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时间:2020-03-07
《基于高分辨率CT成像的疲劳裂纹扩展行为研究.pdf》由会员上传分享,免费在线阅读,更多相关内容在学术论文-天天文库。
1、!"10406#$%"TG115.28%"120085203009!"#$%#&'((&'()*+))*+,-.CT/0123456789:;,-)*+"./01"2345678(9:",-;<&'"=>=?@ABCD("EFGHI@AJKLMN"OPQRSTU6V(D("WXYZ[TheResearchontheFatiguecrackPropagationbehaviorbasedonTheHigh-ResolutionCTimagingADissertationSubmittedfortheDegreeo
2、fMasteronInstrumentandMeterEngineeringbyLuPengUndertheSupervisionofAssociateProf.AoBoSchoolofTestingandOpto-ElectronicEngineeringNanchangHangkongUniversity,Nanchang,ChinaJune,2015<=2A50]^_`abcd3、}~ÄrÅÇ+ÉÑÖÜhátuàâtxäãåçéèsÖÜêëpíìîÖÜïñ4、#ópòôhöÖÜïñõúùûpü†°¢h£§•¶ßE®©•©™´ÖÜpü†êësijh¨≠Æ2A50Ø∞±Ä≤)*á≥hô¥µrg#∂∑CT)*{5、}~Är∏∞±ü†ÖÜïñx≤¶∫?¢sªy2A50Øüº{6、FΩlmæøÖÜïñ¿¡pÉÑF¬hªy√ƒI⊬#ó?∆ÖÜïñêës«rg#∂∑»…CTáÉÑF¬¬x√ƒGç™´æø¿¡pÖÜïñCT®¯°±sáæøïñ¿¡ÖÜCT®¯°±¬xn°±²³h´µ²³°±áæøÉÑïñ¿¡¶†CTÖÜ°±¬xná·#ós«r¸¹ô´©º»ô´ÖÜ°¢h¼ªyü†½¾¯®©™lÖÜü7、†¿Às«rÁÀÂÃÄmÖÜÅÆhôgnÖÜ°±á·fhlmnÇe»ÈpÖÜCT°±hªyü†½¾¯™lnÁÀÂpü†#ÉsÊ4ËÉÑ¿¡ÖÜ°±ÌÍC¶†Î∆ÏhªyÐÑÎ∆ÏÖÜòÚÖÜÓf)*¶†Î∆ÏÖÜïñ°csô¥nÔıD±Ö×fpÖÜïñ8、∆ô´Ñ©h½r`ô´ÖÜÅpk9、∆hÊ4ËÉÑ¿¡ÖÜÌÍmØk10、∆Ï™lnD±Ö×fÖÜïñ11、∆Ço°¿h´µD±Ö×fÖÜïñ12、∆#ónÖÜïñÓfÖÜïñÙ∑h¼ÐÑlmD±Ö×fÖÜïñ13、∆p?∆ÚÛf≤2.2206˱ֺh½r`ÜÝÖÜC×f®ÞÏïñpˇŁAfsô14、¥nÖÜïñłfiâÐÑšûhÐÑlmäòłžfiâ≤0.25häòÖÜïñæ`łž¿¡svç?èhg#∂∑CTéý½r`ßE∞±këCpÉÑÖÜhü†½¾¯lmpÖÜü†êë½r`#óÖÜpü†ïñx≤s>?@Ag#∂∑ìí°±²³ÃÂÖÜD±Ö×fÖÜ15、∆IAbstract2A50wroughtaluminumalloygetsalargenumberofapplicationsintheaerospaceindustrybecauseofitsgoodplasticityandhighstrengthcharacteris16、tics.Thestructuresoftheaircrafttendtoproducefatiguecracksunderthebendingloadsandwillthreatenthesafetyduringtheflight.Determiningthecrackinformationistheprerequisiteforthecrackpropagationanalysis,andthecrackpropagationhastypicalthree-dimensionalcharacteristics,whileth17、econventionalnon-destructivetestingmethodscan’tobtainthree-dimensionalinformationofcracks.Therefore,inthispaper,2A50wroughtaluminummaterialwasselectedastheobjectofthestudy,andthehigh-resolutionCTimagingmethodwasusedtodotheresearchonthree-dimensionalcrackpropagationbe18、haviorsanddamagecharacterizationunderbendingload.Obtainingthespecimenswithcracksofdifferentstagesofthecrackpropagationbythree-point
3、}~ÄrÅÇ+ÉÑÖÜhátuàâtxäãåçéèsÖÜêëpíìîÖÜïñ
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6、FΩlmæøÖÜïñ¿¡pÉÑF¬hªy√ƒI⊬#ó?∆ÖÜïñêës«rg#∂∑»…CTáÉÑF¬¬x√ƒGç™´æø¿¡pÖÜïñCT®¯°±sáæøïñ¿¡ÖÜCT®¯°±¬xn°±²³h´µ²³°±áæøÉÑïñ¿¡¶†CTÖÜ°±¬xná·#ós«r¸¹ô´©º»ô´ÖÜ°¢h¼ªyü†½¾¯®©™lÖÜü
7、†¿Às«rÁÀÂÃÄmÖÜÅÆhôgnÖÜ°±á·fhlmnÇe»ÈpÖÜCT°±hªyü†½¾¯™lnÁÀÂpü†#ÉsÊ4ËÉÑ¿¡ÖÜ°±ÌÍC¶†Î∆ÏhªyÐÑÎ∆ÏÖÜòÚÖÜÓf)*¶†Î∆ÏÖÜïñ°csô¥nÔıD±Ö×fpÖÜïñ
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11、∆Ço°¿h´µD±Ö×fÖÜïñ
12、∆#ónÖÜïñÓfÖÜïñÙ∑h¼ÐÑlmD±Ö×fÖÜïñ
13、∆p?∆ÚÛf≤2.2206˱ֺh½r`ÜÝÖÜC×f®ÞÏïñpˇŁAfsô
14、¥nÖÜïñłfiâÐÑšûhÐÑlmäòłžfiâ≤0.25häòÖÜïñæ`łž¿¡svç?èhg#∂∑CTéý½r`ßE∞±këCpÉÑÖÜhü†½¾¯lmpÖÜü†êë½r`#óÖÜpü†ïñx≤s>?@Ag#∂∑ìí°±²³ÃÂÖÜD±Ö×fÖÜ
15、∆IAbstract2A50wroughtaluminumalloygetsalargenumberofapplicationsintheaerospaceindustrybecauseofitsgoodplasticityandhighstrengthcharacteris
16、tics.Thestructuresoftheaircrafttendtoproducefatiguecracksunderthebendingloadsandwillthreatenthesafetyduringtheflight.Determiningthecrackinformationistheprerequisiteforthecrackpropagationanalysis,andthecrackpropagationhastypicalthree-dimensionalcharacteristics,whileth
17、econventionalnon-destructivetestingmethodscan’tobtainthree-dimensionalinformationofcracks.Therefore,inthispaper,2A50wroughtaluminummaterialwasselectedastheobjectofthestudy,andthehigh-resolutionCTimagingmethodwasusedtodotheresearchonthree-dimensionalcrackpropagationbe
18、haviorsanddamagecharacterizationunderbendingload.Obtainingthespecimenswithcracksofdifferentstagesofthecrackpropagationbythree-point
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