ASTM E1922-2004 叠层和挤拉制聚合物基质合成材料横断面断裂韧性的标准试验方法

作者:标准资料网 时间:2024-05-15 01:52:18   浏览:9490   来源:标准资料网
下载地址: 点击此处下载
【英文标准名称】:StandardTestMethodforTranslaminarFractureToughnessofLaminatedandPultrudedPolymerMatrixCompositeMaterials
【原文标准名称】:叠层和挤拉制聚合物基质合成材料横断面断裂韧性的标准试验方法
【标准号】:ASTME1922-2004
【标准状态】:现行
【国别】:
【发布日期】:2004
【实施或试行日期】:
【发布单位】:美国材料与试验协会(US-ASTM)
【起草单位】:E08.05
【标准类型】:(TestMethod)
【标准水平】:()
【中文主题词】:韧性;分层的;断裂韧性;聚合材料;高聚物;试验方法
【英文主题词】:translaminarfracturtoughness;laminatedpolymer;pultrudedpolymer;matrixcomposite
【摘要】:TheparameterKTLdeterminedbythistestmethodisameasureoftheresistanceofapolymermatrixcompositelaminatetonotch-tipdamageandeffectivetranslaminarcrackgrowthunderopeningmodeloading.Theresultisvalidonlyforconditionsinwhichthedamagezoneatthenotchtipissmallcomparedwiththenotchlengthandthein-planespecimendimensions.Thistestmethodcanservethefollowingpurposes.Inresearchanddevelopment,KTLdatacanquantitativelyestablishtheeffectsoffiberandmatrixvariablesandstackingsequenceofthelaminateonthetranslaminarfractureresistanceofcompositelaminates.Inacceptanceandqualitycontrolspecifications,KTLdatacanbeusedtoestablishcriteriaformaterialprocessingandcomponentinspection.Thetranslaminarfracturetoughness,KTL,determinedbythistestmethodmaybeafunctionofthetestingspeedandtemperature.Thistestmethodisintendedforroomtemperatureandquasi-staticconditions,butitcanapplytoothertestconditionsprovidedthattherequirementsof9.2and9.3aremet.ApplicationofKTLinthedesignofservicecomponentsshouldbemadewithawarenessthatthetestparametersspecifiedbythistestmaydifferfromserviceconditions,possiblyresultinginadifferentmaterialresponsethanthatseeninservice.Notalltypesoflaminatedpolymermatrixcompositematerialsexperiencethecontainednotch-tipdamageandeffectivetranslaminarcrackgrowthofconcerninthistestmethod.Forexample,thenotch-tipdamagemaybemoreextensiveandmaynotbeaccompaniedbyanysignificantamountofeffectivetranslaminarcrackgrowth.Typically,lowerstrengthcompositematerialsandthosewithasignificantproportionofreinforcingfibersalignedinadirectionperpendiculartothenotchaxismaynotexperiencethecontainednotch-tipdamagerequiredforavalidtest.1.1Thistestmethodcoversthedeterminationoftranslaminarfracturetoughness,KTL,forlaminatedandpultrudedpolymermatrixcompositematerialsofvariousplyorientationsusingtestresultsfrommonotonicallyloadednotchedspecimens.1.2Thistestmethodisapplicabletoroomtemperaturelaboratoryairenvironments.1.3Compositematerialsthatcanbetestedbythistestmethodarenotlimitedbythicknessorbytypeofpolymermatrixorfiber,providedthatthespecimensizesandthetestresultsmeettherequirementsofthistestmethod.Thistestmethodwasdevelopedprimarilyfromtestresultsofvariouscarbonfiber-epoxymatrixlaminatesandfromadditionalresultsofglassfiber-epoxymatrix,glassfiber-polyestermatrixpultrusionsandcarbonfiber-bismaleimidematrixlaminates(1-4,6,7).1.4Arangeofeccentricallyloaded,single-edge-notchtension,ESE(T),specimensizeswithproportionalplanardimensionsisprovided,butplanarsizemaybevariableandadjusted,withassociatedchangesintheappliedtestload.Specimenthicknessisavariable,independentofplanarsize.1.5Specimenconfigurationsotherthanthosecontainedinthistestmethodmaybeused,providedthatstressintensitycalibrationsareavailableandthatthetestresultsmeettherequirementsofthistestmethod.Itisparticularlyimportantthattherequirementsdiscussedin5.1and5.4regardingcontainednotch-tipdamagebemetwhenusingalternativespecimenconfigurations.1.6ValuesstatedinSIunitsaretoberegardedasthestandard.1.7Thisstandarddoesnotpurporttoaddressallofthesafetyconcerns,ifany,associatedwithitsuse.Itistheresponsibilityo......
【中国标准分类号】:G31
【国际标准分类号】:83_140_20
【页数】:5P.;A4
【正文语种】:


下载地址: 点击此处下载
基本信息
标准名称:带圆球手柄
中标分类: 航空、航天 >> 航空器与航天器零部件 >> 机械配件、构件
ICS分类: 航空器和航天器工程 >> 航空航天用零部件
替代情况:QJ 57-79
发布日期:1987-12-18
实施日期:1988-10-01
首发日期:
作废日期:
出版日期:
页数:1页
适用范围

没有内容

前言

没有内容

目录

没有内容

引用标准

没有内容

所属分类: 航空 航天 航空器与航天器零部件 机械配件 构件 航空器和航天器工程 航空航天用零部件