogen embrittle-ment experiments.5The typi

20、cal components include:6.2.1 Metal Test CellThe test cell should be constructedfrom materials that have proven to have high resistance tohydrogen embrittlement under the conditions. A list of poten-tial materials of construction is shown in Fig. 2.6Materialswith high values of tensile ratios (enviro

21、nment versus a controlenvironment) should be used. Materials with low values of thisparameter should be avoided.6.2.2 Closure and SealTo facilitate operation of the testcell and tension testing, the closure should provide for rapidopening and closing of the test cell and reliable sealingcapabilities

22、 for hydrogen. This can include either metallic ornonmetallic materials with high resistance to hydrogen em-brittlement and degradation.6.2.3 Gas Port(s)The gas port should be designed topromote flow and circulation of the gaseous test environments,inert gas purging and evacuation as required to pro

23、duce theintended test environment. Usually two ports are used so thatflow-through capabilities are attained to facilitate these func-tions.6.2.4 Electrical Feed-ThroughsIf very high temperatureconditions are required it may be advantageous to utilize aninternal heater to heat the test specimen and t

24、he gaseousenvironment in the immediate vicinity of the specimen. There-fore, a feed-through would be needed to reach an internalresistance or induction heater. These feed-throughs must alsoprovide electrical isolation from the test cell and internalfixtures, and maintain a seal to prevent leakage of

25、 the testenvironment. If external heaters are used, no electric feed-throughs would be required for testing.6.2.5 Tensile Feed-Through(s)To apply tensile loading tothe test specimen it is necessary to have feed-through(s) whichprovide linear motion and transmission of loads from anexternal source. C

26、are must be taken to design such feed-throughs to have low friction to minimize errors due to frictionlosses when using externally applied loads. These are usuallydesigned to incorporate thermoplastic or elastomeric materials,or both. If elevated temperature tests are being conducted, thenextreme ca

27、re must be used in the selection of these materials toalso resist deterioration and loss of mechanical properties at thetest temperature.6.2.6 Pull RodThe pull rod works in combination with thetensile feed-through to provide for loading of the test speci-men. It is usually attached to a tensile test

28、ing machine on oneend and the tension specimen on the other. It should bedesigned to have adequate cross-sectional area to minimizecompliance in the loading system under the anticipated loads tobe used. Also, to minimize frictional forces in the seal andpromote sealing, it should be made with a high

29、ly polished5Kane, R. D., “High Temperature and High Pressure,” Corrosion Tests andStandards, Baboian, Robert, editor, ASTM, West Conshohocken, PA.6Metals Handbook, Vol 9, Corrosion, 9th Edition, ASM International, MetalsPark, OH, 1987, p. 1104.FIG. 1 Hydrogen Tensions Test Autoclave for Various Allo

30、ys inHydrogen versus AirG142 98 (2011)2surfaces 0.25 m (10 in.) RMS. It is possible to obtain pullrod systems that are pressure balanced so specimen loadingfrom the internal pressure in the test cell can be minimized.6.2.7 Load CellLoad cells for conducting high pressuretensile tests may be two conf

31、igurations:6.2.7.1 External load cells which are attached to the pull rodoutside of the test cell, and6.2.7.2 Internal load cells which are either attached to thepull rod or grip assembly inside of the autoclave or areintegrated into the pull rod. When using external load cells it isimportant to cor

32、rect load cell readings for frictional forces inthe pressure seal. Additionally, if non-pressure balanced pullrods are used, compensation for pressure loading of thespecimen must be also performed.6.2.8 Electric Resistance or Induction Heater(s)Eitherinternal or external heaters can be used to obtai

33、n elevatedtemperature. For lower temperatures, and when using testenvironments containing reactive constituents in addition tohydrogen, external heating of the test cell is typically moreconvenient. At high temperatures, when using non-reactive orhydrogen gas environments, an internal heater can be

34、used toheat only the test specimen and the gaseous environment in thevicinity of the test specimen to limit power requirements andproblems with high temperature sealing and pressure contain-ment.6.2.9 GripsGrips shall provide for efficient and accuratetransfer of load from the pull rods to the test

35、specimen. Gripsshould be designed to minimize compliance in the loadingsystem under the anticipated loads to pull the test specimen.6.2.10 Loading FixtureA fixture is used to react the loadused to pull the specimen. An internal fixture is shownschematically in Fig. 1.6.2.11 Testing MachinesTension t

36、esting machines usedfor conducting tests according to this test method shall conformto the requirements of Practices E4. The loads used in testsshall be within the calibrated load ranges of the testingmachines in accordance with Practices E4.7. Reagents7.1 Purity of ReagentsReagent grade chemicals a

37、nd ultralow oxygen gases (1 ppm) shall be used in all tests unless thetest environment is derived from a field or plant environment.If the test is to be conducted for aerospace propulsion appli-cations, the environment shall consist of hydrogen gas perMIL-P-27201B.7.2 If water is to be added to any

38、test environment, distilledor deionized water conforming to Specification D1193 Type IVshall be used.8. Test Environment8.1 Test environments can consist of either field or plantsamples or be prepared in the laboratory from chemicals andgases as indicated in Section 7.8.2 When testing in hydrogen co

39、ntaining environments,susceptibility to hydrogen embrittlement typically increaseswith decreasing oxygen content of the test environment.Therefore, strict procedures for deaeration shall be followedand periodically qualified for oxygen content as discussed inSections 9 and 11.8.3 For purposes of sta

40、ndardization, suggested standardizedpressures for hydrogen gas testing shall be 7 MPa, 35 MPa, and69 MPa. However, for materials evaluation for specific appli-cations, the test pressure should be equal to or greater than thatwhich represents the service conditions.FIG. 2 Notched Tensile Strength (NT

41、S) Ratio for Various Alloys in 35 to 69 MPa Gaseous Hydrogen versus Air Tested at RoomTemperatureG142 98 (2011)39. Sampling9.1 The procedure for sampling mill products is typicallycovered in product or other specifications and is outside thescope of this document.9.2 Sampling of the test environment

42、 is recommended toconfirm that the test environment is in conformance with thistest method and attains the intended test conditions. Suchsampling shall be conducted immediately prior to and aftertesting. The frequency of environmental sampling shall be asrequired to cover applicable product, purchas

43、e or in-housetesting specifications, or both.As a minimum requirement to bein compliance with this test method, however, sampling of thetest environment shall be conducted at the start of testing andagain when any element of the test procedure or test system hasbeen changed or modified.10. Test Spec

44、imens10.1 Tension specimens shall be used for evaluation ofhydrogen embrittlement. These specimens shall conform to thedimensions and guidelines provided in Test Methods E8.However, in some cases, the material size, configuration, andform or the confines of various test cells may limit the actualdim

45、ensions of the test specimen. In such cases, the specimengeometry and dimensions shall be fully described. Take care toonly compare the results obtained from similar specimens.10.2 For purposes of standardizing the evaluation of mate-rials according to this test method, two standard test specimenssh

46、all be used: standard smooth tension specimen, and standardnotched tensile specimen. The dimensions of these specimensare given in Fig. 3a and Fig. 3b.10.3 Specimens shall be machined to have a minimalamount of cold work on the gage or notch surfaces. Total metalremoved in the last two passes shall

47、be limited to a total of 0.05mm and have a surface finish of 0.25 m (10 in.) or better. Themethod of final machining of the gage section should be bygrinding (not turning) to avoid localized grooves and coldworked areas.11. Standardization11.1 To provide an indication when some inadvertent de-viatio

48、n from the correct test conditions occurs, it is necessaryto test a control specimen of a material of known susceptibilityto hydrogen embrittlement using the procedures given herein.This control material should exhibit an easily reproducibledegree of embrittlement.11.2 The control materials for test

49、s conducted in a hydrogencontaining environment shall be as given below:11.2.1 Low ResistanceLow Alloy Steel: UNS G43400(austenitize at 900C for 1 h plus water quench and temper at454C for 2 h).11.2.2 Intermediate ResistanceNickel Base Alloy: UNSN07718 (solution annealed at 954C for 1 h plus air cool; ageat 718C for 8 h plus furnace cool to 620C hold for 8 h plusair cool).11.2.3 High ResistanceStainless Steels: A 286AMS5737 (solution annealed at 893C for 1 h plus water quench andaged at 721C for 16 h plus air cool).12. Test Procedure12.1 Fol

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