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    ASTM C1135-2000(2005) Standard Test Method for Determining Tensile Adhesion Properties of Structural Sealants《测定结构密封件的粘着抗拉强度特性的标准试验方法》.pdf

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    ASTM C1135-2000(2005) Standard Test Method for Determining Tensile Adhesion Properties of Structural Sealants《测定结构密封件的粘着抗拉强度特性的标准试验方法》.pdf

    1、Designation: C 1135 00 (Reapproved 2005)Standard Test Method forDetermining Tensile Adhesion Properties of StructuralSealants1This standard is issued under the fixed designation C 1135; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revisio

    2、n, 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 test method covers a laboratory procedure forquantitatively measuring the tensile adhesion proper

    3、ties ofstructural sealants, hereinafter referred to as the “sealant”.1.2 The values stated in SI (metric) units are to be regardedas the standard. The inch-pound values given in parentheses areprovided for information only.1.3 This standard does not purport to address all of thesafety concerns, if a

    4、ny, 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.NOTE 1Two ISO standards are known that develop similar informa-tion to C 1135; ISO 8339 and

    5、ISO 8340.2. Referenced Documents2.1 ASTM Standards:2C 717 Terminology of Building Seals and Sealants2.2 ISO Standards:3ISO 8339 Determination of Tensile PropertiesISO 8340 Determination of Tensile Properties at MaintainedExtension3. Terminology3.1 DefinitionsRefer to Terminology C 717 for definition

    6、sof the following terms used in this test method: cohesivefailure, primer, sealant, spacer, structural sealant, and substrate.4. Significance and Use4.1 Frequently, glass or other glazing or panel materials arestructurally adhered with a sealant to a metal framing system.The sealants used for these

    7、applications are designed to providea structural link between the glazing or panel and the framingsystem.4.2 Although this test method is conducted at one prescribedenvironmental condition, other environmental conditions andduration cycles can be employed.5. Apparatus and Materials5.1 Tensile Testin

    8、g Machine, capable of producing a tensileload on the specimen at the rate of 50.8 6 5.1 mm (2.0 6 0.20in.) per minute.5.1.1 Fixed MemberA fixed or essentially stationarymember carrying one grip.5.1.2 Movable MemberA movable member carrying asecond grip.5.1.3 GripsThe grips should be suitable to firm

    9、ly graspthe test fixture that holds the test specimen and should bedesigned to eliminate eccentric specimen loading. Specimenloading should be perpendicular to the substrate/sealant inter-faces. For alignment purposes, each grip shall have a swivel oruniversal joint at the end nearest to the specime

    10、n.5.1.4 Grip FixtureA fixture capable of being held by thegrips and furnishing a tensile force to the sealant specimen.5.2 Spatulas, for use in applying sealant.5.3 Caulking Gun, for extruding sealant from cartridgeswhen applicable.5.4 Substrate PanelsTwo substrates of the same finish arerequired fo

    11、r each test specimen.NOTE 2This test method is based on identical substrates of6.3 3 25.4 3 76.2 mm (0.25 3 1.0 3 3.0 in.) clear float glass. Othersubstrates may be tested; however, consideration needs to be given tomaintaining adequate rigidity of the substrates during testing.5.5 SpacerOne piece s

    12、pacer made from polytetrafluoreth-ylene (PTFE) or a suitable rigid material shall be used to whichthe test sealant will not bond.5.6 Substrate Cleaning Materials.5.7 Primer (if needed).6. Test Specimen6.1 Assembly:1This test method is under the jurisdiction ofASTM Committee C24 on BuildingSeals and

    13、Sealants and is the direct responsibility of Subcommittee C24.30 onAdhesion.Current edition approved Sept. 1, 2005. Published October 2005. Originallyapproved in 1990. Last previous edition approved in 2000 as C 1135 00.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact

    14、ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.3Available from American National Standards Institute (ANSI), 25 W. 43rd St.,4th Floor, New York, NY 10036.1Copyright ASTM International, 100

    15、 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.6.1.1 Prior to assembly, wipe the substrates with a clean,dry, lint-free cloth, then thoroughly clean with a solutionappropriate for the substrate material. Prior to evaporation ofthe cleaning solution, wipe the substra

    16、tes dry with a clean,lint-free cloth.NOTE 3The precision and bias statement is based on glass substrateswith a recommended cleaning solution of a 50 to 50 ratio isopropanol andwater.6.1.2 Apply recommended primer, if required. Then, con-struct the test specimen assemblies by forming a sealant cavity

    17、12.7 by 12.7 by 50.8 mm (0.50 by 0.50 by 2.0 in.) between twosubstrate panels (see Fig. 1) with the aid of appropriate spacers.6.2 Preparation of Test Assemblies:6.2.1 Prepare a set of five test specimen assemblies for eachsealant and substrate combination being tested (see Fig. 1).NOTE 4Five test s

    18、pecimen assemblies should be prepared for eachadditional environmental condition being evaluated.6.2.2 Fill each set of five assemblies with the sealant beingtested. Immediately tool the sealant surface to ensure completefilling and wetting of the substrate surfaces. Take special careto strike off t

    19、he sealant flush with the substrate.6.3 LabelingEach of the five specimens of each set shouldbe individually identified.7. Conditioning7.1 Cure the specimens for 21 days at 23C (3.6F) and 506 6 % relative humidity (standard conditions). Any deviationsfrom the curing conditions must be listed in the

    20、report.7.2 Remove all spacer sections from the specimens. Ifdesired, spacers may be removed prior to the end of the 21 daycure. If removed early, note this in the report.8. Procedure8.1 Testing:8.1.1 Pull all specimens on the tensile test machine atstandard conditions at a rate of 50.8 mm (2.0 in.)

    21、per minute.If an analog chart recording device is being used, the chartspeed should be a minimum of 127 mm (5.0 in.) per minute(508 mm (20.0 in.) per minute is preferred) to allow for a moreaccurate reading of force at specific elongations.8.1.2 Measure and record to the nearest 0.8 mm (0.03125in.)

    22、the actual minimum length (Dimension A) and minimumwidth (Dimension B), in millimetres (inches) as shown in Fig.1.8.1.3 Record the tensile load, C, (see Note 5), newtons (lbs)at 10, 25, 50, and 100 %, and at maximum elongation (see Note6). Measure and record percent cohesive failure.NOTE 5If the sub

    23、strate breaks, disregard the value at which it breaks.Other values obtained prior to breakage are acceptable.NOTE 6Calculate the maximum elongation from the recording chartvalue at the point of maximum load.8.2 ObservationsObserve the specimens and record anyobvious air bubbles trapped in the sealan

    24、t during the prepara-tion of test specimens.9. Calculation9.1 Calculate actual sealant minimum contact area, D,insquare millimetres (square inches) as follows:D 5 A 3 B (1)where:A = sealant length, Dimension A (see Fig. 1) andB = sealant bite, Dimension B (see Fig. 1).9.2 Calculate tensile stress as

    25、 follows:T 5CD(2)where:T = tensile strength, MPa (psi), andC = tensile load, N (lb).NOTE 7CD5Nmm25 MPa, andCD5lbin.35 psi.10. Report10.1 Report FormThe test results and observations are tobe reported on the form shown in Fig. 2.10.2 Report the following information:10.2.1 Any primer used and any dev

    26、iations from the testmethod such as, if the spacers were removed prior to the21-day cure period, if the curing conditions deviated fromthose listed, and any other deviation from the test method,10.2.2 The actual sealant minimum contact area, in squaremillimetres (square inches) as calculated in 9.1,

    27、10.2.3 Tensile stress in megapascals (pounds per squareinch) at 10, 25, 50, and 100 % and at maximum elongation, ascalculated in 9.2. (Use actual contact area from 10.2.2.),10.2.4 The percent elongation at maximum tensile load,(a) Glass Substrate and Spacer Assembled to Form a Sealant Cav-ity (Tape

    28、or clamp substrates together prior to injecting the sealant.)(b) Sideview of Test Specimen with Spacer Removed(c) End view of Test Specimen with Spacer RemovedNOTE 1Dimension B in Fig. 1(c) is known as the sealant edge bite orsealant contact depth.FIG. 1 Sealant Test SpecimenC 1135 00 (2005)210.2.5

    29、The mode of failure in percent cohesive failure, and10.2.6 Any observation from 8.2.11. Precision and Bias411.1 PrecisionThe precision for this test method is sum-marized in Table 1.11.2 BiasBias depends on strict conformance to this testmethod when both preparing and measuring test specimens.There

    30、was no bias reported in the test results when both acidand neutral curing structural silicone sealants were evaluatedafter both room temperature conditioning and after condition-ing seven days immersed in water prior to testing at roomtemperature.4Supporting data are available from ASTM Headquarters

    31、. Request RR:C24-1028.FIG. 2 Report FormC 1135 00 (2005)3ASTM International takes no position respecting 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 paten

    32、t rights, and the riskof infringement of such rights, are entirely their own responsibility.This standard is subject to revision at any time by the responsible technical committee and must be reviewed every five years andif not revised, either reapproved or withdrawn. Your comments are invited eithe

    33、r for revision of this standard or for additional standardsand should be addressed to ASTM International 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 he

    34、aring you shouldmake your views known to the ASTM Committee on Standards, at the address shown 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 standar

    35、d 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).TABLE 1 Summary of Precision DataNOTE 1 The intervals in Column 1 were determined based on thetesting of five replicates of

    36、two materials at two conditions (representinga total of four materials) tested by either (1) four or (2) three laboratories.I(r)ARepeatabilityI(R)BReproducibilityStress, psiAt 10 % elongation (1) 6 13At 25 % elongation (1) 6 12At 50 % elongation (1) 7 11At 100 % elongation (1) 11 13Ultimate stress/t

    37、ensile (2), psi 38 51Ultimate elongation (2), % 76 126Mode of failure (2):Cohesive failure, % 42 55AIn future use of this test method, the difference between two test resultsobtained in the same laboratory on the same material will be expected to exceedthe intervals I (r) above only 5 % of the time.BIn future use of this test method, the difference between two test resultsobtained in different laboratories on the same material, will be expected to exceedthe intervals I (R) above only 5 % of the time.C 1135 00 (2005)4


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