外文翻译--螺杆压缩机的三维分析开发.doc_第1页
外文翻译--螺杆压缩机的三维分析开发.doc_第2页
外文翻译--螺杆压缩机的三维分析开发.doc_第3页
外文翻译--螺杆压缩机的三维分析开发.doc_第4页
外文翻译--螺杆压缩机的三维分析开发.doc_第5页
已阅读5页,还剩10页未读 继续免费阅读

下载本文档

版权说明:本文档由用户提供并上传,收益归属内容提供方,若内容存在侵权,请进行举报或认领

文档简介

英文原文4.1IntroductionThischapterdemonstratesthescopeofthemethoddevelopedforthethree-dimensionalanalysisofascrewcompressor.TheCFDpackageusedinthiscasewasCOMETdevelopedbyICCMGmbHHamburg,todayapartofCD-Adapco.Theanalysisoftheflowandperformancecharacteristicsofanumberoftypesofscrewmachinesisperformedtodemonstrateavarietyofparametersusedforgridgenerationandcalculation.Thefirstexampleisconcernedwithadryairscrewcompressor.Acommoncompressorcasingisusedwithtwoalternativepairsofrotors.Therotorshaveidenticaloverallgeometricpropertiesbutdifferentlobeprofiles.Theapplicationoftheadaptationtechniqueenablesconvenientgridgenerationforgeometricallydifferentrotors.Theresultsobtainedbythreedimensionalmodellingarecomparedwiththosederivedfromaone-dimensionalmodel,previouslyverifiedbycomparisonwithexperimentaldata.Therelativeadvantagesofeachrotorprofilearedemonstrated.Thesecondexampleshowstheapplicationofthreedimensionalflowanalysistothesimulationofanoilinjectedaircompressor.Theresults,thusobtained,arecomparedwithtestresultsobtainedbytheauthorsfromacompressorandtestrig,designedandbuiltatCityUniversity.Theyarepresentedintheformofbothintegralparametersandap-indicatordiagram.Calculationsbasedontheassumptionsofthelaminarflowarecomparedtothoseofturbulentflow.Theeffectofgridsizeontheresultsisalsoconsideredandshownhere.Thethirdexamplegivestheanalysisofanoilinjectedcompressorinanammoniarefrigerationplant.Thisutilisestherealfluidpropertysubroutinesintheprocesscalculationsanddemonstratestheblowholeareaandtheleakageflowthroughthecompressorclearances.Thefourthexamplepresentstwocases,oneofadryscrewcompressortoshowtheinfluenceofthermalexpansionoftherotoronscrewcompressorperformanceandoneofahighpressureoil-floodedscrewcompressortoshowtheinfluenceofhighpressureloadsuponthecompressorperformance.4.2FlowinaDryScrewCompressorDryscrewcompressorsarecommonlyusedtoproducepressurisedair,freeofanyoil.Atypicalexampleofsuchamachine,similarinconfigurationtothecompressormodelled,isshowninFigure4-1.Thisisasinglestagemachinewith4maleand6femalerotorlobes.Themaleandfemalerotorouterdiametersare142.380mmand135.820mmrespectively,whiletheircentrelinesare108.4mmapart.Therotorlengthtomaindiameterratiol/d=1.77.Thus,therotorlengthis252.0mm.Themalerotorwithwrapangle=248.40isdrivenataspeedof6000rpmbyanelectricmotorthroughagearbox.Themaleandfemalerotorsaresynchronisedthroughtiminggearswiththesameratioasthatofthecompressorrotorlobesi.e.1.5.Thefemalerotorspeedistherefore4000rpm.Themalerotortipspeedisthen44.7m/s,whichisarelativelylowvalueforadryaircompressor.Theworkingchamberissealedfromitsbearingsbyacombinationoflipandlabyrinthseals.Eachrotorissupportedbyoneradialandoneaxialbearing,onthedischargeend,andoneradialbearingonthesuctionendofthecompressor.Thebearingsareloadedbyahighfrequencyforce,whichvariesduetothepressurechangewithintheworkingchamber.Bothradialandaxialforces,aswellasthetorquechangewithafrequencyof4timestherotationalspeed.Thiscorrespondsto400Hzandcoincideswiththenumberofworkingcyclesthatoccurwithinthecompressorperunittime.Figure4-1CrosssectionofadryscrewcompressorThecompressortakesinairfromtheatmosphereanddischargesittoareceiverataconstantoutputpressureof3bar.Althoughthepressureriseismoderate,leakagethroughradialgapsof150missubstantial.Inmanystudiesandmodelling,procedures,volumetriclossesareassumedtobealinearfunctionofthecrosssectionalareaandthesquarerootofpressuredifference,assumingthattheinterlobeclearanceiskeptmoreorlessconstantbythesynchronisinggears.Theleakagethroughtheclearancesisthenproportionaltotheclearancegapandthelengthoftheleakageline.However,alargeclearancegapisneededtopreventcontactwiththehousingcausedbyrotordeformationduetothepressureandtemperaturechangeswithintheworkingchamber.Hence,theonlywaytoreduceleakageistominimisethelengthofthesealingline.Thiscanbeachievedbycarefuldesignofthescrewrotorprofile.Althoughminimising,leakageisanimportantmeansofimprovingascrewcompressorefficiency,itisnottheonlyone.Anotheristoincreasetheflowareabetweenthelobesandtherebyincreasethecompressorflowcapacity,therebyreducingtherelativeeffectofleakage.Modernprofilegenerationmethodstakethesevariouseffectsintoaccountbymeansofoptimisationprocedureswhichleadtoenlargementofthemalerotorinterlobesandreductioninthefemalerotorlobes.Thefemalerotorlobesaretherebystrengthenedandtheirdeformationthusreduced.Todemonstratetheimprovementspossiblefromrotorprofileoptimisation,athreedimensionalflowanalysishasbeencarriedoutfortwodifferentrotorprofileswithinthesamecompressorcasing,asshowninFigure4-2.Bothrotorsareofthe“N”typeandrackgenerated.Figure4-2NRotors,Case-1upper,Case-2lowerCase1isanolderdesign,similarinshapetoSRM“D”rotors.Itsfeaturesimplythatthereisalargetorqueonthefemalerotor,thesealinglineisrelativelylongandthefemalelobesarerelativelyweak.Case2,shownonthebottomofFigure4-2,hasrotorsoptimisedforoperatingondryair.Thefemalerotorisstrongerandthemalerotorisweaker.Thisresultsinhigherdelivery,arelativelyshortersealinglineandlesstorqueonthefemalerotor.Allthesefeatureshelptoimprovescrewcompressorperformance.Theresultsofthesetwoanalysesarepresentedintheformofvelocitydistributionsintheplanesdefinedbycross-sectionsA-AandB-B,showninFigure4-1.Inthecaseofthisstudy,theeffectofrotorprofilechangesoncompressorintegralperformanceparameterscanbepredictedfairlyaccuratelywithone-dimensionalmodels,evenifsomeofthedetailedassumptionsmadeinsuchanalyticalmodelsareinaccurate.Hencetheintegralresultsobtainedfromthethree-dimensionalanalysisarecomparedwiththosefromaone-dimensionalmodel.4.2.1GridGenerationforaDryScrewCompressorInCase-1,therotorsaremappedwith52numericalcellsalongtheinterlobeonthemalerotorand36cellsalongeachinterlobeonthefemalerotorinthecircumferentialdirection.Thisgives208and216numericalcellsrespectivelyinthecircumferentialdirectionforthemaleandfemalerotors.Atotalof6cellsintheradialdirectionand97cellsintheaxialdirectionisspecifiedforbothrotors.Thisarrangementresultsinanumericalmeshwith327090cellsfortheentiremachine.ThecrosssectionfortheCase-1rotorsisshowninFigure4-3.Thefemalerotorisrelativelythinandhasalargeradiusonthelobetip.Therefore,itismoreeasilymappedthaninCase-2wherethetipradiusissmaller,asshowninFigure4-4.Figure4-3CrosssectionthroughthenumericalmeshforCase-1rotorsTherotorsinCase2aremappedwith60cellsalongthemalerotorlobeand40cellsalongthefemalelobe,whichgives240cellsalongbothrotorsinthecircumferentialdirection.Intheradialdirection,therotorsaremappedwith6cellswhile111cellsareselectedformappingalongtherotoraxis.Thus,theentireworkingchamberforthiscompressorhas406570cells.Inthiscase,differentmeshsizesareappliedanddifferentcriteriaarechosenfortheboundaryadaptationofthesero

温馨提示

  • 1. 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。图纸软件为CAD,CAXA,PROE,UG,SolidWorks等.压缩文件请下载最新的WinRAR软件解压。
  • 2. 本站的文档不包含任何第三方提供的附件图纸等,如果需要附件,请联系上传者。文件的所有权益归上传用户所有。
  • 3. 本站RAR压缩包中若带图纸,网页内容里面会有图纸预览,若没有图纸预览就没有图纸。
  • 4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
  • 5. 人人文库网仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对用户上传分享的文档内容本身不做任何修改或编辑,并不能对任何下载内容负责。
  • 6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
  • 7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

评论

0/150

提交评论