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    • 簡(jiǎn)介:碩士學(xué)位論文碩士學(xué)位論文航空諧波減速器性能測(cè)試裝置研制DEVELOPMENTOFANEQUIPMENTFAERONAUTICALHARMONICREDUCERPERFMANCE申倩哈爾濱工業(yè)大學(xué)哈爾濱工業(yè)大學(xué)2014年6月CLASSIFIEDINDEXTP3062UDC621THESISFTHEMASTERDEGREEINENGINEERINGDEVELOPMENTOFANEQUIPMENTFAERONAUTICALHARMONICREDUCERPERFMANCECIDATESHENQIANSUPERVISPROFZHAOYONGPINGACADEMICDEGREEAPPLIEDFMASTEROFENGINEERINGSPECIALITYINSTRUMENTSCIENCETECHNOLOGYAFFILIATIONDEPTOFAUTOMATICTESTCONTROLDATEOFDEFENCEJUNE27TH2014DEGREECONFERRINGINSTITUTIONHARBININSTITUTEOFTECHNOLOGY
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    • 下載積分: 5 賞幣
      上傳時(shí)間:2024-03-01
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    • 簡(jiǎn)介:中國(guó)民用航空學(xué)院碩士學(xué)位論文基于計(jì)算機(jī)視覺的航空發(fā)動(dòng)機(jī)孔探技術(shù)研究姓名李研強(qiáng)申請(qǐng)學(xué)位級(jí)別碩士專業(yè)導(dǎo)航、制導(dǎo)與控制指導(dǎo)教師羅云林20040214里墾旦塾至蘭墮堡蘭蘭壘笙壅一ABSTRACTTHETECHNIQUEOFHOLEDETECTIONISVERYIMPORTANTMETHODTOTHEMAINTENANCEOFAVIATIONENGINEINPAST,THEDETECTIONOFAVIATIONENGINEWASVIAARTIFICIALLYINSPECTIONBYFIBROUSENDOSCOPEACCORDINGHUMANEXPERIENCES,THEFAULTWASESTIMATEDSOTHEHUMANFACTORANDDIFFICULTYOFDETECTIONISHAPPENEDWITHTHEDEVELOPMENTOFIMAGEPROCESSINGANDCOMPUTERVISION,ANEWMETHODOFHOLEDETECTIONCOMEINTOBEINGBASEDONVISIONTECHNIQUETHEIMAGINGANALYZINGOFHOLEDETECTIONIMAGEHASBEENVERYIMPORTANTINENGINEFAULTDIAGNOSISRESEARCHINGANDDEVELOPINGTHESYSTEMOFTHREEDIMENSIONSMEASUREANDSTEREEBUILDINGBASEDONHOLEDETECTIONIMAGEISVERYNECESSARYFORIMPROVINGTHELEVELOFDIAGNOSISANDMEASUREMEM,ANDREDUCINGTHECOSTOFHUMANANDPHYSICALTHING,SAVINGTHECOSTOFMAINTENANCEWITHTHEDEVELOPMENTOFELECTRONICENDOSCOPEANDIMAGEPROCESSINGANDCOMPEERTECHNIQUE,THISSUBJECT“THERESEARCHOFTECHNIQUEOFHOLEDETECTIONOFAVIONICENGINEBASEDONCOMPUTERVISION”ISPOSSIBLEITPROVESTHEPOSSIBILITYANDGIVESTHESCHEMEWHOLE,ANDANALYZESTHETHEORYABOUTTHEKEYTECHNIQUEITGIVESTHEINTRODUCTIONOFTHEHARDWAREANDSOFTWAREINDETAILSANDATTHESAMETIMESHOWTHEMETHODOFREALIZATIONINPARTLYTHERESEARCHOFTHESUBJECTCANDOSOMEGOODTHINGSTOIMPROVETHEHOLEDETECTIONTECHNIQUEANDTHEMODEMIZATIONOFCIVILAVIATIONKEY、VORDAVIATIONENGINEHOLEDETECTIONIMAGEPROCESSINGCOMPUTERVISION兒
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      上傳時(shí)間:2024-03-01
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    • 下載積分: 5 賞幣
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    • 簡(jiǎn)介:分類號(hào)密級(jí)UDC編號(hào)河北工業(yè)大學(xué)碩士學(xué)位論文民用航空飛機(jī)實(shí)時(shí)參數(shù)信息提取民用航空飛機(jī)實(shí)時(shí)參數(shù)信息提取方法研究及驗(yàn)證方法研究及驗(yàn)證論文作者李永津?qū)W生類別全日制專業(yè)學(xué)位類別工程碩士領(lǐng)域名稱電子與通信工程指導(dǎo)教師李景春職稱教授級(jí)高級(jí)工程師資助基金項(xiàng)目國(guó)家自然科學(xué)基金(61139001)
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 61
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    • 簡(jiǎn)介:大連理工大學(xué)碩士學(xué)位論文高強(qiáng)抗熱腐蝕航空渦輪葉片材料(DZ68)的初步研制姓名于忠鋒申請(qǐng)學(xué)位級(jí)別碩士專業(yè)材料表面工程指導(dǎo)教師于永泗鄭志20070601高強(qiáng)抗熱腐蝕航空渦輪葉片材料DZ68的初步研制PRIMARYDEⅦLOPM匝NTOFHIGHS眥N冊(cè)ANDHOTCORROSIONITESISTANCEAEROENGINETURBINEBLADEMATER【ALDZ68ALLOYABSTRACTINORDERTOMEETTHEREQUIREMENTSOFMARINEGASTURBINEBLADEMATERIALSANEWTYPEDDIRECTIONALSOLIDIFICATIONNICKELBASESUPERALLOYDZ68ALLOYWASDEVELOPEDSODZ68ALLOYSHOULDHAVEHIGLLTEMPERATURECAPABILITYANDGOODHOTCORROSIONRESISTANCEONTHEBASISOFRENE’142,DZL25LANDDZ38G0M38ALLOYSDZ68WASMADEBYOURSELVESWITHLOWSEGREGATIONNESEGREGATINGLIGHTLYPPHASEFORMINGELEMENTSOFAIANDTAA塢ADDEDINTODZ68FORPRECIPITATIONHARDENINGTHISALLOYHASASMALLAMOUNTOFTIANDNOHFORNBSEGREGATINGSEVERELYELEMENTSHI曲CONTENTSOFREFRACTORYELEMENTSSUCH勰WANDRE眥ADDEDFORSOLIDSOLUTIONSTRENGTHENINGANDHIP血CRCONTENTISADDEDINTODZ68FORHOTCOITOSIONRESISTANCEN屺HEATTREATMENTOFDZ68ISCOMPOSEDOFPRIORHOMOGENEOUSLREATMENTSOLIDSOLUTIONTREATMENTANDTWOAGINGTREATRNENTSTHEWHOLEHEALTREATMENTASFOFLOWS1240℃/05HRS1260℃/05HRS1280℃/2HRSAIRC0011120℃/4HRSONEHOURCOOITO1080℃1080℃/4HRSAIRCOOL,900℃/4HRSAIRC001MECHANICALPROPERTIESOFDZL25,DZ38GANDDZ68一LALLOYSAFTEREACHHEATTREATMENTHAVEBEENCOMPAREDINTHISPAPERTHCRUPTURECONDITIONSAIEINTHEC螄SOF980℃/235MAAND980℃/245M腿低HOTCORROSIONRESISTANCESOFDZL25LDZ38GANDIZ68一LALLOYSHAVEBEENCOMPAREDATTHECONDITIONSOF900℃AND75%NAZSOT十25%NACLMOLTENSALT11”MECHANICALLYEXPERIMENTALRESULTSSHOWTHATTHEMECHANICALPROPERTIESOFDZ681ARHIG虹BECAUSETHE1一VOLUMEFACTIONOFDZ681ISABOUT50%ANDITCONTAINSACERTAINAMOUNTSOFWANDRE11艟ROOMTEMPERATURETENSILEPROPERTIESOFDZ681撒SIMILARTODZL25,THEEXTENSIONSTRENGTHANDEXTENSIBILNYOFDZ380ISPOOL111ERUPTUREPROPERTIESOFDZ68LALEEQUIVALENTTODZL25INTHEEXPERIMENTALCAS器ANDBETTERTHANTHATOFDZ38GTHEHOTCORROSIONEXPERIMENTALRESULTSSHOWTHATTHEHOTCORROSIONRESISTANCEOFDZ681ISEQUIVALENTTODZ38GALLOYANDBETTERTHANTHATOFDZL25LINTHISPAPERTHEHOTCORROSIONMECHANISMOFTHRECALLOYSISPREVIOUSLYPROPOSEDTHEBASICDISSOLUTIONMODEL11碓PROCESSESOFTHEIRHOTCORROSIONAREDIFFERENTFURWHICHTHEYHAVEDIFFERENTCOMPOSITIONS,CORROSIVEPRODUCTIONSANDⅡLIC∞蚰ⅫTLL潞DZL25LALLOYISCORRODEDSEVERELYAFTERSHORTTIME;DZ38GALLOYISLOCALLYCORRODEDSERIOUSLYFORITSNONUNIFORMMICROSTRUCTARE;DZ68LALLOYHASA
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    • 簡(jiǎn)介:南京航空航天大學(xué)碩士學(xué)位論文CALS技術(shù)及其在航空產(chǎn)品維修保障中的應(yīng)用研究姓名王金偉申請(qǐng)學(xué)位級(jí)別碩士專業(yè)機(jī)械電子工程指導(dǎo)教師樓佩煌200231CALS技術(shù)及其在航空產(chǎn)品維修保障中的應(yīng)用研究ABSTRACTWEAPONSYSTEMSAREBECOMINGTOOCOMPLEXOWINGTOTHEDEVELOPMENTOFSCIENCEANDTECHNOLOGYHOWEVERHIGHTECHWEAPONCANEXERTADVANCEDTECHNOLOGYUNDERHIGHTECHLOGISTICSSUPPORTSYSTEMTHESEARECHALLENGESFORLOGISTICSSUPPORTTECHNOLOGYTHISTHESISFIRSTLYINTRODUCESNEWDEMANDSOFAERIALPRODUCTLOGISTICSSUPPORTUNDERHIGHTECHWARANDSOMEDEFECTSOFTRADITIONALLOGISTICSSUPPORT,ANDPUTSFORWARDAKINDOFSYSTEMMODELOFAERIALPRODUCTLOGISTICSSUPPORTFOLLOWINGDATASHARINGOFCALS,ANDEMPHASIZESIETMSECONDLYITSETSFORTHAPPLICATIONOFSTEPANDXMLINTHEIETM,RESEARCHSCONVERSIONOFXMLSCHEMAANDRELATIONSCHEMA,ANDSIMPLYRESEARCHSMAPPINGOFXMLANDEXPRESSAFTERWORD,ABASEDXMLFRAMEWORKOFINFOTRANSFERBETWEENDIFFERENTPLATFORMAREPRESENTED,ACCORDINGTOTHISFRAMEWORK,THEAUTHORESTABLISHAARCHETYPALSYSTEMOFHELICOPTERINFORMATIONQUERYSYSTEMBASEDXMLANDDBMSINTHEEND,AFTERTHESUMUPOFTHEWHOLEPAPER,SOMEFURTHERRESEARCHESARESUGGESTEDKEYWORDSCALS、LOGISTICSSUPPORT、IETM、STEP、XML、DATABASE。第1I頁(yè)
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 60
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    • 簡(jiǎn)介:合肥工業(yè)大學(xué)碩士學(xué)位論文航空發(fā)動(dòng)機(jī)主軸軸承可靠性技術(shù)研究姓名焦育潔申請(qǐng)學(xué)位級(jí)別碩士專業(yè)機(jī)械工程指導(dǎo)教師呂新生張錫昌20040301RESEARCHONRELIABILITYTECHNOLOGYFORMAINSHAFTBEARINGSOFAIRCRAFTENGINETHEMAINSHAFTBEARINGSOFAIRCRAFTENGINEAREKEYPARTSOFPLANEITSRELIABILITYANDLIFEAFFECTDIRECTLYONTHERELIABILITYANDLIFEOFENGINEANDEVENWHOLEPLANETHISPAPERESTABLISHEDASITEDATACOLLECTSYSTEMANDADATAMANAGEMENTSYSTEMFORTHEMAINSHAFTBEARINGSOFAIRCRAFTENGINECOLLECTEDALOTOFDATUMANDFAILURESAMPLESTHROUGHSTATISTICANALYSISOBTAINEDTHEMAJORFAILUREMODELOF廿LEBEARINGSANDITSPRINCIPLEOFFORMATION,ANDPUTSOMESPECIFICMEASURESTHATCANPREVENTBEARINGFROMFAILINGINEARLYSTAGETOIMPROVEITSRELIABILITVWCRESEARCHEDANDESTABLISHEDDATAMODELOFTHESITEDATAFORTHEMAINSHAFTBEARINGSANDAPPRAISEDITSRELIABILITYLIFEBYTHESURVIVINGRATIOMETHODT11EMEANHITCHMETHODANDTHEACCUMULATEDHITCHMETHODTHEMINIMUMSQUAREMETHODWASUSEDINREGRESSINGANALYSISFORTHERESULTOFTREATMENTINASUPPOSEDDIS仃IBUTIONFUNCTION,THE“D”EXAMINATIONMETHODWASUSEDFORWEIBULLDISTRIBUTIONANDINDEXDISTRIBUTION,ANDOBTAINEDTHEDISTRIBUTIONTYPEINTHELIFEOFTILEMAINSHAFTBEARINGS,APPRAISEDTHERELIABILITYLIFE,THEMEANLIFEANDTHERELIABILITYIN500HOURSOF廿1EMAINSHAFTBEARINGSWITILTHEORETICALDISTRIBUTIONFUNCTIONW_ERESEARCHEDTHEPECULIARITYOFTHESMALLANDNOLOSSINE伍CACYSAMPLEBOOKANDESTABLISHED廿LERELIABILITYTESTMETHOD,ADVANCEDACHECKPLANFORRELIABILITVTESTMEETINGASPECIFIEDRELIABILITYREQUIREMENTOFTHEMAINSHAFTBEARINGSTHEIMPROVEDBEARINGSWERETESTEDIN500H。600HAND900H,ANDTHERESULTSOF廿LETESTWEREANALYZEDKEYWORDSMAINSHAFTBEARING,F(xiàn)AILURE,RELIABILITY
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    • 簡(jiǎn)介:大連理工大學(xué)碩士學(xué)位論文航空配載與重量平衡計(jì)算系統(tǒng)姓名苗森申請(qǐng)學(xué)位級(jí)別碩士專業(yè)軟件工程指導(dǎo)教師周東清20071125航空配載與重量平衡計(jì)算系統(tǒng)THEAIRCRAFTWEIGHTANDBALANCESYSTEMKBSTRACTASONEADVANCODANDMODEMTRANSPORTMODEAIRTRANSPORTHASBEENDEVELOPEDATFULLSPEEDANDFOCUSEDONWIDELYINTHEFIELDSOFINTERNATIONALTRANSPORTATIONANDBECOMESTHEQUICKESTTRANSPORTMODEWHICHGUARANTEESTHEINTERNATIONALTRADEAILOVERTILEWORLDINFUTURETRANSPORTATIONOFINTERNATIONALTRADE,AIRTRANSPORTWILLBECOMEONEOFTHEMOSTIMPORTANTROLESANDEFFECTIVESTRENGTHINMODEMTRANSPORTATION,11艟DEVELOPMENTOFITACCOMPANIEDWITHTHERESEARCHACHIEVEMENTOFAIRCRAFTWEIGHTANDBALANCESUPPLYTHEBASICTILEORYANDTECHNICALSUPPORTDURINGTHEPROCESSOFDEVELOPMENTANDRESEARCHOFAIRCRAFTWEIGHTANDBALANCEPROG舢WEIGHTANDBALANCEISANIMPORTANTPIOCEDUREOFAIRTRANSPORTFILLINGLOADINGSHEETANDWEIGHTBALANCESHEETMANYDATASHOULDBEPROCESSEDWITHTHECHARACTERISTICSOFACCU陽(yáng)TCCA_LCTFIATIONMUCH】IMITAFIONANDTIGHTTIMETHEAIRCRAFTWEIGHTANDBALANCESYSTEMHELPSS詛FRWORKMOREEFFNCIENTLY。MOREACCURATELYANDMOREINTELLECTUALLYTHEAIRCRAFTWEIGHTANDBALANCESYSTEMISANAPPLICABLEMODULEOFCOMPUTERDEPARTURESYSTEMANDMAINLYUSEDBYSTAFFOFAIRLINESANDAIRCARGOTERMINALSITCANBEUSEDEITHERACCOMPANIEDBYTHEOTHERSYSTEMORALONEWEIGHTANDBALANCINGISTHENECESSARYPROCEDUREBEFOREDEPARTURETHESTAFFOFWEIGHTANDBALANCEDEPARTMENTSHOULDCONSIDERALLKINDSOFFACTORSWHICHINFLUENCETHEBALANCEOFAIRCRAFTTHENDECIDETHESCALLEI“OFLOADINGANDCHEEKIFTHEWEIGHTANDCENTEROFGRAVITYISWITHINTHEREGULATEDLIMITATIONAFTERGETTINGTHERELEVANTAIRCRAFTDATAWEIGHTANDBALANCINGALSOCANBEPROCESSEDBYMATLPOWERBUTIT’SVERYCOMPLICATEDANDEASILYAFFECTEDBYARTIFICIALFACTORSWHICHRESULTINEITORSMEANWHILETHESPACEANDMAXIMUMLOADOFCABINETCAN’TBEUSEDSUFFICIENTLYTRADITIONALWEIGHTANDBALANCINGCALLONLYUSE50%SPACEAND70%LOADING,THECOMPUTERSYSTEMANDMANPOWERJOBFOLLOWTHESAMEFLOW,ESTABLISHCOMPLETEOUTBOUNDCARGODATABASE,PUTTHECARGOINORDERACCORDINGTOLIMITATIONSANDCHOOSETHEBESTCOMMODITYFORTHEOTHERCONSIDERINGTHESPACEANDLOADINGUSAGE,INTELLECTUALWEIGHTANDBALANCESYSTEMHELPSBALANCINGDEPARTMENTGAINHIGHE伍FICIENCY,ACCURACYANDBENEFITKEYWORDSAIRTRANSPORT;WEIGHT;BALANCING;CENTEROFGRAVITYII
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    • 簡(jiǎn)介:浙江大學(xué)碩士學(xué)位論文綜合應(yīng)力作用下航天電連接器加速壽命試驗(yàn)的研究姓名李奇志申請(qǐng)學(xué)位級(jí)別碩士專業(yè)機(jī)械設(shè)計(jì)及理論指導(dǎo)教師陳文華盧獻(xiàn)彪20040201浙江大學(xué)碩士學(xué)位論文ABSTRACTINTHISDISSERTATION,THEMODELY11X1419ELECTRICALCONNECTORASTHEOBJECT、UNDERTEMPERATUREANDVIBRATIONSTRESSES,THEFAILUREMECHANISMHASBEENANALYZED.THERELIABILITYMODELHASBEENBUILT,BASEDONABOVE,THERELIABILITYTESTMETHODOFELECTRICALCONNECTORSHASBEENDEEPLYRESEARCHEDANDTHEDATEDRAWINGFROMTESTEXPERIMENTWASTREATED.FIRST,BRIEFLYSTATEDTHEDEVELOPINGHISTORYANDCURRENTSITUATIONOFRELIABILITYENGINEERING,INTRODUCETHERELIABILITYTESTMETHODANDDEVELOPINGTRENDSMOREOVER,THESTATISTICALANALYSISMETHODANDEXISTINGPROBLEMS,ELECTRICALCONNECTORSRELIABILITYRESEARCH’SCURRENTSITUATIONANDEXISTINGPROBLEMS,ANDRELIABILITYTESTPLANANDEXISTINGPROBLEMSWASPRESENTATION.SECOND,THROUGHANALYZINGTHERELATIONBETWEENTHETEMPERATUREANDVIBRATIONSTRESSANDTHELIFEOFCONNECTOR,ANDCOMBININGWITHTHETHEORYOFPROBABILITYANDSTATISTICS,DEDUCETHEFAILUREPHYSICSEQUATION,ANDSETUPARELIABILITYSTATISTICALMODEL.LAIDAFOUNDATIONFORWORKINGOUTELECTRICALCONNECTORRETIABILITYTESTPLANSANDTREATINGELECTRICALCONNECTORSTESTDATA.,THIRD.PROPOSEDANDRESEARCHEDOPTIMIZINGDESIGNMODEOFCONSTANTSTRESSACCELERATED1IRETESTPLANSUNDERTHETEMPERATUREANDVIBRATIONSTRESSES.ACCORDINGTOTHISMODE,UNDERTHETEMPERATUREANDVIBRATIONSTRESSES,ANDCOMBININGWITHUNIFORMLYORTHOGONALDESIGNTHEORY,ANDOPTIMIZEDTHETESTPLANSOFELECTRICALCONNECTOR.THERESULTSHOWSTHAT,THROUGHOPTIMIZINGTESTPLANUNDERTHECONDITIONOFESTIMATEPRECISIONKEEPINGFIXED,THETIMESOFTESTANDCORRESPONDINGNUMBEROFSPECIMENSMAYBEREDUCED,THUS,THETIMEMAYBESHORTENEDANDTESTCOSTREDUCEDGREATLY.BYTHISMEANS,PRODUCTRELIABILITYLEVELMAYBEEVALUATEDQUICKLY.FOURTH,PROPOSEDANDRESEARCHEDTHEEVALUATIONMETHODOFACCELERATEDLIFETESTPLANSBYSIMULATION.0NTHEBASISOFSIMULATINGEVALUATIONTOVARIOUSELECTRICALUSINGUNIFORMLYORTHOGONALDESIGNTHEORYTOARRANGETHEFOURLEVERTEMPERATURESANDFOUR.1EVERVIBRATIONSTRESS,CATCHANEXCELLENTACCELERATEDLIFETEXTPLAN.WHICHMAKETHEESTIMATEVALUEHAVETHEWELLPRECISIONINNORMALSTRESSLEVER,ATTHESAMETIMETHATCARLREDUCETHESAMPLENUMBERANDSHOLTENTHETESTTIME.FIFTH.THROUGHSTATISTICALANALYSISOFELECTRICALCONNECTORACCELERATEDLIFETESTDATA.VERIFIEDTHATTHERELIABILITYSTATISTICALMODELOFELECTRICALCONNECTORISCORRECTTHEN.TOOKLEASTSQUARESESTIMATOROFTESTDATAASPRELIMINARYESTIMATE,APPLIEDVERSATILEMAXIMUMLIKELIHOODESTIMATEMETHODTOTREATTESTDATA,OBTAINEDTHEESTIMATORSOFELECTRICALCONNECTORRELIABILITYCHARACTERISTICVALUES.EVENTUALLY.GAVEACONCLUSIONTORESEARCHCONTENTOFENTIREDISSERTATION,ANDPROPOSEDTHERESEARCHCONTENTOFTHERELIABILITYTESTANDANALYSISOFELECTRICALCONNECTORS,ANDTHERESEARCHDIRECTIONOFTHISFOUNDATIONPROJECTKEYWORDSELECTRICALCONNECTOR,ENVIRONMENTMULTIPLESTRESSES,RELIABILITY,ACCELERATEDLIFETESTII
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    • 簡(jiǎn)介:中圖分類號(hào)V355論文編號(hào)102870715S033學(xué)科分類號(hào)082303碩士學(xué)位論文機(jī)場(chǎng)航空器滑行路徑優(yōu)化技術(shù)研究研究生姓名陳浩學(xué)科、專業(yè)交通運(yùn)輸規(guī)劃與管理研究方向空中交通流量管理指導(dǎo)教師王湛講師南京航空航天大學(xué)研究生院民航學(xué)院二О一五年三月NANJINGUNIVERSITYOFAERONAUTICSANDASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFCIVILAVIATIONRESEARCHONOPTIMIZATIONTECHNIQUESOFAIRPORTAIRCRAFTTAXIPATHATHESISINTRANSPORTATIONPLANNINGANDMANAGEMENTBYCHENHAOADVISEDBYLECTURERWANGZHANSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFORTHEDEGREEOFMASTEROFENGINEERINGMARCH,2015
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    • 簡(jiǎn)介:分類號(hào)丁厶妨6密級(jí)公哥⑧單位代碼10422學(xué)號(hào)汐I(xiàn)ITL啦∥戶茹只番SHANDONGUNIVERSITY碩士學(xué)位論文THESISFORMASTERDEGREE論文題目理干I,厶夠虢空綴硼扔同型復(fù)件1刀崗I『毅捐承使鉑哥友%娜伽七叫%一冬耐~矗擁,,N,D如桫手FE肌幣廠負(fù)P場(chǎng)P凹躐Q尸;C反F戶R千5作者姓名與;鳴肆培養(yǎng)單位盤煎查塞鱟I魚專業(yè)名稱札樹釧刪自動(dòng)億指導(dǎo)教師畝L埔緩教授合作導(dǎo)師≯T峰年F月≥。日原創(chuàng)性聲明本人鄭重聲明所呈交的學(xué)位論文,是本人在導(dǎo)師的指導(dǎo)下,獨(dú)立進(jìn)行研究所取得的成果。除文中已經(jīng)注明引用的內(nèi)容外,本論文不包含任何其他個(gè)人或集體已經(jīng)發(fā)表或撰寫過的科研成果。對(duì)本文的研究作出重要貢獻(xiàn)的個(gè)人和集體,均己在文中以明確方式標(biāo)明。本聲明的法律責(zé)任由本人承擔(dān)。論文作者簽名皇道益日期X堅(jiān)苧里關(guān)于學(xué)位論文使用授權(quán)的聲明本人完全了解山東大學(xué)有關(guān)保留、使用學(xué)位論文的規(guī)定,同意學(xué)校保留或向國(guó)家有關(guān)部門或機(jī)構(gòu)送交論文的復(fù)印件和電子版,允許論文被查閱和借閱;本人授權(quán)山東大學(xué)可以將本學(xué)位論文的全部或部分內(nèi)容編入有關(guān)數(shù)據(jù)庫(kù)進(jìn)行檢索,可以采用影印、縮印或其他復(fù)制手段保存論文和匯編本學(xué)位論文。保密論文在解密后應(yīng)遵守此規(guī)定論文作者簽名墨絲壟導(dǎo)師簽名
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    • 簡(jiǎn)介:西北工業(yè)大學(xué)碩士學(xué)位論文航空有機(jī)玻璃疲勞裂紋特性的試驗(yàn)研究姓名賈敬華申請(qǐng)學(xué)位級(jí)別碩士專業(yè)固體力學(xué)指導(dǎo)教師李亞智20060301西北工業(yè)太學(xué)碩士學(xué)位論文ABSTRACTPOLYMETHYLMETHACRYLATEPMMAHASBEENWIDELYUSEDASTHETRANSPARENTMATERIALOFTHEAIRCRAFTCANOPIESBECAUSEOFITSPROPERTIESOFEXCELLENTTRANSPARENCYANDSTRENGTHTHEUNDERSTANDINGTOITSFATIGUEBEHAVIOURISONEOFTHEKEYPARISOFTHEFATIGUELIFEPREDICTIONOFAIRCRAFTSTRUCTURESYBMD3PMMAHASBEENUSEDINSEVERALCHINESEAIRCRAFTTYPESASTHECANOPYTRANSPARENTSTRUCTURALMATERIALSINORDERFORUSINGTHEMATERIALSAFELYANDECONOMICALLYITISOFENGINEERINGSIGNIFICANCETOSTUDYTHERESPONSEOFTHEKINDOFDAMAGECONTAINEDMATERIALSANDSTRUCTURESWITHSTANDINGSERVICELOADINGQUANTITATIVELYANDTODEVELOPCORRESPONDINGANALYTICALTECHNIQUESTHEMAINPURPOSEOFTHISDISSERTATIONISTOCHARACTERIZEITSFATIGUECRACKPROPAGATIONBEHAVIOUREXPERIMENTALLY,ANDTHEREBYTOOFFERBASISTOTHEEVALUATIONOFTHERESIDUALLIFEANDTHEMAINTENANCEGUIDELINEOFCANOPYSTRUCTURESANEXPERIMENTALSTUDYOFSTABLEFATIGUECROCKPROPAGATIONBEHAVIORWASCARRIEDOUTATROOMTEMPERATUREDURINGTHEPREPARATIONOFINITIALTHROUGHFATIGUECRACKSFORMTSPECIMENS,LOADCYCLESWITHCOMPRESSIVEPORTIONDEMONSTRATESBERERQUALITYTHANUSUALTENSIONTENSIONLOADINGTHEFATIGUECROCKPROPAGATIONRATEINPARIS’SREGIONFORCERTAINLOADRATIOSHOWSGOODCORRELATIONWITHASTRAIGHTLINEINDOUBLELOGARITHMICDA/DN△KCOORDINATETHEDAMNANDTHESLOPEOFTHESTRAIGHTLINEINCREASESWITHTHEINCREASEOFLOADRATIOFORTHENEGATIVELOADRATIOS,HOWEVERTHECOMPRESSIVEPORTIONINLOADCYCLESACCELERATESTHECRACKGROWTHAPROPERFORMULATIONTOTHESEEFFECTSISUNAVAILABLETHEN,THEWALKER’SEQUATIONWASDRAWNUPFORTHEPOSITIVELOADRATIOS,AMODIFIEDWALKER’SEQUATIONISDEVELOPEDANDGIVESAGOODREGRESSIONTOTHEBEHAVIOROFTHEPMMAMATERIALWHILEFORTHENEGATIVELOADRATIOS,THECOMPRESSIVEPORTIONINLOADCYCLESACCELERATESTHECRACKGROWTHOFTHEPMMATHEINFLUENCEOFTHECOMPRESSIVEPORTIONOFTHELOADCYCLESONTHEFATIGUECRACKPROPAGATIONRATEFCPRMAYBEINTERPRETEDBYTHEPLASTICITYINDUCEDCRACKCLOSUREPHENOMENONANDAPROPERFORMULATIONISSOFARUNAVAILABLE1I
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    • 簡(jiǎn)介:碩士學(xué)位論文碩士學(xué)位論文航天器撓性附件動(dòng)力學(xué)相似性理論及實(shí)驗(yàn)研究RESEARCHOFSPACECRAFTFLEXIBLEATTACHMENTDYNAMICSSIMILARITYTHEORYANDEXPERIMENT譚利臨譚利臨哈爾濱工業(yè)大學(xué)哈爾濱工業(yè)大學(xué)2012015年6月CLASSIFIEDINDEXV416UDC620DISSERTATIONFORTHEMASTER’SDEGREEINENGINEERINGRESEARCHOFSPACECRAFTFLEXIBLEATTACHMENTDYNAMICSSIMILARITYTHEORYANDEXPERIMENTCANDIDATETANLILINSUPERVISORPROFQINAIMINGACADEMICDEGREEAPPLIEDFORMASTEROFENGINEERINGSPECIALITYSPACECRAFTDESIGNAFFILIATIONDEPTOFASTRONAUTICENGINEERINGDATEOFDEFENCEJUNE,2015DEGREECONFERRINGINSTITUTIONHARBININSTITUTEOFTECHNOLOGY
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      頁(yè)數(shù): 69
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    • 簡(jiǎn)介:中國(guó)民用航空學(xué)院碩士學(xué)位論文摘要論文緊密結(jié)合航空發(fā)動(dòng)機(jī)維修中的實(shí)際問題,對(duì)維修過程中的裝配間隙對(duì)發(fā)動(dòng)機(jī)性能的影響進(jìn)行統(tǒng)計(jì)分析,介紹了多元線性回歸的基本理論和方法,重點(diǎn)分析了發(fā)動(dòng)機(jī)裝配間隙對(duì)風(fēng)扇壓氣機(jī)和渦輪性能的影響。論文完成以下主要工作T收集了AMECO近年來維修的PW4000發(fā)動(dòng)機(jī)的裝配間隙數(shù)據(jù)和試車數(shù)據(jù),并對(duì)數(shù)據(jù)進(jìn)行整理,以此作為統(tǒng)計(jì)分析的依據(jù)2用相關(guān)分析和逐步回歸方法選擇那些對(duì)發(fā)動(dòng)機(jī)性能有重要影響的間隙,將選出來的間隙與EGT建立多元線性回歸模型和多元非線性回歸模型,通過計(jì)算以及對(duì)回歸模型的檢驗(yàn)后,給出兩種模型下的擬合效果圖,繪出EGT隨間隙變化的性能曲線圖,最后還分別用兩種模型進(jìn)行預(yù)測(cè),得到合理的結(jié)果3通過逐步回歸方法選擇對(duì)發(fā)動(dòng)機(jī)其余的性能參數(shù)如N2NT和WF有重要影響的間隙,將這些選出來的間隙與三個(gè)性能參數(shù)建立多元非線性回歸模型,通過計(jì)算和對(duì)回歸模型的檢驗(yàn)后,給出在該模型下的擬合效果圖,繪出三個(gè)性能參數(shù)隨間隙變化的性能曲線圖,最后還分別用該模型對(duì)四個(gè)樣本進(jìn)行預(yù)測(cè),得到合理的結(jié)果4用逐步回歸方法選擇出對(duì)發(fā)動(dòng)機(jī)的推力有重要影響的間隙,并建立間隙與推力之間的多元線性回歸模型并通過該模型進(jìn)行預(yù)測(cè),得到合理的結(jié)果結(jié)合課題工作,論文利用VC和ODBC數(shù)據(jù)庫(kù)開發(fā)了應(yīng)用程序,通過該程序可以對(duì)EGT等航空發(fā)動(dòng)機(jī)性能參數(shù)進(jìn)行了分析,為評(píng)估、預(yù)測(cè)裝配間隙對(duì)發(fā)動(dòng)機(jī)性能影響提供了參考,為以后發(fā)動(dòng)機(jī)維修提供參考和指導(dǎo)。關(guān)鍵詞航空發(fā)動(dòng)機(jī)間隙性能分析多元回歸分析一一一一一一一一一一一一絲韭遇碩士學(xué)位論文ACCORDINGTOTHEACHIEVEMENTOFTHEPROJECTANAPPLICATIONPROGRAMISDEVELOPEDBYVCLANGUAGEANDODBCDATABASESUCHPROGRAMCANBEUSEDTOANALYZETHEPERFORMANCEPARAMETERSSUCHASEGTN2N1ANDWEITALSOCANGIVESOMEREFERREDADVICEOFMAINTENANCEWHENTHEINFLUENCETHATTOLERANCECLEARANCESAFFECTEDAEROENGINEPERFORMANCEISESTIMATEDANDFORECASTEDKEYWORDAEROENGINETIPCLEARANCEPERFORMANCEMULTIREGRESSIONM
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