Results 1 to 10 of about 106,651 (339)

Fiber Bragg Grating Based Load Monitoring for Carrier-Based Aircraft Main Landing Gear [PDF]

Sensors
A three-dimensional load regression system based on fiber Bragg grating strain sensor is proposed to meet the load monitoring requirements of the main landing gear of an aircraft during take-off and landing. The FBG sensors, featuring a strain resolution
Weijun Xue, Heng Huang, Xiwen Pang, Guang Yan   +3 more
doaj   +3 more sources

Optimization of the Main Landing Gear Structure of LSU-02NGLD

Computational and Experimental Research in Materials and Renewable Energy, 2021
The mass of the landing gear structure becomes an important aspect of the total mass of the UAV (unmanned aerial vehicle). Therefore, many efforts have been made to reduce the mass of the landing gear by performing structural optimization.
Fajar Ari Wandono
doaj   +4 more sources

Inerter-Based Configurations for Main-Landing-Gear Shimmy Suppression [PDF]

Journal of Aircraft, 2017
The work reported in this paper concentrates on the possibility of suppressing shimmy oscillations of landing gear more effectively using a linear passive suppression device incorporating inerter. The inerter is a one-port mechanical device with the property that the applied force is proportional to the relative acceleration between its terminals.
Yuan Li, J. Z. Jiang, S. Neild
semanticscholar   +7 more sources

A Novel Framework for Qualification of a Composite-Based Main Landing Gear Strut of a Lightweight Aircraft. [PDF]

Polymers (Basel), 2023
The determination of suitable testing and qualification procedures for fiber-reinforced polymer matrix composite structures is an active area of research due to the increased demand, especially in the field of aerospace.
Ahmad MA, Ali Shah SI, Khan SA, Khan HA, Shams TA.   +4 more
europepmc   +2 more sources

Application of Operational Load Monitoring System for Fatigue Estimation of Main Landing Gear Attachment Frame of an Aircraft. [PDF]

Materials (Basel), 2021
In this paper, we present an approach to fatigue estimation of a Main Landing Gear (MLG) attachment frame due to vertical landing forces based on Operational Loads Monitoring (OLM) system records.
Dziendzikowski M, Kurnyta A, Reymer P, Kurdelski M, Klysz S, Leski A, Dragan K.   +6 more
europepmc   +2 more sources

Selection Methodology of Composite Material for Retractable Main Landing Gear Strut of a Lightweight Aircraft

Applied Sciences, 2022
The design and development of high-strength and low-weight composite landing gear struts is still a challenge in today’s world. In this study, a selection methodology for fiber-reinforced composite material for retractable main landing gear struts for ...
Muhammad Ayaz Ahmad, Hamza Rafiq, Syed Irtiza Ali Shah, Sabih Ahmad Khan, Syed Tauqeer ul Islam Rizvi, Taimur Ali Shams   +5 more
doaj   +2 more sources

Optimisation of shimmy suppression device in an aircraft main landing gear [PDF]

Journal of Physics: Conference Series, 2016
In earlier publications of landing gear shimmy analysis, efforts have concentrated on predicting the onset of shimmy instability and investigating how to stabilise shimmy-prone landing gears. Less attention has been given to the improvements of shimmy performance for a gear that is free from dynamic instability.
Li, Yuan, Jiang, Jason Zheng, Neild, Simon   +2 more
openaire   +5 more sources

Analisis Kekuatan Struktur Komposit Sandwich Pada Main Landing Gear UAV

Jurnal Teknologi Kedirgantaraan, 2023
Tricycle landing gear adalah konfigurasi landing gear pada pesawat dengan nose landing dan main landing. Analisis kekuatan komposit sandwich dengan beban impact bertujuan mengetauhi kekuatan maksimal yang dapat ditahan oleh sandwich dengan beberapa ...
Jauharul Akfiya Sudjaelan, Sahril Afandi, Endah Yuniarti   +2 more
semanticscholar   +2 more sources

Rancang Bangun Alat Peraga Ground Lock Main Landing Gear

Jurnal Teknologi Kedirgantaraan
The Landing gear is a critical component of an aircraft that supports its weight and absorbs shocks during takeoff and landing, as well as reduces air resistance during flight.
Fadli Hidirsyah, Riskha Agustianingsih, Fadli Hirdirsyah   +2 more
semanticscholar   +2 more sources

Weak links design for the main landing gear leg mount

Engineering Journal: Science and Innovation, 2023
The paper presents an overview of the main strength requirements to the typical civil aircraft landing gear design. Elements of the main landing gear leg mount on the airframe were considered in more detail.
E.I. Titov, S. A. Serebryanskiy
semanticscholar   +2 more sources