PERANCANGAN DAN ANALISIS KEKUATAN STRUKTUR
PESAWAT UAV SPRAYER AMF–16 IF
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
IKHSANUL MIRJA, MUHD
Subject
T Technology (General)
Datestamp
2024-07-19 08:27:57
Abstract :
The UAV Sprayer AMF?16 IF aircraft is designed with a mission of watering and spraying plants with a carrying capacity of 3 kg. This aircraft is also made for helping agricultural activities can be more effective and efficient. It is categorized as a rotary wing with a total of 4 motors and can take?off landing in narrow runway conditions. For this reason, this study discusses the design and analysis of structural strength for UAV Sprayer AMF?16 IF. The process begins by calculating the weight sizing and creating the geometry. Then proceed to the modeling process using CATIA V5R21 software. The finished modeling is imported into the ANSYS 17.1 software for structural strength analysis. Structure loading is carried out under 2 conditions, namely static load and vertical take?off. The results of the analysis to obtain the maximum stress value which is useful for knowing the failure criteria value and the margin of safety. The results of this studys show that the UAV Sprayer AMF?16 IF aircraft has an overall weight of 7.806 kg. The maximum stress value that occurs in the aircraft structure is 2,0129x107 Pa (static load) and 1,4919x107 Pa (vertical take? off). Hence, the highest value of failure criteria is 1,1171x10-2 (static load) and 3,6362x10-2 (vertical take?off). while the highest value is margin of safety of 15,3258 (static load) and 16,6383 (vertical take?off).
The UAV Sprayer AMF?16 IF aircraft is designed with a mission of watering and spraying plants with a carrying capacity of 3 kg. This aircraft is also made for helping agricultural activities can be more effective and efficient. It is categorized as a rotary wing with a total of 4 motors and can take?off landing in narrow runway conditions. For this reason, this study discusses the design and analysis of structural strength for UAV Sprayer AMF?16 IF. The process begins by calculating the weight sizing and creating the geometry. Then proceed to the modeling process using CATIA V5R21 software. The finished modeling is imported into the ANSYS 17.1 software for structural strength analysis. Structure loading is carried out under 2 conditions, namely static load and vertical take?off. The results of the analysis to obtain the maximum stress value which is useful for knowing the failure criteria value and the margin of safety. The results of this studys show that the UAV Sprayer AMF?16 IF aircraft has an overall weight of 7.806 kg. The maximum stress value that occurs in the aircraft structure is 2,0129x107 Pa (static load) and 1,4919x107 Pa (vertical take? off). Hence, the highest value of failure criteria is 1,1171x10-2 (static load) and 3,6362x10-2 (vertical take?off). while the highest value is margin of safety of 15,3258 (static load) and 16,6383 (vertical take?off).
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