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    • 簡(jiǎn)介:上海交通大學(xué)碩士學(xué)位論文典型航天產(chǎn)品電子束焊接變形預(yù)測(cè)與控制姓名吳飛申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)材料加工工程指導(dǎo)教師陸?zhàn)?0040101PREDICTIONCONTRALOFTHEDEFMATIONOFELECTRONBEAMWELDINGONTYPICLEAEROWKPIECESABSTRACTFIRSTLYSEVERALNUMERICALMETHODSOFPREDICTINGWELDINGDEFMATIONARECOMPAREDBASICTHEYPROPERTYAPPLICABILITYOFEACHNUMERICALMETHODAREDISCUSSEDTHEMECHANICSOFWELDINGDEFMATIONISALSODISCUSSEDINTHISPAPERTHETHERMOELASTICPLASTICFEMISPAIDMEATTENTIONTOINTHETHESISTAKINGINTOACCOUNTTHEGEOMETRICALDIMENSIONSMATERIALSPROPERTIESHEATDISTRIBUTIONTHEMESHASERIESOFTHINCYLINDERISCREATEDFELECTRONBEAMWELDINGEBWAFTERCOMPARISONRULESAREGIVENOUTTODETERMINEEACHFACTTHEEFFECTOFTHELATENTHEATOFFUSIONMOLTENMETALISRESEARCHEDINTHISPAPERTHEAPPLICABILITYOFTHEINHERENTSTRAINMETHODISDISCUSSEDFEBWONTHINCYLINDERSTHEVALUEOFKCM3JINTHEEQUATIONOFWXKQVTOGETHERWITHTHEVALUEOFCM3JINTHEEQUATIONOFWYQVAREGIVENFEBWCOMPUTATIONFCYLINDERSOFDIFFERENTMATERIALSDIFFERENTSIZESSHOWSTHATISACONSTANTVALUEFEBWONTHINCYLINDERKISAFFECTEDBYTHERADIUSOFCYLINDERSBASEDONTHERMOELASTICPLASTICFEMTHEPREDEFMATIONPROCESSISSIMULATEDAMETHODISGIVENTODETERMINEPREDEFMATIONVALUESOMEADVICESAREGIVENTOIMPROVECURRENTPREDEFMATIONPROCESSATLASTTHECOOLINGEFFECTOFTHEFIXERTHEEFFECTOFSKIPWELDINGAREEVALUATEDBYNUMERICALANALYSIS
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    • 簡(jiǎn)介:哈爾濱工程大學(xué)碩士學(xué)位論文小型航空發(fā)動(dòng)機(jī)傳感器容錯(cuò)控制技術(shù)研究姓名劉漢斌申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)控制工程指導(dǎo)教師蘭海;何保成20111104哈爾濱工程大學(xué)碩士學(xué)位論文II
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 70
      2人已閱讀
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    • 簡(jiǎn)介:航天遙測(cè)數(shù)據(jù)實(shí)時(shí)存儲(chǔ)及可視化系統(tǒng)設(shè)計(jì)與實(shí)現(xiàn)重慶大學(xué)碩士學(xué)位論文(專(zhuān)業(yè)學(xué)位)學(xué)生姓名邱翊峰指導(dǎo)教師柴毅教授兼職導(dǎo)師王剛高工學(xué)位類(lèi)別工程碩士(控制工程)重慶大學(xué)自動(dòng)化學(xué)院二O一七年四月DESIGNIMPLEMENTATIONOFREALTIMESTAGEVISUALIZATIONSYSTEMFAERIALTELEMETRYDATAATHESISSUBMITTEDTOCHONGQINGUNIVERSITYINPARTIALFULFILLMENTOFTHEREQUIREMENTFTHEPROFESSIONALDEGREEBYQIUYIFENGSUPERVISEDBYPROFCHAIYIPLURALISTICSUPERVISEDBYSENIENGWANGGANGSPECIALTYMECONTROLENGINEERINGCOLLEGEOFAUTOMATIONOFCHONGQINGUNIVERSITYCHONGQINGCHINAAPRIL2017
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 80
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      ( 4 星級(jí))
    • 簡(jiǎn)介:中南工業(yè)大學(xué)博士后學(xué)位論文航空剎車(chē)用CC復(fù)合材料氧化行為抗氧化涂層的研究姓名易茂中申請(qǐng)學(xué)位級(jí)別博士后專(zhuān)業(yè)材料學(xué)指導(dǎo)教師黃伯云19990701出爐。其最佳抗氧化效果為9000C、2小時(shí)靜態(tài)氧化失重率為015%,9000C、4小時(shí)氧化失重率為113%。5未固化處理的涂層試樣900。C靜態(tài)氧化動(dòng)力學(xué)曲線(xiàn)呈二段直線(xiàn)型,而固化處理的涂層試樣在900。C氧化的動(dòng)力學(xué)曲線(xiàn)具有拋物線(xiàn)形狀,不論涂層固化與否在較低溫度的700。C靜態(tài)氧化動(dòng)力學(xué)曲線(xiàn)基本上呈直線(xiàn)型。6帶涂層的C/C復(fù)合材料氧化過(guò)程是一個(gè)復(fù)雜的氣固反應(yīng)過(guò)程,包括I氧氣向內(nèi)的擴(kuò)散;2氧與涂層中的耗氧組元反應(yīng)生成新的陶瓷組元;3進(jìn)入涂層與基體材料界面的氧與材料發(fā)生氧化反應(yīng)形成氣體;4反應(yīng)氣體向外擴(kuò)散。關(guān)鍵詞C/C復(fù)合材料氧化抗氧化涂層飛機(jī)剎車(chē)盤(pán)
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 98
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    • 簡(jiǎn)介:中南大學(xué)碩士學(xué)位論文航空發(fā)動(dòng)機(jī)軸間密封CC復(fù)合材料的制備及摩擦磨損特性研究姓名彭春蘭申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)材料學(xué)指導(dǎo)教師易茂中20020101ABSTRACTTHESEALRINGISTHECRITICALPARTFBRTHESEALINGOFTHEMAINAXISOFAEROPLANEENGINEACCORDIⅡGTOTHEREQUIREMEⅡTOFAPPLYINGCONDITIONS,ITMUSTHAVEHIGHSTRENGTH,EXCELLENTOXIDATIONRESISTANCEANDLOWCOEFFICIENTOFFRICTIONANDWEARRATIOTHECARBONCARBOⅡCOMPOSITESWEREFABRICATEDANDTHEIRPROPERTIESWEREANALYZEDWHAT’SMORE,F(xiàn)RICTIONANDWEARPROPERTIESOFTWOTYPESOFMATERIALS,CARBONCARBONCOMPOSITEANDHIGHSTREⅡGTHGRAPHITEW血ICHWASSUPPOSEDTOBEUSEDASTHESEALRINGOFTHEMAINAXISOFAEROPLANEENGINE,WEREINVESTIGATEDACCORDIⅡGTOTHEREQUIREMENTOFAPPLYINGCONDITIONSANDPFOPERTIESOFTHESEAL“ⅡGOFTHEMAINAXISOFAEROPLANEENGINE,PREFBRMSWEREDESIGNEDINTOTHESUBSTRATETHATTHECARBONCLOTHANDFELTALTERNATELYWEREWINDEDAROUⅡDTHECYLIⅡDERAⅡDTHENNEEDLEDWITHCARBONFIBERINTHERADIALDIRECTIONANDTHEOTHER3一DWEAVIⅡGSUBSTRATETBREINFBRCETHEFIBREANDTHEMATRIXCONNECTING,PREFORMSWEREDENSIFIEDBYCVDFIRSTLYTHEPYROLYTICCARBOⅡWITHRL/SLSTRUCTUREORSLSTRUCTUREWASOBTAINEDAFTERTHATTHEMATERIALSWEREFURTHERDENSIFIEDWITHRESINANDHEATTREATEDAT2L00℃THESTRENGTH觚DWEARRESISTANCEWASIMPROVED,ANDTHERESINWOULDGUARANTEETHESEALINGEFFECTAFTERHEATTREATMENT,THEDEGREEOFGRAPHITIZATIONOFTHEMATERIALSWASABOUT30~50%,ANDTHEDEGREEOFGRAPHITIZATIONOFMATERIALL6拌WASAMOUNTT0471%THEHARDNESSOFTHE3DPREFBRMMATERIALWASCLOSEINTHERADIALANDCIRCUMAMBIENTDIRECTIONBUTTHEHARDNESSOFTHEOTHERPREFORMWASALMOSTANISOTROPICTHETHERMALCONDUCTIVITYWASALSOANISOTROPICTHECOEFFICIENTOFTHERMALEXP蚰SIONDECREASEDWITHTHETEMPERATUREINCREASEDWHEN400℃,ITWASATTHEBOTTOM,鋤DWHEⅡTO500℃,ITINCREASEDANDTHEMECHANICALPROPERTYOFCARBONCARBONCOMPOSITEWASPSEUDOPLASTICBYSTUDYINGFICTIOⅡANDWEAROFTHECARBONCARBONCOMPOSITEANDIT
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    • 簡(jiǎn)介:中圖分類(lèi)號(hào)V2337論文編號(hào)102870215S103學(xué)科分類(lèi)號(hào)082502碩士學(xué)位論文航空發(fā)動(dòng)機(jī)控制系統(tǒng)傳感器故障診斷與容錯(cuò)控制研究生姓名姜潔學(xué)科、專(zhuān)業(yè)航空宇航推進(jìn)理論與工程研究方向航空發(fā)動(dòng)機(jī)傳感器故障診斷指導(dǎo)教師李秋紅副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一五年三月NANJINGUNIVERSITYOFAERONAUTICSANDASTRONAUTICSTHEGRADUATESCHOOLCOLLEGEOFENERGYANDPOWERENGINEERINGRESEARCHONAEROENGINECONTROLSYSTEMSENSORFAULTDIAGNOSISANDFAULTTOLERANTCONTROLATHESISINAEROSPACEPROPULSIONTHEORYANDENGINEERINGBYJIANGJIEADVISEDBYASSOCIATEPROFESSORLIQIUHONGSUBMITTEDINPARTIALFULFILLMENTOFTHEREQUIREMENTSFORTHEDEGREEOFMASTEROFENGINEERINGMARCH,2015
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    • 簡(jiǎn)介:西北工業(yè)大學(xué)碩士學(xué)位論文某型航空螺旋離心泵性能計(jì)算研究姓名何海強(qiáng)申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)控制理論與控制工程指導(dǎo)教師郭迎清20040301ABSTRACTFUELPUMPANDLUBEPUMPUSEDINPRESENTAEROENGINEANDSPACEENGINEAREORIENTEDTOSMALLERVOLUME,BIGGERFLUXANDHIGHERPRESSURETHEYDIFFERSMUCHFROMTHETRADITIONALHYDRAULICELEMENTBOTHINMECHANICSANDINPRINCIPLETHEFRESHTHOUGHTANDCUTEMETHODUSEDINTHESEPUMPSMAKETHEMWORKBETTERANDCONTRIBUTEMORETOTHEOPERATIONOFTHERULESYSTEMTHUS,ITISOFMUCHINDISPENSABILITYTOFINDOUTTHENEWIDEASANDEXCLUSIVEMECHANICSSTRUCTUREANDPERFORMANCEOFASCREWCENTRIFUGALPUMPUSEDINAEROENGINEWASDISCUSSEDINTHISPAPERANDTHECALCULATIONMETHODOFTHEPUMP’SPERFORMANCEWASALSOGIVENOUTTHEPAPERBEGINSWITHTHEDISCUSSIONOFTHEOPERATINGPRINCIPLEANDFUNCTIONOFTHESCREWINDUCERSPECIALELEMENTOFTHEPUMP,ANDTHENGIVESTHEDEFINITIONANDRELATIONSHIPOFTHEPARAMETERSANDTHECURVEFUNCTIONOFTHEINDUCERASWELL,WHICHISOFGREATIMPORTANCETODATAANALYZINGANDPUMPMANUFACTURINGBYPRESENTINGTHESIMPLIFIEDFLOWMODEL,THEFLOWANDVELOCITYTRIANGLESWEREANALYZEDTNTHEPAPERTHEAUTHOREXCAVATEDTHEPERFORMANCE,CALCULATEDTHEVELOCITY,PRESSUREANDFLOWLOSSOFTHEWORMSHELL,THEOUTLETELEMENTOFTHEPUMPACCORDINGTOTHECOMMONMETHODOFTHEPERFORMANCECALCULATIONOFCENTRIFUGALPUMP,THEAUTHORCALCULATEDTHEHEADANDPOWEROFTHEPUMP,SHOWEDTHEWAYTOGETTHEPRESSUREOFTHEOUTLETANDTHEAUTHORALSOINDICATEDTHEIMPACTOFTHESTRUCTUREPARAMETERSANDTHUSGUIDEDTHEDESIGNOFTHEPUMPTHERESULTSSHOWTHATTHESCREWCENTRIFUGALPUMPISATYPEOFWELLWORKINGPUMPWITHGOODPERFORMANCE,ITHASHIGHERHEADANDEFFICIENCYWITHBETTERABILITYOFANTIEROSIONBOTHTHEPARAMETERSANDTHEWORKINGCONDITIONCANAFFECTTHEPUMP’SOPERATIONANDPERFORMANCEDIRECTLYITISAUSEFULWAYTOCHANGETHESEPARAMETERSTOMEETTHENEEDOFTHEENGINEERING【KEYWORDS】SCREWCENTRIFUGALPUMP;SCRE%VINDUCER;WORMSHELLPERFORMANCECALCULATION
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    • 簡(jiǎn)介:中國(guó)民用航空學(xué)院碩士學(xué)位論文BP網(wǎng)絡(luò)與航空發(fā)動(dòng)機(jī)模型在間隙對(duì)性能影響研究中的應(yīng)用姓名馬曉剛申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)航空宇航推進(jìn)理論與工程指導(dǎo)教師白杰李書(shū)明20040110中國(guó)民用航空學(xué)院碩士學(xué)位論文ABSTRACTTHISPAPEROPTIMIZEDANDANALYZEDTHEDATAOFASSEMBLYTOLERANCESINTEGRATEDWITHTHEFACTDURINGAEROENGINEMAINTENANCE,ANDASSEMBLEDAMODELTORESEARCHTHERELATIONSHIPBETWEENTHETOLERANCESOFKEYENGINECOMPONENTSINCLUDINGTIPCLEMANCESOFROTATINGCOMPONENTSANDENGINEPERFORMANCETHROUGHTHECOMBINEDUSEOFBPARTIIKIALNEURALNETWORKANDCONVENTIONALTHEORETICMODELOFAEROENGINEINTHERESULTOFTHISPAPER,SOMERULESAREGIVENTOOUTLINETHESERELATIONSHIPSTHATISVERYUSEFULTOCONTROLTHEASSEMBLYTOLERANCESANDACHIEVEHIGHLEVELSOFENGINEPERFORMANCEAFTERSERVICINGDATAOFASSEMBLYTOLERANCESDISCUSSEDINTHISPAPERARESTATICTOLERANCEBEFORETESTANDEMPHASIZEPARTICULARLYOILINVESTIGATINGTHERELATIONSHIPBETWEENCLEARANCESOFASSEMBLYBLADESANDTHEENGINEPERFORMANCEBESIDES,BPARTIFICIALNEURALNETWORKANDWORKINGCONDITIONEQUATIONOFTHEENGINEAREADOPTEDINTHISPAPERTOFORECASTTHEEFFECTOFTIPCLEARANCEONPARAMETERSOFENGINESUCHASEFFICIENCYOFPRESSURECOMPRESSOGEFFICIENCYOFTURBINE,THETEMPERATUREINTHEFRONTOFTURBINEANDEXHAUSTGASTEMPERATUREBECAUSEOFTHELIMITATIONOFTHEANALYTICALMETHODOFMATHEMATICS,THERELATIONSHIPOFTOLERANCERECORDEDDURINGMAINTAININGANDENGINEPERFORMANCEDESCRIBEDINTHISPAPERCORRESPONDSTOTHESPECIFICSERVICINGCONDITIONANDMODELBUTTHEMETHODCANAPPLYTODEALWITHOTHERENGINEMODELTHEDATAINTHISPAPERARECOLLECTEDFROMACIVILTURBINEFANENGINEWITHAFAN,TWOAXIALCOMPRESSORS,ANAXIALHIGHPRESSURETURBINEHPRLL,ANDANAXIALLOWPRESSURETURBINELPTCANREPRESENTCOMMONMODELTHROUGHANALYZINGINTHISPAPERWEVERIFIEDTHATTIPCLEARANCESAFFECTSENGINEPERFORMANCEANDOPERABILITYATTHESAMETIMESOMEOTHERTOLERANCESHAVEEFFECTSTOENGINEPERFORMANCESOMECONCLUSIONDRAWNINTHISRESEARCHCANOFFERREFERENCETELEVANTRESEARCHERFINALLY,ANAPPLICATIONPROGRAMPW4000ASSEMBLYTOLERANCESANDENGINEPERFORMANCEANALYSISSYSTEMWASDEVELOPEDINVCLANGUAGEANDODBCDATABASETHROTLGHANALYSISANDPREDICTIONEMPLOYEDTHISSYSTEMTHEVALIDITYOFTHERESEARCHAPPROACHESINTHISPAPERWASVERIFIEDKEYWORDSAEROENGINE,PERFORMANCE,TOLERANCE,BPANN
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 69
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    • 簡(jiǎn)介:合肥工業(yè)大學(xué)碩士學(xué)位論文航空軸承性能試驗(yàn)測(cè)試控制系統(tǒng)的研制姓名劉蘇亞申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)機(jī)械工程指導(dǎo)教師尹志強(qiáng)徐同申20040401THERESEARCHINGANDMANUFACTURINGOFCONTR0IIINGANDTESTSYSTEMFORAVIATIORBERINGTESTERABSTRACTTHEAVIATIONBEARING‘‘661701”ISDEVELOPEDASINTERVENINGBEARINGWHICHISALSOCALLEDONEWAYBEARINGOFAVIATIONENGINEFORTHE608RESEARCHINSTITUTEOFAVIATIONINDUSTRYBYLUOYANGBEARINGSCIENCEANDTECHNOLOGYCD.,LTD.THEPERFORMANCEOFTHEBEARINGISDIRECTLYASSOCIATEDWITHTHESTARTUP.THEREFOR,ITISVERYIMPORTANTTOTESTTHEONEWAYBEARING“66I701”。TWOELECTRICSPINDLESAREUSED,ONESIMULATESTHESTARTERMOTOR,THEOTHERSIMULATESENGINETODRIVEBEARING.INTHETEST,THESPEEDOFREVOLUTION,TEMPERATURE,OILSUPPLYPRESSUREANDOTHERPARAMETERAREMEASUREDBYTHEINDUSTRYCONTROLCOMPUTER。ATTHESAMETIME,ITDETAILEDDEMONSTRATEANDCARRYOUTTHEWAY,WHICHAPPLYHOUSINGELECTRICSPINDLESATGENERATIONSTATETOCARRYOUTHOUSINGTOQUELOADINGINTHEJOINTTESTINGANDINDIRECTLYESTIMATIONHOUSINGTORQUELOADINGBYTHEELECTROMAGNETISMTORQUEOFINNERTUBEELECTRICSPINDLES.THUS,THETECHNICALPROBLEMTHATTHEHIGHSPEEDSHAFTINGTORQUELOADINGDEVICEANDTORQUESENDERAREDIFFICULTTOINSTALLISSOLVEDANDITSAVESASETOFEXPENSIVEHIGHSPEEDSHAFTINGTORQUELOADINGANDMEASURINGDEVICE.THEOUTCOMEFILLTHEBLANKINTHEDOMESTICFIELDOFTORQUELOADINGFORHIGHSPEEDONEWAYBEARINGTEST.ANDITREACHESADVANCEDLEVELINOURCOUNTRY。THEPARAMETRICSELFADJUSTINGONLINEINTERPOLATIONFUZZYCONTROLISFORMEDBYTHEAPPLYINGPRACTICALINTERPOLATIONMETHODANDPARAMETRICSELFADJUSTINGMETHODTOROUTINEFUZZYCONTROLSYSTEMTHESYSTEMLOWERTHESTATICERRORANDAVOIDTHEFLUTTEROFROUTINEFUZZYCONTROLLER.THESIMULATIONRESULTSPROVETHATTHISSYSTEMHASRAPIDDYNAMICRESPONSESPEEDANDHIGHSTEADYSTATE,ASWELLASGOODFOLLOWINGCAPABILITYANDSTRONGROBUSTNESS.
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      頁(yè)數(shù): 64
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 130
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    • 簡(jiǎn)介:東南大學(xué)碩士學(xué)位論文加強(qiáng)政府航空安全管理對(duì)策研究姓名陳忠躍申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)公共管理指導(dǎo)教師袁久紅20110930ABSTRACTTITLETHESTRATEGYFORTHEGOVERNMENTTOSTRENGTHENAVIATIONSAFETYMANAGEMENTNAMECHENZHONGYUESUPERVISORYUANJIUHONGUNIVERSITYSEUSOUTHEASTUNIVERSITYALONG霄ITHTHERAPIDDEVELOPMENTOFCIVILAVIATIONINDUSTRYOFCHINA。THEDEMANDOFAIRTRANSPORTHASBEENDRAMATICALLYINCREASINGTHECONFLICTBETWEENTHERAPIDGROWTHOFTHEFLIGHTTRAFFICANDTHERELATIVELYWEAKSAFETYBASISISMORESERIOUSTHISPAPERFIRSTANALYZESTHEPRESENTSITUATION8NDCHARACTERISTICSOFTHECIVILAVIATIONSAFETYMANAGEMENTTHENFROMTHESTATISTICALANALYSISOFTHECRASHINTHEPASTTWODECADES,WEOBTAINTHEMAINMANAGEMENTFACTORSFORAVIATIONSAFETYBASEDONTHEABOVEMANAGEMENTFACTORS,霄EANALYZESTHEMAINSECURITYMANAGEMENTPROBLEMSINTHEAVIATIONINDUSTRYFROMTHEPLANNING,ORGANIZATIONCOORDINATIONANDCONTROLFUNCTIONSWEPROVETHATTHE90VER咖ENTNEEDENHANCETHEAVIATIONSAFETYMANAGEMENTFROMSCIENTIFICPLANNING。MACROCONTROL,INSTITUTIONALCHANGE,STRENGTHENINGPRODUCTIONSAFETYRESPONSIBILITY,STRENGTHENINGEMERGENCYMANAGEMENTANDSOONTHEGOVERNMENTISTHEMOSTIMPORTANTAVIATIONSAFETYREGULATORTHISARTICLEPROVIDESTHESTRATEGYFORTHEGOVERNMENTSTRENGTHENINGAVIATIONSECURITYMANAGEMENTTHESTUDYPROVIDESAGOODREFERENCEFORTHEGOVERNMENTTOENHANCETHEAVIATIONSAFETYMANAGEMENTKY的RD8GOVER珊ENT;CIVILAVIATION;SAFETY艙NAGEMENT№NAGEMENTSYSTEM
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 47
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    • 簡(jiǎn)介:西北工業(yè)大學(xué)碩士學(xué)位論文基于隨機(jī)PETRI網(wǎng)的航空電子綜合系統(tǒng)數(shù)據(jù)總線(xiàn)建模分析姓名耿修堂申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)系統(tǒng)工程指導(dǎo)教師吳勇20040301西北工業(yè)大學(xué)碩卜論文基于隨機(jī)PETRI網(wǎng)的航空電F綜合系統(tǒng)數(shù)據(jù)總線(xiàn)的建模分析ABSTRACTTHETHESISCONTENTISMODELLINGANDANALYSISOFINTEGRATEDAVIONICSSYSTEMDATABUSWITHSTOCHASTICPETRINETTHEPURPOSEISOPTIMIZINGBUSTRANSMISSIONSYSTEMBYTHEANALYSISOFINTEGRATEDAVIONICSSYSTEMDATABUSCAPABILITYPARAMETERUTILIZINGTIMEDPETRINETSTOCHASTICPETRINETMODELLINGTOOLANDCOMPUTERTOOLSIMULATINGANDANALYZINGINTEGRATEDAVIONICSSYSTEMDATABUSANDATTAININGSYSTEMTIMECAPABILITYPARAMETERARETHESTUDYINGMETHODOFTHETHESISASARESULTOFSTUDYINGWEGAINTHREESYSTEMTIMECAPABILITYPARAMETEROFMONOLAYERBUSFRAMEWORKANDTWODOUBLEBUSFRAMEWORKDATABUSUTILIZATIONLENGTHOFTHEDATAWAITINGQUEUEANDTIMEOFSYSTEMTIMEDBASINGONFIXEDBCCONTROLSEASONALREPERTOIRETIMEDPETRINETANDSTOCHASTICPETRINETWEALSOTAKETWOCONCLUSIONSBYFOREGOINGRESULTFIRSTOFALLTHESYSTEMBECOMESMOREANDMORECOMPLEXTHESYSTEMDATABUSUTILIZATIONCOPYRESULTTIMEOFSYSTEMTIMEDANDLENGTHOFTHENEWSWAITINGQUEUEBECOMEMOREANDMOREPRECISEBASINGONSTOCHASTICPETRINETATTHESAMETIMETHEMODELISVISUALVIVIDCONCISEANDCURRENTSECONDLYWHENITISTWODOUBLEBUSFRAMEWORKTHEUTILIZATIONOFDATABUSANDLENGTHOFTHEDATAWAITINGQUEUEWILLFALLQUICKLYKEYWORDSINTEGRATEDAVIONICSSYSTEMSTOCHASTICPETRINET1553BDATABUSTIMEDPETRINET
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      上傳時(shí)間:2024-03-01
      頁(yè)數(shù): 69
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    • 簡(jiǎn)介:西北工業(yè)大學(xué)碩士學(xué)位論文航空高壓直流稀土永磁無(wú)刷電機(jī)控制技術(shù)研究姓名梅彥平申請(qǐng)學(xué)位級(jí)別碩士專(zhuān)業(yè)電機(jī)與電器指導(dǎo)教師馬瑞卿20050301西北工業(yè)大學(xué)碩士學(xué)位論文ABSTRACTABSTRACTRESPONDTOTHEREQUIREMENTOFANAVIATIONDEPARTMENTTHESPEEDCONTROLTECHNIQUESANDTHERELATIVEAPPLIANCETECHNIQUESOFRAREEARTHPERMANENTMAGNETBRUSHLESSDCMOTORBLDCMWHICHWORKSFORTHENEWHIGHVOLTAGEPOWERSUPPLYSYSTEMOFPLANEISRESEARCHEDINTHISPAPERTHEPAPERMAINLYINCLUDESTHREEPARTSFIRSTBASEONTHECOMPREHENSIVEANALYSISANDSTUDYABOUTTHESTRUCTUREPRINCIPLESANDCONTROLRULESOFBLDCMOTORCONTROLSYSTEMITSCONTROLMETHODTHATUSEDFORHVDCSYSTEMISRESEARCHEDINORDERTEALIZETHEMOTORS“SOFTSTART“ANIDEALSTARTPROCESSIONASOFTWAREPROGRAMANDASTRATEGYOFSPEEDANDCURRENTDOUBLECLOSELOOPCONTROLSYSTEMTIMETHESPEEDAREINTRODUCEDTOLIMITITSSTARTCURRENTATTHESAMECLOSELOOPSYSTEMARESIMULATEDSECONDDEPENDONTHESTUDYOFTHEPRINCIPLESANDTECHNIQUESOFTHEMINIATUREHIGHFREQUENCYSINGLEENDEDFLYBACKSWITCHINGPOWERSUPPLYESPECIALLYTHEPRINCIPLESOFTHESINGLECONTROLCHIPOFSWITCHINGPOWERSUPPLYTOP224YANDTHECALCULATIONANDDESIGNOFHIGHFREQUENCYTRANSFORMER,ASWITCHINGPOWERSUPPLYWHOSECONTROLCHIPISTOP224YISDESIGNEDWHICHACCOMPLISHTHEPOWERTRANSFORMATIONFROM270VDCTO5VDCAND15VDCINTHEMEANINGTIMETHEPROBLEMOFEMCISRESEARCHEDANDSOMEMETHODSTOREDUCETHEINFLUENCESOFEMCAREPUTFORWARDLASTBASEONALLTHOSERESEARCHESABOVEACONTROLLERWHICHUSETHEMICROCONTROLLERCHIPAT89C51ISDESIGNEDITUSESTHESIGNALSTHATCOMEFROMTHEROTORPOSITIONSENSORTOGETTHEMOTORSSPEEDINDIRECTLYANDUSESSOFTWARETOACCOMPLISHTHESIGNALSOFPWMWAVEANDTHESTRATEGYOFSPEEDCLOSELOOPCONTROLTHESIMULATIONABOUTTHECONTROLTHEORYISVERIFIEDBYTHEEXPERIMENTTHISCONTROLLERGUARANTEESTHEMOTORWORKSIN4KINDSOFPATTERNSSAFELYANDTHEWORKSSTABILITYISENSUREDTHROUGHSEVERALKINDSOFANTIDISTURBANCETECHNIQUESTHEEXPERIMENTRESULTSSHOWSTHATTHESWITCHINGPOWERSUPPLYPROVIDEAPERFECTQUALITYPOWERFORTHECONTROLLERTHEMOTORSSPEEDCANBESTABILIZEDORADJUSTEDINCESSANTLYIN4KIND
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