Résumé

The Boeing 747-400 aircraft incorporates a tricycle four-wheeled and two-axled landing gear. Being a jumbo-jet, the landing gear of Boeing 747-400 deals with tremendous loads during an approach, therefore, it becomes extremely important to identify critical sections and estimate the maximum stresses the gear can take, corresponding to various glideslopes. This paper deals with the determination of critical section and stresses developed in a landing gear during an approach. Three glideslopes of 3, 5 and 10 degrees were used to find critical section in a landing gear.

Détails

Titre
Stress Analysis of Landing Gear of Boeing 747-400 Aircraft
Auteur
Khatawate, Vinayak H 1 ; Parikh, Parva 2 ; Radadiya, Ronak 2 

 Associate Professor, Dept. of Mechanical Engineering, Dwarkadas J. Sanghvi College of Engineering, Mumbai, India 
 UG Student, Dept. of Mechanical Engineering, Dwarkadas J. Sanghvi College of Engineering, Mumbai, India 
Année de publication
2021
Date de publication
Apr 2021
Éditeur
IOP Publishing
ISSN
17578981
e-ISSN
1757899X
Type de source
Publication académique
Langue de publication
English
ID de document ProQuest
2535588110
Copyright
© 2021. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.