PERANCANGAN DAN ANALISIS KEKUATAN STRUKTUR
PESAWAT TANPA AWAK EAGLE -X MIRIP BURUNG MENGGUNAKAN SOFTWARE ANSYS
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
MAULANA, AGUS
Subject
T Technology (General)
Datestamp
2024-06-21 06:11:35
Abstract :
Many missions are so difficult to reach by humans, one of the interesting parts to address is the agricultural sector, the rise of bird pests that interfere with the agricultural process, and difficult to control agricultural land that has a large area resulting in damage to agricultural products that have an impact on less than the maximum farm results obtained. The use of bird-like UAVs is expected to maximize the process of preventing damage to agricultural areas by flocks of birds. Modeling the internal structure of the aircraft is carried out using the CATIA Software, modeling the structure grouped in parts by section, aiming to make the analysis phase easier. In the analysis phase the results to be seen are how the total deformation that occurs in the plane by assuming the load incurred, and varying the analysis using load factor 2.5. after displaying the total deformation, then displaying the stresses that occur, the voltage values that have been obtained, will be used for the process of calculating the margin of safety. The results of the UAV structure modeling show that the Fuselage structure uses a semi monocoque structure, which uses bulkhed and Struktur as reinforcement of the Fuselage structure. The wing is strengthened by 16 ribs and uses carbon joiner s. And coated with skin using balsa material. In the tail only uses polyfoam material as the main material. from the structure test shows that the maximum stress that occurs in Fuselage is 0.055079 Mpa, the maximum stress in the wing model is 11.541 Mpa. In the tail model the voltage occurs at 0.01159 MPa. With a total deformation of the tail of 0.0158 mm. total deformation in Fuselage is 0.01363 mm. the total deformation of the wing is 1.7609 mm. these results indicate that the structure used on the EAGLE-X aircraft is safe..
Many missions are so difficult to reach by humans, one of the interesting parts to address is the agricultural sector, the rise of bird pests that interfere with the agricultural process, and difficult to control agricultural land that has a large area resulting in damage to agricultural products that have an impact on less than the maximum farm results obtained. The use of bird-like UAVs is expected to maximize the process of preventing damage to agricultural areas by flocks of birds. Modeling the internal structure of the aircraft is carried out using the CATIA Software, modeling the structure grouped in parts by section, aiming to make the analysis phase easier. In the analysis phase the results to be seen are how the total deformation that occurs in the plane by assuming the load incurred, and varying the analysis using load factor 2.5. after displaying the total deformation, then displaying the stresses that occur, the voltage values that have been obtained, will be used for the process of calculating the margin of safety. The results of the UAV structure modeling show that the Fuselage structure uses a semi monocoque structure, which uses bulkhed and Struktur as reinforcement of the Fuselage structure. The wing is strengthened by 16 ribs and uses carbon joiner s. And coated with skin using balsa material. In the tail only uses polyfoam material as the main material. from the structure test shows that the maximum stress that occurs in Fuselage is 0.055079 Mpa, the maximum stress in the wing model is 11.541 Mpa. In the tail model the voltage occurs at 0.01159 MPa. With a total deformation of the tail of 0.0158 mm. total deformation in Fuselage is 0.01363 mm. the total deformation of the wing is 1.7609 mm. these results indicate that the structure used on the EAGLE-X aircraft is safe..
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