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簡介:中圖分類號V2319TN9117論文編號102870213S025學(xué)科分類號082502碩士學(xué)位論文航空發(fā)動(dòng)機(jī)多混疊微弱振動(dòng)信號的識別與分離方法研究研究生姓名郭海東學(xué)科、專業(yè)航空宇航推進(jìn)理論與工程研究方向推進(jìn)系統(tǒng)振動(dòng)檢測與診斷指導(dǎo)教師李舜酩教授南京航空航天大學(xué)研究生院能源與動(dòng)力學(xué)院二О一三年一月承諾書本人聲明所呈交的碩士學(xué)位論文是本人在導(dǎo)師指導(dǎo)下進(jìn)行的研究工作及取得的研究成果。除了文中特別加以標(biāo)注和致謝的地方外,論文中不包含其他人已經(jīng)發(fā)表或撰寫過的研究成果,也不包含為獲得南京航空航天大學(xué)或其他教育機(jī)構(gòu)的學(xué)位或證書而使用過的材料。本人授權(quán)南京航空航天大學(xué)可以將學(xué)位論文的全部或部分內(nèi)容編入有關(guān)數(shù)據(jù)庫進(jìn)行檢索,可以采用影印、縮印或掃描等復(fù)制手段保存、匯編學(xué)位論文。(保密的學(xué)位論文在解密后適用本承諾書)作者簽名日期
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上傳時(shí)間:2024-03-01
頁數(shù): 98
大?。?4.18(MB)
子文件數(shù):
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簡介:南京航空航天大學(xué)博士學(xué)位論文航空發(fā)動(dòng)機(jī)高速滾動(dòng)軸承力學(xué)特性研究姓名唐云冰申請學(xué)位級別博士專業(yè)航空宇航推進(jìn)理論與工程指導(dǎo)教師高德平20051101航空發(fā)動(dòng)機(jī)高速滾動(dòng)軸承力學(xué)特性II軸承系統(tǒng)振動(dòng)的主要因素之一。建立了一種滾動(dòng)軸承轉(zhuǎn)子系統(tǒng)分析模型,研究了質(zhì)量、剛度對系統(tǒng)穩(wěn)定性和振動(dòng)特性的影響規(guī)律。綜上所述,本文分別研究了滾動(dòng)軸承的載荷分布、剛度和阻尼特性、疲勞壽命、滑動(dòng)分析以及軸承系統(tǒng)振動(dòng)等方面的問題。研究結(jié)果對于提高航空發(fā)動(dòng)機(jī)主軸軸承的設(shè)計(jì)、制造、使用和維護(hù)具有重要的理論意義和工程應(yīng)用價(jià)值。關(guān)鍵詞滾動(dòng)軸承,載荷分布,等效剛度,疲勞壽命,打滑,變剛度振動(dòng),表面波紋度
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上傳時(shí)間:2024-03-01
頁數(shù): 167
大小: 2.12(MB)
子文件數(shù):
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簡介:國內(nèi)圖書分類號U5268國際圖書分類號P208西南交通大學(xué)研究生學(xué)位論文密級公開年級三Q二Q級姓名王明出申請學(xué)位級別亟專業(yè)太絲邇』量堂皇測量王猩指導(dǎo)老師壺垡教援二零一三年六月二十日西南交通大學(xué)學(xué)位論文版權(quán)使用授權(quán)書本學(xué)位論文作者完全了解學(xué)校有關(guān)保留、使用學(xué)位論文的規(guī)定,同意學(xué)校保留并向國家有關(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)西南交通大學(xué)可以將本論文的全部或部分內(nèi)容編入有關(guān)數(shù)據(jù)庫進(jìn)行檢索,可以采用影印、縮印或掃描等復(fù)印手段保存和匯編本學(xué)位論文。本學(xué)位論文屬于1保密口,在年解密后適用本授權(quán)書;2不保密∥使用本授權(quán)書。請?jiān)谝陨戏娇騼?nèi)打“√”學(xué)位論文作者簽名互明山日期糾1CL指導(dǎo)老師簽名日期邳”
下載積分: 5 賞幣
上傳時(shí)間:2024-03-01
頁數(shù): 76
大小: 17.73(MB)
子文件數(shù):
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簡介:中圖分類號V21論文編號102870713S065學(xué)科分類號082304碩士學(xué)位論文航空發(fā)動(dòng)機(jī)氣路故障模擬試驗(yàn)臺及靜電監(jiān)測技術(shù)研究研究生姓名余有鋒學(xué)科、專業(yè)載運(yùn)工具運(yùn)用工程研究方向系統(tǒng)可靠性指導(dǎo)教師左洪福教授南京航空航天大學(xué)研究生院民航學(xué)院二〇一三年三月NANJINGUNIVERSITYOFAERONAUTICSASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFCIVILAVIATIONAEROENGINEGASPATHFAULTSIMULATIONTESTDESKELECTROSTATICMONITINGTECHNOLOGYRESEARCHATHESISINVEHICLEOPERATIONENGINEERINGBYYUYOUFENGADVISEDBYPROFESSZUOHONGFUSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFTHEDEGREEOFACADEMICMASTERMARCH,2013
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上傳時(shí)間:2024-03-01
頁數(shù): 75
大?。?2.72(MB)
子文件數(shù):
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簡介:1■L一分類號UDC密級公玨學(xué)位論文題目基于聲波傳感器的航空發(fā)動(dòng)機(jī)燃燒室出口溫度分布測量研究研究生姓名王交峰學(xué)科專業(yè)名稱計(jì)算機(jī)應(yīng)用技術(shù)研究方向計(jì)算機(jī)檢測與控制論文類型應(yīng)用研究申請學(xué)位碩士指導(dǎo)教師姓名田豐指導(dǎo)教師職稱教授指導(dǎo)教師單位沈陽航空工業(yè)學(xué)院論文提交日期2009年02月20日論文答辯日期2009年03月07日沈陽航空工業(yè)學(xué)院2009年02月●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)立完成的。除文中已經(jīng)注明引州的內(nèi)容外,本論文不包含其他個(gè)人或集體已經(jīng)發(fā)表或撰寫過的作品或成果,194包含本人為獲得其他學(xué)位而使用過的成果。對本文研究做出重要貢獻(xiàn)的個(gè)人或集體均已在論文中進(jìn)行了說明并表示謝意。本聲明的法律后果由本人承擔(dān)。論文作者簽名卻印疊顫緩只狷2JO日
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上傳時(shí)間:2024-03-01
頁數(shù): 59
大?。?5.15(MB)
子文件數(shù):
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簡介:南京航空航天大學(xué)碩士學(xué)位論文航空發(fā)動(dòng)機(jī)分布式仿真研究姓名李濤申請學(xué)位級別碩士專業(yè)航空宇航推進(jìn)理論與工程指導(dǎo)教師黃金泉20051201航空發(fā)動(dòng)機(jī)分布式仿真研究IIABSTRACTDISTRIBUTEDSIMULATIONCANSAVETIMEANDMONEYINDESIGNANDDEVELOPMENTOFENGINE,PLAYINGAVERYIMPORTANTROLEINEACHPHASEOFAEROENGINEDEVELOPMENTINTHISTHESISTHEDISTRIBUTEDSIMULATIONENVIRONMENTISINVESTIGATEDWHICHPROVIDESCAPABILITIESOFCOMPONENTINTEGRATION,VARIABLECOMPLEXITYANALYSISANDMULTIDISCIPLINARYCOUPLINGANDITPRESENTSANEXCELLENTPLATFORMANDSOLUTIONACCOUNTINGFORTHISGOALAEROENGINEDISTRIBUTEDSIMULATIONSYSTEMSBASEDONBOTHSERIALCOMPONENTSLEVELANDPARALLELFULLENGINESLEVELAREDEVELOPEDACOMPONENTLEVELAEROTHERMODYMAMICMODELOFATURBOFANAEROENGINEISCREATEDINTHISTHESISUSINGOOTECHNOLOGYASANOPENSOURCEMIDDLEWAREACE/TAOWHICHCOMPLIESWITHCORBASTANDARDISUSEDASCOMMUNICATIONINFRASTRUCTURE,MODEL’STASKISDECOMPOUNDEDTOCONSTITUTEANAEROENGINEDISTRIBUTEDSYSTEMBASEDONCOMPONENTLEVELACONCURRENTSIMULATIONINTERFACEFORFULLENGINEISDEFINED,ANDTHENSERVERANDCLIENTPROGRAMSAREDEVELOPEDTHROUGHCOCODINGTHESKELETONANDSTUBWHICHCOMEFROMCOMPILINGPREDEFINEDIDLFILE,ACCORDINGTORESOLVINGTHENONLINEAREQUATIONSGROUPOFCONCURRENTDISTRIBUTEDMODELTHEGUIISDESIGNEDBASEDONMFCSIMULATIONTESTSINDICATETHATITISEASYTOUSE,MAINTAINANDEXTENDANDALSOCANIMPROVESTHEPERFORMANCEOFCOMPLEXSIMULATIONTASKREMARKABLYKEYWORDSAEROENGINEMODELING,DISTRIBUTEDSIMULATION,CORBA,ACE/TAO,OOTECHNIQUE,UML
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上傳時(shí)間:2024-03-01
頁數(shù): 70
大小: 0.69(MB)
子文件數(shù):
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簡介:中圖分類號V2337論文編號102870213S008學(xué)科分類號082502碩士學(xué)位論文航空動(dòng)力裝置建模與過渡態(tài)控制規(guī)律研究研究生姓名倪斌斌學(xué)科、專業(yè)航空宇航推進(jìn)理論與工程研究方向推進(jìn)系統(tǒng)建模與仿真指導(dǎo)教師黃向華教授南京航空航天大學(xué)研究生院能源與動(dòng)力學(xué)院二О一三年三月NANJINGUNIVERSITYOFAERONAUTICSASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFENERGYPOWERENGINEERINGRESEARCHONAIRCRAFTPOWERPLANTMODELDESIGNTRANSITIONCONTROLLAWATHESISINAEROSPACEPROPULSIONTHEYENGINEERINGBYNIBINBINADVISEDBYPROFHUANGXIANGHUASUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFTHEDEGREEOFMASTEROFENGINEERINGMARCH2013
下載積分: 5 賞幣
上傳時(shí)間:2024-03-01
頁數(shù): 80
大小: 3.86(MB)
子文件數(shù):
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簡介:學(xué)校代碼10699分類號記605密級學(xué)號01610G573餓再辦王歹喪蟲嘻’\奎籮筘;少N口RTHWEGTERN尸口LYTEC二NICALUNIVERS■Y碩士學(xué)位論文題目專業(yè)學(xué)位研究生航空產(chǎn)品的工藝裝備作者鄭洼指導(dǎo)教師王位壹、楊國榮申請學(xué)位日期2QQ魚璽旦西北工業(yè)大學(xué)碩士學(xué)位論文璐TRCTABSTRACTAPRODUCTCOREMANUFACTURINGENTERPRISENOWSTARTSTOUSEINCREASINGLYPⅢPRODUCTLIFECYCLEMANAGEMENTMANAGEMENTTECHNOLOGYINORDERTOMANAGEALLOFTHEELEMENTSTHROUGHOUTTHEPRODUCTLIFECYCLETHEAPPLICATIONOFPLMTECHNOLOGYWILLENHANCECOMPETITIVEEDGEOFTHEMANUFACTURINGENTERPRISE,PROMOTEINNOVATIVECAPABILITIESOFPRODUCTSFABRICATIONANDMAKEGREATPROFITABILITYFORTHEENTERPRISETHROUGHANALYZINGTHEFEATURESOFTOOLINGDESIGNANDFABRICATIONASWELLASINTEGRATINGTOOLINGDATAMANAGEMENT,THISPAPERHASANEXHAUSTIVESTUDYONHOWTOMANAGEWHOLELIFECYCLEOFTHETOOLINGPRODUCTSTBOMDEFINITIONISRAISEDWITHREGARDTOTHECORETOOLINGPRODUCTDATAMANAGEMENTREQUIREMENTSOFTHETOOLINGWHOLELIFECYCLEMANAGEMENTDURINGDESIGNANDFABRICATIONPROCESSOFTHETOOLINGPRODUCTS,TBOMPLAYSANIMPORTANTROLEASCOREDATAANDSERVICESASINFORMATIONBRIDGEBETWEENPRODUCTDESIGNANDFABRICATIONPHASEITESTABLISHESTBOMBASEDSINGLEDATASOURCEOFTOOLINGPRODUCT,COVERSTHERULESFORTOOLINGDETAILPARTSANDASSEMBLIESNUMBERSDURINGTOOLINGDESIGNANDSPECIFIESTOOLING3DMODELTHETOOLINGDESIGNWORKFLOWSANALYZEDOPTIMISTICALLYONTHEBASISOFSSPDBYWAYOFSECONDDEVELOPMENTOFENOVIALCASYSTEM,THETBOMBASEDTOOLINGPRODUCTSSPDSYSTEMISPRELIMINARILYCREATEDWHICHLAYSASOLIDFOUNDATIONFORREALIZINGTOOLINGPRODUCTPLMSYSTEMEVENTUALLYESTABLISHMENTOFATOOLINGPRODUCTSTRUCTURETREEANDDEFINITIONOFITSEACHLEVELPROPERTYALLOWSAUTOMATICGENERATIONOFTBOMANDOTHERSTATEMENTSTHESECONDDEVELOPMENTOFLCANAVIGATORSYSTEMCOMESUPWITHWORKFLOWMANAGEMENTREQUIREMENTSFORTOOLINGDESIGNANDESTABLISHESANDOPTIMIZESRELEASEWORKFLOWFROMTOOLINGDESIGNTOTOOLINGDATATHROUGHTHEPAPERSTUDY,THESINGLEDATASOURCEOFTOOLINGPRODUCTCOMESINTOBEINGANDWILLPROVIDEELEMENTARYDATAFORCAPPANDTOOLINGERPWHILEBEINGCONSIDEREDASTHECOREOFTOOLINGWHOLELIFECYCLEMANAGEMENTKEYWORDSTHEWHOLELIFECYCLE,TBOM,SINGLESOURCEOFPRODUCTDATAWORKFLOWMANAGEMENTI卜一
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上傳時(shí)間:2024-03-01
頁數(shù): 58
大小: 1.76(MB)
子文件數(shù):
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簡介:西北工業(yè)大學(xué)碩士學(xué)位論文學(xué)位研究生作者呈駿學(xué)科專業(yè)導(dǎo)航、制導(dǎo)與控制指導(dǎo)教師臼盔ABSTRACTAERODIGITALCAMERAISTHESUBSTITNTEDPRODUCTIONOFAEROFILMCAMERAINTHEAIRITSCREEILSREALSEENASOFGROUNDOBJECTSUSINGHIGHRESOLVINGCAPABILITYLARGESURFACEARRAYCCDCOMPONENTSATTHESALTLETIME,SCOUTPICTURESCANBESTOREDINTHECAMERADIRECTLYORBETRANSLATETOGROUNDCONTROLCENTERSOROTHERPLANESTHROUGHDIGITALTMNSMITEDSYSTEMCOMPAREDWITHAEROFILMCAMERAIT’SPROMINENTCHARACTERSAREGOODREALTIMECAPABILITYSMALLVOLUMEANDCONVENIENTFORDIGITALIMAGEDISPOSALLATERATPRESENT,CCDISONEOFTHEMOSTWIDELYUSEDOPTELECTRICDETECTIVEDEVICE,THEIMAGEACQUIRINGSYSTEMBASEDONCCDISALSOWIDELYAPPLIEDINMANYFIELDSSUCHASMILITARYAIRCRAFT,MEDICINE,CHEMENGINEERINGCCD’SWITHMEGAPIXELSAREPOPULARONTHEMARKET,THEIMAGEACQUISITIONANDPROCESSINGSYSTEMBASEDONTENMEGACCDISSTILLONTHESTAGEOFRESEARCHANDDEVELOPMENTATTHELABASTHEPIVOTALSUBASSEMBLYOFAVIATIONDIGITALCAMERATHEDRIVERSYSTEMBASEDONCCDAFFECTSTHEIMAGINGQUALITYOFAVIATIONDIGITALCANLELADIRECTLYANDTHESTATICPREVENTIONPROBLEMINAPPLICATIONAFFECTSTHESAFETYOFCCDCOMPONENTFORTHESAKEOFTHESEPROBLEMS,ACCD’SCIRUITOFOUTSIDEDESIGNISINTRODUCEDINTHISTHESISCCD’SCHIPSOFOUTSIDEISUSEDINTHISDESIGN,INCLUDINGTDA9991HL、SAA8103、AD9824、C8051F330MOREOVERSOMEPROBLEMSNEEDTOBECONSIDEREDDURINGTHEDESIGNOFLARGERESOLU虹ONCCDIMAGESENSORTWOCOREOFPIXELSAREALSODISCUSSEDINDETAILINTHISARTICLETHECIRCUITDESIGNHASSIMPLECONFIGURATIONRELIABILITYANDHIGHINTEGRATIONTHEREALIZATIONOFHIGHSPEEDDIGITALIMAGESTORAGESYSTEMHSDISSREFERTOBUS,MEMORYMEDIUM,ARRAYPROTOCOL,DEVELOPINGSOFTWAREANDHARDWAREANDOTHERPIVOTALTECHNOLOGIESINTHISRESEARCH,BASEDONSCSIBUSANDFAST40BOTTOMPROTOCOL,THROUGHBOTTOMDESIGNSHSDISSISDESIGNEDBYHARDWARETECHNOLOGYANDPUTFORWARDPRACTICALDESIGNSCHEMEKEYWORDSAERODIGITALCAMERA;LARGERESOLUTIONCCD;APPROPRIATIVECHIPS;SCSIBUSⅡ
下載積分: 5 賞幣
上傳時(shí)間:2024-03-01
頁數(shù): 59
大?。?1.5(MB)
子文件數(shù):
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簡介:西北工業(yè)大學(xué)碩士學(xué)位論文基于DSP的航空電子通信系統(tǒng)研究姓名康涌泉申請學(xué)位級別碩士專業(yè)交通運(yùn)輸規(guī)劃與管理指導(dǎo)教師史忠科20050101西J匕不業(yè)人學(xué)碩卜論文ABSTRACTABSTRACTHIGHSPEEDANDRELIABLETECHNOLOGYOFDATACOMMUNICATIONISIMPORTANTTOTHESTUDYOFAVIONICSTOTALICATIONSYSTEMINTHISPAPERAUTHORAIMATTHEDATABUSCOMMUNICATIONSYSTEMREQUESTSOFCOMPATIBILITYCOMMUNICATIONSPEEDRELIABILITYANTIJAMMINGANDSTUDYTHEAVIONICSCOMMUNICATIONSYSTEMINTHISPAPERANAVIONICSCOMMUNICATIONSYSTEMBASEDONDSPISDESIGNEDBYTHEMEANSOFMODULARIZATIONCOMPUTERINTERFACETECHNOLOGYDSPTECHNOLOGYINTELLIGENTCORRECTIONANDANTI一AMMINGTECHNOLOGYARINC429BUSANDLONWORKSBUSTECHNOLOGYAREUSEDTOREALIZETHESYSTEMTHISSYSTEMHASTHEGOODCOMPATIBILITYWITHDATAFORMATOFMULTIFORMDATABUSESSUCHASARINC429BUSLONWORKSBUSANDSOONTHEHARDWAREANDSOFTWAREDESIGNOFSYSTEMAREDISCUSSEDINDETAILTHEREALIZATIONOFCRCALGORITHMINSOFTWAREWHICHACHIEVETHEFUNCTIONOFINTELLIGENTCORRECTIONISGIVENTHEANTI一AMMINGDESIGNISREALIZEDONHARDWAREANDSOFTWARESEVERALEXPERIMENTSHAVEBEENANALYZEDTOVERIFYTHEAVAILABILITYOFTHESYSTEMPRESENTEDINTHISPAPERFINALLYTHEMAINWORKOFTHEPAPERISSUMMARIZEDANDSUGGESTIONSAREGIVENFORFUTURESTUDYKEYWORDSAVIONICSCOMMUNICATIONSYSTEMLONWORKSBUSINTELLIGENTDSPARINC429BUSCRECTION
下載積分: 5 賞幣
上傳時(shí)間:2024-03-01
頁數(shù): 127
大小: 4.07(MB)
子文件數(shù):
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簡介:中圖分類號V233.7學(xué)科分類號085232論文編號102870213一SZ013航空發(fā)動(dòng)機(jī)傳感器故障診斷、信號重構(gòu)的理論與試驗(yàn)研究研究生姓名專業(yè)類別專業(yè)領(lǐng)域指導(dǎo)教師趙成偉工程碩士航空工程葉志鋒教授南京航空航天大學(xué)研究生院能源與動(dòng)力學(xué)院二0一二年十二月承諾書本人聲明所呈交的碩士學(xué)位論文是本人在導(dǎo)師指導(dǎo)下進(jìn)行的研究工作及取得的研究成果。除了文中特另TLDH以標(biāo)注和致謝的地方外,論文中不包含其他人已經(jīng)發(fā)表或撰寫過的研究成果,也不包含為獲得南京航空航天大學(xué)或其他教育機(jī)構(gòu)的學(xué)位或證書而使用過的材料。本人授權(quán)南京航空航天大學(xué)可以將學(xué)位論文的全部或部分內(nèi)容編入有關(guān)數(shù)據(jù)庫進(jìn)行檢索,可以采用影印、縮印或掃描等復(fù)制手段保存、匯編學(xué)位論文。保密的學(xué)位論文在解密后適用本承諾書作者簽名皇監(jiān)日期墊12Z
下載積分: 5 賞幣
上傳時(shí)間:2024-03-01
頁數(shù): 67
大?。?7.97(MB)
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簡介:南京航空航天大學(xué)碩士學(xué)位論文航空發(fā)動(dòng)機(jī)非線性參數(shù)估計(jì)方法研究姓名翟高蘭申請學(xué)位級別碩士專業(yè)航空宇航科學(xué)與技術(shù)(系統(tǒng)仿真與控制)指導(dǎo)教師孫健國20080101航空發(fā)動(dòng)機(jī)非線性參數(shù)估計(jì)方法研究IIABSTRACTDIRECTTHRUSTCONTROLBECOMESANIMPTANTRESEARCHPROJECTINAEROENGINECONTROLFIELDBECAUSEITCANREDUCETHEDESIGNMARGINCANEXCAVATEAEROENGINE’SPERFMANCEPOTENTIALTHISMETHODNEEDSINFMATIONABOUTTHRUSTSTALLMARGINPROVIDESIMPTANTINFMATIONFAIRCRAFT’SSAFEFLYBUTTHEYBOTHCAN’TBEDIRECTLYMEASUREDDURINGFLIGHTTHISPAPERSTUDIEDTWOMETHODSINDERTOFINDTHEBESTEVALUATIONOFTHEMONEISTODESIGNACONSTANTGAINEXTENDKALMANFILTERCGEKFTHECGEKFISDEVELOPEDBYCOMBININGANONBOARDENGINEMODELASINGLEKALMANGAINMATRIXITCANESTIMATEAEROENGINE’SPERFMANCEPARAMETERSINDIRECTLYTHROUGHESTIMATINGTHEEFFICIENCIESFLOWCAPACITIESHEALTHPARAMETERSOFIT’SCOMPONENTSONLYASUBSETOFHEALTHPARAMETERSCANBEESTIMATEDBECAUSETHENUMBEROFAVAILABLESENSSINGENERALISLESSTHANTHENUMBEROFHEALTHPARAMETERSALSOBECAUSEOFTHECONVERGECONDITIONOFKALMANFILTERTECHNOLOGYTHEREFETHOSEESTIMATEDHEALTHPARAMETERSNOTONLYREPRESENTTHEMSELVESBUTALSOTHECHANGEOFOTHERHEALTHPARAMETERSTHEYBECOMETUNINGPARAMETERSTOMAKETHEONBOARDENGINEMODELADAPTIVETOTHEREALENGINE’SPERFMANCEVARIATIONSDUETOTHEDEGRADATIONANOMALIESPERFMANCEOFTHECGEKFISEVALUATEDINMANYSIMULATIONCONDITIONSTHESIMULATIONRESULTSSHOWTHATTHECGEKFISABLETOESTIMATETHEPARAMETERSWITHHIGHACCURACYTHEOTHERMETHODUSESNONLINEAREQUATIONSWHICHINCLUDEHEALTHPARAMETERSASTHEWAYTOESTIMATEPERFMANCEPARAMETERSACCDINGTOTHENUMBEROFTHEEQUATIONSHEALTHPARAMETERSEDTHEREARETHREEDIFFERENTWAYSINWHICHNONLINEAROPTIMIZINGISTHEMOSTIMPTANTTOSOLVEEQUATIONSTHESIMULATIONRESULTSSHOWTHATTHEYARESUITABLEKEYWDSAEROENGINEKALMANFILTERTUNINGPARAMETERSNONLINEAREQUATIONSNONLINEAROPTIMIZING
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上傳時(shí)間:2024-03-01
頁數(shù): 78
大?。?0.78(MB)
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簡介:西北工業(yè)大學(xué)碩士學(xué)位論文航空電源故障特征提取與故障診斷研究姓名黃根全申請學(xué)位級別碩士專業(yè)控制理論與控制工程指導(dǎo)教師張涇周20050301西北工業(yè)大學(xué)碩士學(xué)位論文AIRCRAFTELECTRICPOWERSOURCESYSTEMAEPSSISANIMPORTANTEQUIPMENTTRANSFORMINGTHEENGINEENERGYTOELECTRICENERGYFORALLELECTROEQUIPMENTSINAIRPLANEITSRIGHTWORKINGSTATEISAKEYTOENSURENORMALANDSECURERIGHTOFAIRPLANECONDITIONDETECTIONANDFAULTDIAGNOSISISAMAINRESEARCHINFIELDOFAIRCRAFTELECTRICPOWERSOURCESYSTEMAIRCRAFTELECTRICPOWERSOURCEISUSUALLYCONSTITUTEDBYTHREEGRADESOFGENERATORBUTITISDIFFICULTTOBUILDFAULTMODELFORITSCOMPLEXITYSTRUCTUREATPRESENTEXAMINEANDREPAIRONTHEGROUNDDEPENDSONSOMETRADITIONALINSTRUMENTSANDROUTINEEXAMINEWHOSEDISADVANTAGESAREFEWINSPECTINGITEMSANDLOWEFICIENCYTHISOFLINETESTINGMETHODCANNOTEXACTLYGETIMPORTANTSTATESANDPARAMETERSOFFAULTSINTHISPAPERACONDITIONDETECTIONANDFAULTDIAGNOSISSYSTEMSIMULATING“ONLINE“ONTHEGROUNDOFTHEAIRCRAFTELECTRICPOWERSOURCESYSTEMISDESIGNEDWHICHBASEDONMULTISENSORINFORMATIONFUSIONTECHNIQUEANALYZEDTHREEKINDSOFFAMILIARELECTRICFAULTSOFAIRCRAFTELECTRICPOWERSOURCEGENERALINSPECTINGITEMSARECONFIRMEDFORDIFFERENTDATAOFMULTISENSORDIFERENTSIGNALPROCESSINGMETHODSEXTRACTFAULTFEATURESANDIMPROVESNRTHEFOUNDATIONOFFAULTFEATUREDATABASEPROVIDESAGOODBASEFORFAULTDIAGNOSISANDCLASSIFYINGEVIDENCEREASONINGISUSEDINFAULTDIAGNOSISANDCLASSIFYINGOFTHEAIRCRAFTELECTRICPOWERSOURCESYSTEMTHEORYOFEVIDENCEANDDEMPSTERSRULEAREINTRODUCEDANDTHEMETHODGETTINGPROBABILITYEVALUATEISSTUDIEDTHERESULTSOFTHESIMULATIONSSHOWTHEEFECTIVENESSOFEVIDENCEREASONINGMETHODANDTHECONDITIONDETECTIONANDFAULTDIAGNOSISSYSTEMONTHEGROUNDWORDSAIRCRAFTELECTRICPOWERSOURCEFEATUREEXTRACTIONFAULTDIAGNOSISINFORMATIONFUSIONEVIDENCEREASONING11
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上傳時(shí)間:2024-03-01
頁數(shù): 120
大?。?4(MB)
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簡介:中圖分類號V23191學(xué)科分類號082502論文編號1028702100021碩士學(xué)位論文航空發(fā)動(dòng)機(jī)輪盤標(biāo)準(zhǔn)載荷譜編制方法研究研究生姓名學(xué)科、專業(yè)研究方向指導(dǎo)教師周楠航空宇航推進(jìn)理論與工程結(jié)構(gòu)強(qiáng)度與振動(dòng)宋迎東教授南京航空航天大學(xué)研究生院能源與動(dòng)力學(xué)院二。一。年三月K◆●NANJINGUNIVERSITYOFAERONAUTICSANDASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFENERGYANDPOWERENGINEERINGRESEARCHONTHEMETHODOFASTANDARDIZEDFATIGUETESTLOADINGSEQUENCEFORAIRCRAFTCOLDSECTIONENGINEDISCSATHESISINAEROSPACEPROPULSIONTHEORYANDENGINEERINGBYNAMEZHOUNANADVISEDBYPROFSONGYINGDONGSUBMITTEDINPATTIALFULFILLMENTOFTHEREQUIREMENTSFORTHEDEGREEOFMASTEROFENGINEERINGMARCH,2010
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上傳時(shí)間:2024-03-01
頁數(shù): 80
大小: 2.44(MB)
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簡介:西北工業(yè)大學(xué)碩士學(xué)位論文噪聲分析系統(tǒng)在航空發(fā)動(dòng)機(jī)試車臺的應(yīng)用研究姓名黃晶晶申請學(xué)位級別碩士專業(yè)環(huán)境工程環(huán)境信息處理指導(dǎo)教師雷勇20060301萬P≯士摯碩士學(xué)位論文英文摘要RESEARCHOFNOISEANALYSISSYSTEMINAEROENGINETESTABSTFACTTHISPAPERPRESENTSASYSTEMEXPLOITINGWAYBASED0NDIGITALTECHNOLOGYANDVIRTUALDISPLAKWHICHCANBEAPPLIEDINENGINEERINGFIELDASYSTEMWASDESIGNEDTOANALYZINGNOISESIGNALUTILIZINGNISOFTWARETOOLINVISUALC十ENVIRONMENTTHISSYSTEMSUPPLIESAIGST,EXACTANAVISUALWAY,WHICHCANCOLLECTANDANALYZESIGNALITREALIZESALOTOFFMLCTIONSSUCHASDECIBEDMETERCALIBRATIONANDDIMENSIONCONVERSION,THECOLLECTIONANDSAVEDOFNOISESIGNAL,WINDOWFUNCTIONS,F(xiàn)ILTERS,AVERAGETIMES,POWERSPECTRUM,CEPSTRUM,THIRDOCTAVEBAND,ANDSOONTHISSYSTEMWASUSEDTOCOLLECTEDANDANALYZEDNOISESIGNALOFTURBOJET一7,TURBOPROP一6,TURBOFANJETTTISSTRESSEDINTHISPAPERTHATTHEANALYSISMETHODSOFPOWERSPECTRUMANDTHIRDOCTAVEBAND,ACCORDINGTOTHEANALYSISONNOISESIGNALOFABOVEAEROENGINESOPERATIONSTATUSMESSAGESOFAEROENGINESWEREAVAILABLE,MEASURINGANDANALYZINGTHENOISEOFINSIDEANDOUTSIDEOFAEROENGINETEST,WHICHPROVIDESTHEFOUNDATIONOFTHEAEMENGINETESTDESIGN,EVALUATETHENOISEENVIRONMENTINAEROCNGINETEST,ITINDICATESTHATNOISEMEASUREMENTISNOTONLYTHEREQUIREMENTOFREDUCINGENGINENOISEBUTALSOANASSISTANTINSTRUMENTOFENGINECONFIGURATIONANDFAILUREDIAGNOSISKEDUORDSNOISE,DIGITALSIGNALPROCESSING,POWERSPECTRUMFL矗RDOCTAVEBAND,AEMENGINE1J
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上傳時(shí)間:2024-03-01
頁數(shù): 66
大?。?2.39(MB)
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