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二元喉道倾斜矢量喷管调节方法 Title:MethodsofRegulatingBinaryThroat-InclinedVectorNozzle Introduction: Thebinarythroat-inclinedvectornozzleisanessentialcomponentofmodernpropulsionsystemsusedinaerospaceapplications.Thenozzleplaysapivotalroleinachievingthedesiredthrustandmaneuverabilityofrocketsandaircraft.Efficientregulationandcontrolofthenozzle'sparameterscansignificantlyimprovetheperformance,stability,andfuelefficiencyofthepropulsionsystem.Thispaperaimstoexploreanddiscussvariousmethodsandtechniquesforregulatingthebinarythroat-inclinedvectornozzle. 1.OverviewofBinaryThroat-InclinedVectorNozzle: Thebinarythroat-inclinedvectornozzleisanoveldesignthatallowsforthrustvectoringcontrolbychangingtheinclinationangleoftwothroatchannels.Bymanipulatingthethroatarearatio,theexpansionprocesswithinthenozzlecanbeadjusted,leadingtovariableexhaustvelocityandthrustdirection.Thistechnologyenablesimprovedvehiclestability,enhancedmaneuverability,anddecreasedfuelconsumption. 2.TraditionalMethodsofNozzleControl: Historically,mechanicalgimbalingsystemshavebeenusedtocontrolnozzleinclination.Thesemethodsinvolvetheuseofactuatorsandmechanicallinkagestoadjustthenozzle'spositioningduringflight.Whileeffective,thesesystemsarecomplex,heavy,andpronetowearandtear.Moreover,suchmechanicaldeviceslimittherangeandspeedofnozzleadjustment. 3.ElectromagneticActuation: Analternativeapproachforregulatingthebinarythroat-inclinedvectornozzleisthroughelectromagneticactuation.Thismethodutilizesmagneticfieldsgeneratedbyelectromagnetstoinducemotioninthenozzle'sthroatchannels.Theadvantageofthistechniqueisitsabilitytoprovideprecisecontrol,rapidresponsetime,andreducedmechanicalcomplexity.Additionally,iteliminatestheneedforphysicalcontactbetweenmovingparts,makingithighlyreliableanddurable. 4.PiezoelectricControl: Piezoelectricmaterialscanbeemployedforcontrollingbinarythroat-inclinedvectornozzles.Thesematerialsundergodeformationwhensubjectedtoanelectricfield.Byintegratingpiezoelectricactuatorsintothenozzlestructure,theinclinationangleca