ANALISIS KEKUATAN STRUKTUR PLATFORM PUNA CW AERONES
AD28 MENGGUNAKAN SOFTWARE CATIA V5R20
Total View This Week0
Total View This Week0
Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
HIDAYAT, ZAKI
Subject
T Technology (General)
Datestamp
2024-06-21 06:10:26
Abstract :
PUNA CW is a development of type multicopter PUNA which has a mission to clean the windows of high buildings. One important part of PUNA CW is the frame where this part is the place to put the engine, then this frame will be lifted by the engine first. Because the mission of PUNA CW, the frame is often exposed to water which can cause corrosion in material aluminum. So it is necessary to consider the use of material in this frame. Carbon material is known to be strong and resistant to corrosion and is widely used in the aviation. So in this research, it will discuss the strength analysis of the structure to determine the maximum stress that occurs and the safety of the PUNA CW Aerones AD28 platform structure. The geometrics of PUNA CW Aerones AD28 platform modeled with CATIA V5R20 Software in Part Design workbench, are combined in Workbench Assembly Design. The results of the Assembly Product will be analyzed in the Workbench Generative Structural Analysis. The loading of the platform structure is carried out under take off and steady conditions with thrust load variations. The results of the analysis will get the stress value, then calculated a Margin of Safety. The results of this research show that for the highest maximum stress at take off is 6.02404 x 108 N/m2 precisely located on a plate with a Margin of Safety of 0.44. While the maximum stress value that occurs on the platform structure of PUNA Aerones AD28 at a steady state is 9.58918 x 107 N/m2 precisely located on a plate with a 8.04 Margin of Safety. These results indicate that the structure of the PUNA Aerones AD28 platform is safe in operation.
PUNA CW is a development of type multicopter PUNA which has a mission to clean the windows of high buildings. One important part of PUNA CW is the frame where this part is the place to put the engine, then this frame will be lifted by the engine first. Because the mission of PUNA CW, the frame is often exposed to water which can cause corrosion in material aluminum. So it is necessary to consider the use of material in this frame. Carbon material is known to be strong and resistant to corrosion and is widely used in the aviation. So in this research, it will discuss the strength analysis of the structure to determine the maximum stress that occurs and the safety of the PUNA CW Aerones AD28 platform structure. The geometrics of PUNA CW Aerones AD28 platform modeled with CATIA V5R20 Software in Part Design workbench, are combined in Workbench Assembly Design. The results of the Assembly Product will be analyzed in the Workbench Generative Structural Analysis. The loading of the platform structure is carried out under take off and steady conditions with thrust load variations. The results of the analysis will get the stress value, then calculated a Margin of Safety. The results of this research show that for the highest maximum stress at take off is 6.02404 x 108 N/m2 precisely located on a plate with a Margin of Safety of 0.44. While the maximum stress value that occurs on the platform structure of PUNA Aerones AD28 at a steady state is 9.58918 x 107 N/m2 precisely located on a plate with a 8.04 Margin of Safety. These results indicate that the structure of the PUNA Aerones AD28 platform is safe in operation.
Download
book
BibTex
Latex, Jabref
cloud_download
Original Resource
url resource Institution
