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20144doi∶10.11832/j.issn.1000-4858.2014.04.0051231.1001912.1001913.100190A320、B737A380、B787———、、、。3+13H+E。、、。TH137V227V271.1B1000-4858201404-0019-07ConfigurationDesignofFlightControlActuationSystemsforTrunkLineAircraftsQIHai-tao1FUYong-ling2LANGYan31.EngineeringTrainingCenterBeihangUniversityBeijing1001912.SchoolofMechanicalEngineeringandAutomationBeihangUniversityBeijing1001913.BeijingInstituteofControlEngineeringBeijing100190AbstractTheflightcontrolactuationsystemconfigurationandcharacteristicsofthecurrentmainstreamlargeair-craftsA320B737andnewaircraftsA380B787areintroduced.Thefuturetrendsofflightcontrolactuationsys-temforcurrenttrunklineaircraftareoutlinednamelyhighlyintegratedpower-by-wiresignal-by-lighthighpressurehydraulicandintelligent.Forthedevelopmentgoalsofourtrunklineaircraftasuitablepowerconfigura-tionofactuationsystemsforChina’sactualconditionsisproposedwhichconsistsofthreesetsofindependenthy-draulicsystemsplusonesetofelectricalsystemandthecorrespondingactuationsystemconfiguration.Thekeytechnologiesofdevelopingflightcontrolactuationsystemsnamelyarchitecturehighreliableactuatorsfaultprog-nosticsandhealthmanagementareindicated.Keywordsaircraftflightcontrolactuationsystemtrendproposalkeytechnique《2006-2020》161。。、、、、、2。2013-12-2220132851033YWF-13-T-RSC-1001981—、。91201445、、、、3-4。5-13。2013UTC、、、A380、787A400MF-35。14-19。。。1AirbusBoe-ingA320、B737A380、B78716。4。1.1A320A320、、、15017。A320SHAServo-HydraulicActuatorGreenHydraulicSystem、YellowHydraulicSystemBlueHydraulicSystem118。Ailer-onSHARudderSHAElevatorSHASpoilerSHASlatSHAFlapSHATHSTrimmableHorizontalSta-bilizerSHA。1A3201.2B737B737、、、19。B737SHAA、B220。2B7371.3A380A380、“”、、、60021。A380———EHAElec-tro-HydrostaticActuatorEB-HAElectricalBack-upHydraulicActuator、313。02201443A3801.4B787B787、200~300。、“”22。B787———EMAElectro-MechanicalActuator、、423。4B7871.51。1。2、、/。。1A320B737A380B787/2SHA2SHASHA+EHASHA+EHA2SHA2SHA3SHA3SHA2EBHA2EBHA3SHA/1SHASHASHASHA2SHASHASHASHA3SHASHASHASHA4SHASHASHAEMA5SHASHAEBHAEMA6//EBHASHA7//SHASHA8//SHA//2SHA2SHASHA+EHASHA+EHA2SHA2.1。。1、122014423、、、24。4。2.2、、。。251。2。3。4。、。2.3FBLFly-y-LightFBWFly-y-Wire。FBWFBL。261。。2。FBW1/20。FBW3。2010000100Hz4。、。2.4。27。。。A320B73721MPaA380B78735MPa。2.5、、、、28。、、、、、、、。、。、。。3150、、A320B73729。222014453H+E。A320B737A38022B78731。21MPa28MPa。、3128MPa3H+E3Hydraulic+Electircal5。431、、。180L/minEDPEngineDrivenPump30L/minEMPElectricMotorPump30L/minEMPRATRamAirTurbine。EDPEMP。EDPEDPEDPEMP。EMP。EMP2RATRATCSM/GCon-stantSpeedMotor/Generator。PTUPowerTransferUnit。。。。6。EHA/、、SHA。56EHA。3220144644.1。、、、、。4.2。。。4.3。。51、、、23+13H+E3、、。1.2006-2020EB/OL.2006-02-09.http//.htm.2.M.2005148-169.3《》.12M.2003131-153.4MoirI.SeabridgeA.AircraftSystemsMechanicalElectri-calandAvionicsSubsystemsIntegrationM.ThirdEdition.EnglandJohnWiley&SonsLtd.200830-34.5AldenR.C-141andC-130Power-by-wireFlightControlSys-temsC//ProceedingsoftheIEEE1991NationalAero-spaceandElectronicsConference.Dayton1991535-539.6NavarroR.PerformanceofanElectro-hydrostaticActuatorontheF-18SystemsResearchAircraftR.NASA1997.7JensenS.C.JenneyG.D.RaymondB.FlightTestExperi-encewithanElectromechanicalActuatorontheF-18Sys-temsResearchAircraftC//Proceedingsofthe19thDigitalAvionicsSystemsConferences.Philadelphia20002E3/1-2E3/10.8CrokeS.HerrenschmidtJ.MoreElectricInitiative-Power-by-wireActuationAlternativesC//ProceedingsoftheIEEE1994NationalAerospace&ElectronicsConference.NewYork19941338-1346.9BosscheD.V.D.“Moreelectric”ControlSurfaceActuation-AStandardforthenextGenerationofTransportAircraftC//ProceedingsoftheConferenceonMore-electricAir-craft.LondonRoyalAeronauticalSociety2004.10BiedermannO.BildsteinM.DevelopmentQualificationandVerificationoftheA380SpoilerEBHAC//ProceedingsoftheInternationalConferenceonRecentAdvancesinAer-ospaceActuationSystemsandComponents.Toulouse200497-101.11SchleyW.R.ThestateoftheArtandRemainingChallen-gesinElectricActuationforFlightandPropulsioncontrolC//ProceedingsoftheConferenceonMore-ElectricAir-craft.LondonRoyalAeronauticalSociety2004.12TodeschiM.A380FlightControlActuationLessonsLearnedonEHAsDesignC//ProceedingsoftheInternationalConferenceonRecentAdvancesinAerospaceActuationSystemsandComponents.Toulouse200721-26.13CharrierJ.J.KulshreshthaA.ElectricActuationforFlight&EngineControlSystemEvolutionCurrenttrends&Fu-tureChallengesC//Proceedingsofthe45thAIAAAero-spaceSciencesMeetingandExhibit.Reno20071-20.2742201445。。4、。。。5201357。1.M.1999.2.M.1997.3.M.1988.4.J.2009946-47.5.J.200912-4.6.J.200811櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄櫄78-80.2414ToddJ.R.HayJ.A.DinhT.IntegratingFly-by-light/Pow-er-by-wireFlightControlSystemsonTransportAircraftC//AIAA/IEEE12thDigitalAvionicsSystemsConfer-ence.FortWorth1993457-462.15ZavalaE.
本文标题:大型客机飞控作动系统配置方案设计-齐海涛
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