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文件名称:无人机正交双轴折叠翼展开机构设计及气动特性研究.pdf
文件大小:5.19 MB
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更新时间:2025-06-23
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文档摘要

Abstract

Withtherapiddevelopmentofunmannedaircrafttechnology,fixed-wingunmanned

aircrafthavemadeitdifficulttomeetthedemandformulti-missionadaptabilityincomplex

environments.Folding-wingunmannedaircrafthavebeengraduallyappliedtovariousfields,

especiallyinthemilitaryfield,duetotheiruniqueadvantagesofportability,concealment,and

remotecontrol,whichcangreatlyreducecasualtiesandstriketargetsquicklyandaccurately.

Unmannedaerialvehicleswillbeusedforaerialtargets,andgraduallydevelopintohigh-tech

armeddevicesthatcanachievevariousfunctionssuchasdetection,interference,andshooting.

Theminiaturization,intelligence,systematization,andhighspeedandlongflighttimeofUAVs

willbethefuturedevelopmenttrend.Atpresent,therearemorestudiesonthefolding

mechanismathomeandabroad,andthedevelopmentofUAVstendstobemoreandmore

diversifiedinthefoldingmethod,intelligentinthefoldingmechanism,andinexpensiveinthe

productioncost.Inthefuture,improvingthereliabilityofthefoldingmechanismofUAVsand

reducingthemanufacturingcostwillbethetoppriorityforthedevelopmentofUAVsindustry,

whiletheunfoldingmodeofUAVsfoldingwingandtheinnovativedesignofthefolding

mechanismwillbecomethekeytosolvetheaboveproblems.Therefore,thedevelopmentof

lightweight,low-cost,andhigh-reliabilityfoldingmechanismtechnologyhasaverybroad

researchprospect.Inthispaper,wecarryoutresearchontheunfoldingmode,folding

mechanism,andaerodynamiccharacteristicsoffoldedwingsforUAVs.

Aimingatthecharacteristicsoftheorthogonalbiaxialfoldingwingmechanism,wecontrol

theunfoldingtimesequenceofthefoldingwinganddesignavarietyofunfoldingmodesfor

thefoldingwingofth