Results 41 to 50 of about 106,651 (339)

Theoretical Model of the Methodology of Landing Gear Bracket Design Taking into Account the Adjusted Calculation for Shear Bolt Design [PDF]

open access: yesE3S Web of Conferences, 2023
The subject of this paper is the methodology of main landing gear (MLG) design, in particular, the algorithm. The new algorithm considered in this paper is intended for designing modern structures of the MLG using a large number of methods of ...
Titov Egor, Serebryansky Sergey
doaj   +1 more source

Investigation of gear walk suppression while maintaining braking performance in a main landing gear [PDF]

open access: yesAerospace Science and Technology, 2019
Abstract In this paper, a nonlinear dynamic landing gear model considering the influence of the coupling of the shock absorber stroke variation and the landing gear longitudinal motion with an anti-skid PID braking control system that captures gear walk is established.
Yin, Qiaozhi   +3 more
openaire   +3 more sources

Effects of Freeplay on Dynamic Stability of an Aircraft Main Landing Gear [PDF]

open access: yes, 2013
A study is made into the occurrence of shimmy oscillations in a dual-wheel main landing gear. Nonlinear equations of motion are developed for the system, and various effects are considered, including gyroscopic coupling, nonlinear tire properties ...
Howcroft, Chris   +3 more
core   +2 more sources

Linear and Nonlinear Models for Drop Simulation of an Aircraft Landing Gear System with MR Dampers

open access: yesActuators, 2023
In this study, our focus is on the drop test simulation of an MR (Magnetorheological) damper-based main landing gear (MRMLG), aiming to explore multi-degree-of-freedom (DOF) dynamic models during aircraft landing. Three different 6-DOF dynamic models are
Byung-Hyuk Kang   +4 more
doaj   +1 more source

Effect of Bolt Hole Size on Static Stress and Fatigue Life of UAV Main Landing Gear Using Numerical Simulation

open access: yes, 2021
Currently, the use of Unmanned Aerial Vehicle (UAV) or Drone for various applications in science and engineering has increased significantly. One of the essential components of a UAV aircraft is the landing gear which plays an important role during take ...
Lasinta Ari Nendra Wibawa
semanticscholar   +1 more source

Dynamics Simulation Research on Tricycle Landing Gear UAV During Taxiing and Take-off Phase

open access: yesHangkong gongcheng jinzhan, 2018
The UAV taxiing and take-off phase is a dangerous phase in the flight process, during which the force of UAV is very complex and the dynamic characteristics is different from that in the air.
Zhang Lin, Gong Xiying, Pang Junfeng
doaj   +1 more source

Computational Evaluation of Aerodynamic Loading on Retractable Landing-Gears

open access: yesAerospace, 2020
Computational fluid dynamics is employed to evaluate the mean aerodynamic loading on the retractable landing-gears of a regional transport commercial aircraft. The mean turbulent flow around simplified landing-gear systems including doors is simulated by
Giuliano De Stefano   +3 more
doaj   +1 more source

MODIFICATION METHOD OF STRAIN-LIFE CURVES UNDER DIFFERENT SURFACE CONDITIONS OF COMPONENTS (MT)

open access: yesJixie qiangdu, 2022
Based on the practical problem of fatigue life prediction of landing gear, the fatigue life prediction model of landing gear components with surface treatment was studied.
DUAN Heng   +4 more
doaj  

Simulation analysis on semi-active control drop dynamics of whole aircraft landing gear

open access: yesHangkong gongcheng jinzhan, 2023
The application of semi-active control technology on landing gear is mostly limited to single or magnetorheological landing gear. The research on the whole aircraft is more valuable for the practical application of semi-active control.
REN Panting, XU Feng
doaj   +1 more source

Aircraft tire temperature at touchdown with wheel prerotation [PDF]

open access: yes, 2017
Because of the skidding process that occurs when a heavy aircraft’s main landing gear tires touchdown, since the 1940s, a number of ideas have been patented to improve tire safety and decrease the substantial wear and smoke during every landing by ...
Abdurrhman A. Alroqi   +4 more
core   +1 more source

Home - About - Disclaimer - Privacy