PROSES MANUFAKTUR SAYAP PESAWAT UAV GIP-X DAN UJI BEBAN MAKSIMUM AKIBAT BENDING DENGAN PENDEKATAN EKSPERIMEN

Iwan Purnomo, Giarto (2022) PROSES MANUFAKTUR SAYAP PESAWAT UAV GIP-X DAN UJI BEBAN MAKSIMUM AKIBAT BENDING DENGAN PENDEKATAN EKSPERIMEN. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

UAV (Unmanned Aerial Vehicle) is a technology developed on an airplane or aircraft engine that can be controlled remotely or can be programmed for a particular mission. In its development, UAV technology is widely used in the military field, namely for reconnaissance or spying activities, used to attack the enemy and guard the border by air so that it is more profitable because it can reduce casualties, besides that it can also be used in various activities such as land mapping, taking pictures, knowing the condition of an area through aerial photography and various other activities. With this goal, of course, UAV aircraft must have toughness in various fields, so it is necessary for the development of UAV aircraft, one of which is in the manufacturing process for UAV aircraft components, especially on the wing of the aircraft. In the manufacturing process of manufacturing aircraft wings, the materials used are balsa wood and composites, then a comparative test will be carried out to measure the strength of the UAV wings. This study aims to produce a prototype of the composite wing of the UAV GIP-X using the hand lay-up method and aims to determine the maximum load and deflection that can be resisted by the Balsa Wood and the Carbon wing of the UAV GIP-X and. By using the Hand lay-up method which is the first method in making composites. In this hand lay-up method, the most widely used resins are polyester and epoxies. Based on the results obtained from data analysis, it can be concluded that the results of the study show: From the results of making composite wings of the GIP-X UAV aircraft using the hand lay-up method, it can produce a prototype of the GIP-X UAV aircraft with carbon material. The test results on the wing obtained from the full test of balsa wood with a maximum load of 6.75 kg. And the results of testing on carbon composites obtained a Maximum Bending Load of 4.5kg. the maximum deflection of the full balsa wood test is 160mm while the maximum deflection of the carbon composite test is 159.5mm.

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