MODIFIKASI DAN MANUFAKTUR BATANG VTOL (VERTICAL TAKE OFF LANDING) PESAWAT UAV V-SKY 14 STTA

CIPTO PURBONINGRUM, SATRIO (2020) MODIFIKASI DAN MANUFAKTUR BATANG VTOL (VERTICAL TAKE OFF LANDING) PESAWAT UAV V-SKY 14 STTA. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

Research and development of UAV (Unmaned Aerial Vechiel) aircraft has been carried out at Adisutjipto College of Technology. One of the aircraft that is being developed is the V-SKY 14 aircraft which has special capabilities in the form of vertical take-off and landing and flying Cruise such as fixs wing aircraft. In its design the aircraft has 5 engines installed in the form of 4 engines that are useful for VTOL and 1 engine that is useful for flying Cruise. This configuration causes complex control systems as well as large system loads. Therefore, research is conducted that aims to modify the VTOL bar so that the VTOL bar can change the direction of the thrust of the VTOL engine, this allows the VTOL engine to be used as an engine for flying Cruises. The process of modelling the VTOL Bar modification and kinematics simulation using CATIA V5R20 software, calculation of the strength of the structure using ANSYS 15 software. In the case of loading, a load factor of 3.8 is used based on FAR 23 regulations. There are 4 cases of loading carried out on the VTOL Bar in accordance with the location and manouver to be carried out. After finding the maximum stress results, we get a Margin of Safety. Manufacturing of designs that have been made is done by the method of 3D printing, conventional machines, and bench work. After going through the stages of structural analysis and kinematics simulation, it was found that the highest stress occurred in part 2 with a value of 8413500 pa. and the relationship between two different gears is having the same angular speed with different rotational directions with the ratio between the engine linear speed to the gear linear speed being 5: 3.

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