Desain dan Analisis Kekuatan Rangka Tricycle Landing Gear UAV Menggunakan Metode Elemen Hingga

Abstract

This study examined the design and analysis of tricycle landing gear frame strength using the finite element method. Linear static analysis was carried out using Autodesk Inventor Professional 2017. The landing gear frame material used Aluminum 6061. Variable vertical landing speeds were 4 m/s, 6 m/s, 8 m/s, and 10 m/s. Simulation results show that the landing gear frame is safe enough to withstand landing speeds of up to 8 m/s because it has a safety factor of 2.32. Abstrak Penelitian ini mengkaji tentang desain dan analisis kekuatan rangka tricycle landing gear menggunakan metode elemen hingga. Analisis statik linear dilakukan menggunakan software Autodesk Inventor Professional 2017. Material rangka landing gear menggunakan Aluminium 6061. Variabel kecepatan landing vertikal yaitu 4 m/s, 6 m/s, 8 m/s, dan 10 m/s. Hasil simulasi menunjukkan bahwa rangka tricycle landing gear cukup aman untuk menahan kecepatan landing hingga 8 m/s karena memiliki faktor keamanan sebesar 2,32.