Üç Dönerkanatlı ve Döner-Rotorlu İnsansız Hava Aracının Tasarımı - Design of the Triple Tilt-Rotor Unmanned Aerial Vehicle

Bu makalede, tüm dönerkanat rotorları dönebilen (tilt mekanizmasına sahip), üç dönerkanatlı, dikey kalkış iniş yapabilen insansız hava aracının tasarım süreci sunulmuştur. Bu kapsamda üç rotorlu insansız hava aracı için literatür araştırması, malzeme ve bileşen seçimi, modelleme alt yapısının kurulması, enerji tüketim analizi, titreşim analizi, statik yük analizi ve fiziksel sistem testleri gibi çalışmalar yürütülmüştür. In this paper, design process of a VTOL (Vertical Take Off – Landing) type unmanned aerial vehicle with three tilting rotors is presented. In this framework, literature survey, material and component selection, modeling environment, energy consumption analysis, vibration analysis,  statical load analysis, and physical system test studies are carried out for the tri-rotor unmanned aerial vehicle.

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In this paper, design process of an VTOL (Vertical Take Off – Landing) type unmanned aerial vehicle with three tilting rotors is presented. In this framework, modeling environment, energy consumption analysis, material and component selection, vibration analysis, static load analysis, and physical system test studies are discussed. Initial prototype is reached and flight tests are initiated

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