ImageVerifierCode 换一换
格式:PDF , 页数:4 ,大小:99.36KB ,
资源ID:463494      下载积分:10000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
注意:如需开发票,请勿充值!
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【http://www.mydoc123.com/d-463494.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: 微信登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(ASTM C1135-2000(2011) 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)为本站会员(inwarn120)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

ASTM C1135-2000(2011) 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: C1135 00 (Reapproved 2011)Standard Test Method forDetermining Tensile Adhesion Properties of StructuralSealants1This standard is issued under the fixed designation C1135; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision,

2、 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 laboratory procedure forquantitatively measuring the tensile adhesion propertie

3、s 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 any,

4、 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 C1135; ISO 8339 and ISO

5、8340.2. Referenced Documents2.1 ASTM Standards:2C717 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 C717 for definitionsof th

6、e 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 applic

7、ations 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 Testing Mach

8、ine, 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 firmly gra

9、spthe 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 specimen.5.1.

10、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 for each

11、 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 spacer

12、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 Sealan

13、ts and is the direct responsibility of Subcommittee C24.30 onAdhesion.Current edition approved Jan. 1, 2011. Published March 2011. Originallyapproved in 1990. Last previous edition approved in 2005 as C1135 00(2005).DOI: 10.1520/C1135-00R11.2For referenced ASTM standards, visit the ASTM website, www

14、.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.3Available from American National Standards Institute (ANSI), 25 W. 43rd St.,4th Floor, New York, NY 10036.1Copyright AS

15、TM International, 100 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 solut

16、ion, wipe the substrates 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 for

17、ming a sealant cavity12.7 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.

18、 1).NOTE 4Five test specimen 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 specia

19、l careto strike off the 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 m

20、ust be listed in the 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

21、of 50.8 mm (2.0 in.) 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

22、 0.8 mm (0.03125in.) 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 fai

23、lure.NOTE 5If the substrate 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

24、trapped in the sealant 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 Calcul

25、ate tensile stress as 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 pr

26、imer used and any deviations 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)

27、as calculated in 9.1,10.2.3 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 S

28、ealant Cav-ity (Tape 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 SpecimenC11

29、35 00 (2011)210.2.5 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 t

30、est specimens.There 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 have been filed

31、at ASTM International Headquarters and maybe obtained by requesting Research Report RR:C24-1028.FIG. 2 Report FormC1135 00 (2011)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 a

32、re expressly advised that determination of the validity of any such patent 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

33、 revised, either reapproved or withdrawn. Your comments are invited either 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 y

34、ou 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 below.This standard is copyrighted by ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959,Unite

35、d 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 al

36、so be secured from the ASTM website (www.astm.org/COPYRIGHT/).TABLE 1 Summary of Precision DataNOTE 1 The intervals in Column 1 were determined based on thetesting of five replicates of two materials at two conditions (representinga total of four materials) tested by either (1) four or (2) three lab

37、oratories.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/tensile (2), psi 38 51Ultimate elongation (2), % 76 126Mode of failure (2):Cohesive failure, % 42 55AIn future use

38、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.C1135 00 (2011)4

copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
备案/许可证编号:苏ICP备17064731号-1