Development of tilt-rotor unmanned aerial vehicle (UAV): material selection and structural analysis on wing design

4th AEROTECH- Innovation in Aerospace Engineering and Technology

航空航天工程

Saharudin, M.F.^1

Jabatan Penyenggaraan Pesawat, Politeknik Banting, Selangor, Malaysia^1

关键词: Flight loads;    Flight test;    Material selection;    Standard requirements;    Structure design;    Tilt rotor;    Wing design;    Wing section;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/152/1/012017/pdf
DOI  :  10.1088/1757-899X/152/1/012017

学科分类：航空航天科学

来源: IOP

【 摘 要 】

This paper presents the design of a tilting rotor unmanned aerial vehicle (UAV), evaluation of flight loads based on the standard requirement, structural analysis to determine stress and sizing of the wing, and flight test of the UAV. The main objective is to perform structural analysis to size the UAV's wing section. The analysis shows that the structure design of the wing is safe to be used.