ASTM D3762-2003(2010) Standard Test Method for Adhesive-Bonded Surface Durability of Aluminum (Wedge Test)《用胶粘剂粘结的铝表面耐久性的标准试验方法(楔入试验)》.pdf

《ASTM D3762-2003(2010) Standard Test Method for Adhesive-Bonded Surface Durability of Aluminum (Wedge Test)《用胶粘剂粘结的铝表面耐久性的标准试验方法(楔入试验)》.pdf》由会员分享，可在线阅读，更多相关《ASTM D3762-2003(2010) Standard Test Method for Adhesive-Bonded Surface Durability of Aluminum (Wedge Test)《用胶粘剂粘结的铝表面耐久性的标准试验方法(楔入试验)》.pdf（5页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: D3762 03 (Reapproved 2010)Standard Test Method forAdhesive-Bonded Surface Durability of Aluminum (WedgeTest)1This standard is issued under the fixed designation D3762; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, th

2、e 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 method2,3simulates in a qualitative manner theforces and effects on an adhesive bond joint at meta

3、l-adhesive/primer interface. It has proven to be highly reliable in deter-mining and predicting the environmental durability of adher-end surface preparations. The method has proven to becorrelatable with service performance in a manner that is muchmore reliable than conventional lap shear or peel t

4、ests (Note 2).NOTE 1While this test method is intended for use in aluminum-to-aluminum applications it may be used for determining surface durabilityof other metals and plastics provided consideration is given to thicknessand rigidity of the adherends.NOTE 2This test method is not a quantitative fra

5、cture strength testmethod. To measure fracture strength see Test Method D3433.1.2 The values stated in SI units are to be regarded as thestandard. The values given in parentheses are for informationonly.1.3 This standard does not purport to address all of thesafety concerns, if any, associated with

6、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 ASTM Standards:4D907 Terminology of AdhesivesD3433 Test Method for Fracture Strength

7、in Cleavage ofAdhesives in Bonded Metal Joints3. Terminology3.1 DefinitionsMany of the terms used in this test methodare defined in Terminology D907.4. Summary of Test Method4.1 A wedge is forced into the bondline of a flat-bondedaluminum specimen, thereby creating a tensile stress in theregion of t

8、he resulting crack tip. The stressed specimen isexposed to an aqueous environment, usually at an elevatedtemperature, or to an appropriate environment relative to theuse of the bonded structure. The resulting crack growth withtime and failure modes are then evaluated. Variations inadherend surface q

9、uality are easily observable when thespecimens are forcibly, if necessary, opened at the test conclu-sion.5. Significance and Use5.1 The test is primarily qualitative, but is very discriminat-ing in determining variations in adherend surface preparationparameters and adhesive environmental durabilit

10、y. The test hasfound application in controlling surface preparation operationsand in screening surface preparations, primer and adhesivesystems for durability. In addition to determining crack growthrate and assigning a value to it, the adhesivejoint failure isevaluated and reported. For example, ad

11、hesion failure; cohe-sion failure; or adherend failure are noted after opening up thespecimen at the conclusion of the test period.6. Apparatus6.1 Magnifier (preferably stereo binocular), 5 to 30-power.6.2 Marking Stylus, sharp-pointed, or triangular file.6.3 Wedges, aluminum or stainless steel.NOTE

12、 3Wedges are preferably of the same composition as theadherends of the specimen being tested to reduce the possibility ofelectrolytic corrosion. Stainless steel wedges have been found to workwell with many adherends and are very durable and reuseable.6.4 Scale, small, graduated in millimetres or hun

13、dredths ofan inch.1This test method is under the jurisdiction of ASTM Committee D14 onAdhesives and is the direct responsibility of Subcommittee D14.80 on MetalBonding Adhesives.Current edition approved Oct. 1, 2010. Published October 2010. Originallyapproved in 1979. Last previous edition approved

14、in 2003 as D3762 03. DOI:10.1520/D3762-03R10.2Marceau, J. A., Moji, Y., and McMillan, J. C., “A Wedge Test for EvaluatingAdhesive Bonded Surface Durability,” 21st SAMPE Symposium, Vol 21, April 68,1976.3Scardino, W. M., Marceau J. A., “Comparative Stressed Durability of AdhesiveBonded Aluminum Alloy

15、 Joints,” Symposium on Durability of Adhesive BondedStructures, U. S.ArmyArmament Research and Development Command, Dover, N.J. Oct, 2729, 1976.4For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards v

16、olume information, 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.7. Test Specimen7.1 Use a minimum of five 25.4 by 203-mm (1 by 8-in.)specimens from a single assembly

17、for each test (Fig. 1).7.2 It is desirable to prevent plastic deformation (yielding)of the test specimen adherends when inserting the wedge intothe bondline. However, some plastic deformation is permis-sible providing it is not excessive. (Fig. 2 illustrates data inwhich some plastic deformation of

18、high-strength aluminumalloys occurred when the wedges was forced into the bond-line.)7.3 The adherend yield point and the toughness of theadhesive are the two most important factors in determining asatisfactory adherend thickness. The configuration of Fig. 1 hasbeen satisfactory for high-strength al

19、uminum alloys, for ex-ample, 2024T-3 and 7075-T6, when used with most tough,high-strength aerospace adhesives.7.4 A satisfactory adherend thickness for a specificadhesive-adherend system can be determined by trial and errormethods and can also be approximated.NOTE 4The minimum permissible thickness

20、in a uniform symmetri-cal adherend may be computed from the following relationship:h 56TaBFty(1)where:h = thickness of metal normal to plane of bonding, mm (or in.),Fty= tensile yield point of metal (or the stress at proportional limit)MPa (or psi),T = 150 % of the maximum load to start the crack in

21、 the adhesivebond, N (or lbf),a = crack length at maximum load, mm (or in.), andB = bond width, mm (or in.).8. Conditioning8.1 Expose the specimens to any environment appropriateto the bonded structure being represented, for example: humid-ity, heat, thermal shock, salt spray, etc. However, for most

22、applications water is the most deleterious environment to thepolymer-adherend interface. A typical accelerated aging envi-ronment commonly used is 50C (122F) and condensinghumidity. This and other standard test environments are listedin Table 1 (Note 5). The time of exposure may be varied. If thejoi

23、nt is affected by the chosen environment, significant crackgrowth normally occurs.NOTE 5For maximum acceleration of aging effect, the aerospaceindustry typically uses environment 8 for adhesive systems that cure at121C (250F) with performance to about 80C (178F) and environment9 for adhesive systems

24、 that cure at 177C (350F) with performance toabout 150C (302F).9. Procedure9.1 Prepare the surfaces of a piece of 152 by 203 by 3.2-mm(6 by 8 by 0.125-in.) aluminum using a surface treatmentprocess appropriate for the test requirements.9.2 Prime the faying surface of each panel, apply theadhesive, a

25、ssemble the panels, and cure the adhesive asrequired by the appropriate specification. Insert a 50.8 by 152by 0.10 mm (2 by 6 by 0.004-mm.) separation film along oneof the 152-mm wide edges of the assembly as shown in Fig. 1to omit the adhesive from between the separation film and thealuminum surfac

26、e.9.3 Cut the test assembly into five 1-in. wide test specimensas shown in Fig. 1. The surface finish of both cut edges is 3.175m (125 in.) or finer. No burrs or smearing of adherendmaterial onto the bondline is allowed. Do not overheat ordamage the bond when cutting or finishing.9.4 Mark all test s

27、pecimens to identify them appropriatelywith respect to their processing in a manner such that testing ina high-humidity environment does not destroy the identifica-tion markings. Appropriately positioned identification mark-ings can be made on the 152 by 152-mm (6 by 6-in.) panelsprior to surface pr

28、eparation processing.9.5 Open the end of the test specimen that contains theseparation film, and insert the wedge. Position the wedge so theend and sides are approximately flush with the sides of thespecimen. (In any use of an auxiliary tool to open thespecimen, remove the separation film or insert

29、the wedge, donot bend the specimen.)9.6 Using 5 to 30-power magnification and adequate illu-mination, locate the tip of the crack, ao, on the 3.175-m(125- in.) finish edge of each specimen. This is the point, ao,farthest from the wedge where the specimen (the adhesive,primer, or adherends, on both)

30、has separated. Mark the locationon both sides of the adherend edge, using a fine stylus or scribe.If the specimen is to be used in salt spray or other environmentexpected to be corrosive and likely to obliterate the mark, thendeepen the scribe mark with a triangular file.9.7 For additional accuracy,

31、 take and average readings onboth sides of the specimen. Expose the wedged specimens tothe environment as required by the appropriate specification,the environments suggested in 8.1, or the environment dictatedby actual expected service conditions.9.8 Remove the specimens from the environment and wi

32、thin15 min mark the location of the tip of the crack, Da, in the samemanner as in 9.6.9.9 Measure the initial crack length aoand the crackextension, Da, of each specimen to the nearest 0.254 mm (0.01in.).9.10 At the conclusion of the test, forcibly open the speci-men and note the failure mode of the

33、 test section.10. Interpretation of Results10.1 Report the crack extension, Da, and the adhesivejointfailure.10.2 The initial crack length, ao, the crack extension, Da,and the adhesivejoint failure are all functions of the adherend,surface treatment, and the adhesive/primer systems beingconsidered.

34、Because of these variables, the acceptance criteriafor a bonded system of interest has to be established. Below isan example of an acceptance criterion for sodium dichromate-sulfuric acid-etched, aluminum adherends bonded with 121C(250F) curing high-peel modified epoxy structural adhesives:Ten speci

35、mens, representing two individual bonded testassemblies, are tested. Typically good durability surface prepa-ration is evidenced by no individual specimen having a crackextension, Da, exceeding 19 mm (0.75 in.) with the average ofD3762 03 (2010)2FIG. 1 Crack Extension Specimen ConfigurationD3762 03

36、(2010)3all specimens not over 6.3 mm (0.25 in.), when placed in 50C(122F) condensing humidity for 1 h.11. Report11.1 Report the following:11.1.1 Complete identification of the adhesive and specimentested, including types, source, manufacturers code numbers,form, etc.11.1.2 Method of preparing test s

37、pecimens, including mix-ing and dispensing of adhesive.11.1.3 Conditioning procedure.11.1.4 Testing conditions.11.1.5 Number of specimens tested.11.1.6 Report the original crack length, ao, and the crackextension, Da, at the end of various time intervals such as 1, 4,8, 24 h; 7, 30 days.11.1.7 Also

38、report the adhesivejoint failure such as 100 %cohesive, 100 % primer to adherend, or 50 % adhesive toprimer, etc.12. Precision and Bias12.1 Precision and bias must be established for each systemsince initial crack length, ao, the crack extension,D a, and theadhesivejoint failure are all functions of

39、 the adherends,surface treatment, the adhesive/primer, and the environmentused.12.2 Fig. 2 is a plot of data on one such system (see 10.2)atfive separate locations over a period of 1 year.13. Keywords13.1 adhesive; crack extension; durability; surface prepara-tion; wedgeNOTE 1Distribution of crack e

40、xtension Da at five locations for one adherend, surface preparation, adhesive, primer system. (Adhesive is a 121C(250F) curing high-peel modified expoxy structural adhesive).FIG. 2 Distribution of Crack ExtensionTABLE 1 Standard Test EnvironmentsTestEnvironmentNumberTemperature,C (F)AMoisture Condit

41、ions % RelativeHumidityB1 23 (73.4) immersed in distilled or deionized water2 23 (73.4) 503 23 (73.4) 154 35 (95) 905 35 (95) 1006 50 (122) 907 50 (122) 1008 60 (140) 1009 71 (160) 10010 35 (95) 5 % salt fog11 ambient (outdoors) ambient (outdoors)12 other (specify) other, including aqueous solutions

42、 ornonaqueous liquids (specify)AThe tolerance for test temperature shall be 6 1C or 1.8F for environments 1to 10.BThe moisture condition may be provided by controlling the relative humidity ofa box, room, or other chamber by any convenient means.D3762 03 (2010)4ASTM International takes no position r

43、especting the validity of any patent rights asserted in connection with any item mentionedin this standard. Users of this standard are expressly advised that determination of the validity of any such patent rights, and the riskof infringement of such rights, are entirely their own responsibility.Thi

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45、rnational Headquarters. Your comments will receive careful consideration at a meeting of theresponsible technical committee, which you may attend. If you feel that your comments have not received a fair hearing you shouldmake your views known to the ASTM Committee on Standards, at the address shown

46、below.This standard is copyrighted by ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959,United States. Individual reprints (single or multiple copies) of this standard may be obtained by contacting ASTM at the aboveaddress or at 610-832-9585 (phone), 610-832-9555 (fax), or serviceastm.org (e-mail); or through the ASTM website(www.astm.org). Permission rights to photocopy the standard may also be secured from the ASTM website (www.astm.org/COPYRIGHT/).D3762 03 (2010)5