AIRFRAME RECONSTRUCTION OF A 2-SEATER HELICOPTER

Air vehicles are particularly suitable for express deliveries or pick-ups on short routes. Helicopters with a UAV control could be the answer for delivering logistics in limited access areas such as Papua with a topography that is hard to access. UAV could reduce the possibility of casualties becaus...

Full description

Saved in:
Bibliographic Details
Main Author: Jovann Muliono, Ignatius
Format: Final Project
Language:Indonesia
Subjects:
Online Access:https://digilib.itb.ac.id/gdl/view/83083
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:83083
spelling id-itb.:830832024-08-01T11:48:13ZAIRFRAME RECONSTRUCTION OF A 2-SEATER HELICOPTER Jovann Muliono, Ignatius Teknik (Rekayasa, enjinering dan kegiatan berkaitan) Indonesia Final Project AISI 4130, Body, Helicopter, Leg, Tail, Safety Factor, Structure INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/83083 Air vehicles are particularly suitable for express deliveries or pick-ups on short routes. Helicopters with a UAV control could be the answer for delivering logistics in limited access areas such as Papua with a topography that is hard to access. UAV could reduce the possibility of casualties because with a UAV the control is autonomous with a computer without a pilot like a regular aircraft. This study aims to design the helicopter structure and determine the tube sizing used as the material of the helicopter structure. This research will be divided into three main parts, namely the helicopter body, helicopter tail, and helicopter legs where each design of the three main parts will be analyzed based on the safety factor and stress. The results of the study show that in the initial design of the helicopter body, the safety factor value is below 1.5 so it is necessary to reinforce the design. The results of the reinforcement carried out resulted in a safety factor value above 1.5, so that the reinforced design of the helicopter body was accepted. In the tail of the helicopter, the analysis was reviewed in 2 conditions, namely normal conditions and 1/12 MTOW. All analysis results on the tail of the helicopter also produced a safety factor value above 1.5, so that the reinforced helicopter design was accepted. All analysis results on the tail of the helicopter also produced a safety factor so that the reinforced helicopter design was accepted. Then on the helicopter legs, the AISI 4130 material cannot be used because the safety factor value is too small, so it is replaced with carbon fiber or Kevlar. In this design, High Strength Steel AISI 4130 will be used as the material that makes up the frame with a material diameter of 0.5 inches (12.7 mm) and a schedule of 40 (4 mm). text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
topic Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
spellingShingle Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
Jovann Muliono, Ignatius
AIRFRAME RECONSTRUCTION OF A 2-SEATER HELICOPTER
description Air vehicles are particularly suitable for express deliveries or pick-ups on short routes. Helicopters with a UAV control could be the answer for delivering logistics in limited access areas such as Papua with a topography that is hard to access. UAV could reduce the possibility of casualties because with a UAV the control is autonomous with a computer without a pilot like a regular aircraft. This study aims to design the helicopter structure and determine the tube sizing used as the material of the helicopter structure. This research will be divided into three main parts, namely the helicopter body, helicopter tail, and helicopter legs where each design of the three main parts will be analyzed based on the safety factor and stress. The results of the study show that in the initial design of the helicopter body, the safety factor value is below 1.5 so it is necessary to reinforce the design. The results of the reinforcement carried out resulted in a safety factor value above 1.5, so that the reinforced design of the helicopter body was accepted. In the tail of the helicopter, the analysis was reviewed in 2 conditions, namely normal conditions and 1/12 MTOW. All analysis results on the tail of the helicopter also produced a safety factor value above 1.5, so that the reinforced helicopter design was accepted. All analysis results on the tail of the helicopter also produced a safety factor so that the reinforced helicopter design was accepted. Then on the helicopter legs, the AISI 4130 material cannot be used because the safety factor value is too small, so it is replaced with carbon fiber or Kevlar. In this design, High Strength Steel AISI 4130 will be used as the material that makes up the frame with a material diameter of 0.5 inches (12.7 mm) and a schedule of 40 (4 mm).
format Final Project
author Jovann Muliono, Ignatius
author_facet Jovann Muliono, Ignatius
author_sort Jovann Muliono, Ignatius
title AIRFRAME RECONSTRUCTION OF A 2-SEATER HELICOPTER
title_short AIRFRAME RECONSTRUCTION OF A 2-SEATER HELICOPTER
title_full AIRFRAME RECONSTRUCTION OF A 2-SEATER HELICOPTER
title_fullStr AIRFRAME RECONSTRUCTION OF A 2-SEATER HELICOPTER
title_full_unstemmed AIRFRAME RECONSTRUCTION OF A 2-SEATER HELICOPTER
title_sort airframe reconstruction of a 2-seater helicopter
url https://digilib.itb.ac.id/gdl/view/83083
_version_ 1822997945128058880