组合无人机柔顺分离机构设计与特性研究

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中图分类号：V222 文献标志码：A DOI：10.16385/j.cnki.issn.1004-4523.202312054

Abstract：Tometthedemandforfastandreliableseparationtechnologyinaerospaceengineering，alow-impactcomplianteparation mechanismdrivebytorueisproposd.emechanicalaractersticsimuationandcallationasisereoducteddte separainexperintasvaliatdBasdotopechacteristoftusalaeleratiofuctioemealoel oftheseparationmechanismasconstructedTemometumNavier-StoksequatiosandCoulobsfrictionlawwereemploedtodeteie theaerodyamicloaddistributionunderalloperatingconditiosTemechanicalcharacterisicsofteseparationmehanismweeaalyd usingthefinitelementmetodandadmesioalparameterotimizationtechiqueasapliedtootimizetesparationcis， effectivelyreducingstressoncetrationonitsaibearingpartoughdyamicsimuationofseparatios，preliaryerificationof flexibilityaractestsinodelfsepatiesasceedalototstimostatedsuesuling andseparationinvariousenvironmentsSimulationresultslongwithgroundexperimentsidicatethat theproposedseparationmchanism exhibitseeltactproeslsntiosproingietdodalrohoble aerospace engineering separation technology.

Keywords;separation mechanism; compliantseparation technology;separationdynamics;aerodynamiccharacteristics

近年来，随着电子技术、控制技术与人工智能技术的更新迭代，无人机（unmannedaerialvehicle，UAV）技术得到迅速发展，在民用领域和军事领域得到了广泛应用[1-2]。（剩余12290字）