Results 1 to 10 of about 783 (209)
Investigation into the Interaction of Nose Landing Gear and Fuselage Dynamics [PDF]
Pilots may experience vibrations in the cockpit during ground maneuvers because of energy being transferred from the nose landing gear to the fuselage. This indicates that the fuselage dynamics could also have an effect on the dynamics of the gear. To study this interaction, a mathematical model of a nose landing gear coupled to a fuselage model with ...
Mark Lowenberg +2 more
exaly +5 more sources
Selection Methodology of an Electric Actuator for Nose Landing Gear of a Light Weight Aircraft
Landing gear system of an aircraft enables it to take off and land with safety and comfort. Because of the horizontal and vertical velocity of aircraft, upon landing, the complete aircraft undergoes different forcing functions in the form of the impact ...
Taimur Ali Shams +2 more
exaly +4 more sources
Influence of Nose Landing Gear Torsional Damping on the Stability of Aircraft Taxiing Direction
The design of the nose landing gear (NLG) torsional damping is very important to avoid the taxiing vibration of the aircraft. On the one hand, increasing the torsional damping can suppress the nose wheel shimmy.
Bingyan Jiang
exaly +4 more sources
In the field of civil aviation, the nose landing gear is a critical component that is prone to damage during taxiing. With the advent of new technologies such as towing taxi-out and hub motors, the nose landing gear faces increasingly complex operational
Jiahao Qin, Qiwei Lin
exaly +4 more sources
Landing Impact Load Analysis and Validation of a Civil Aircraft Nose Landing Gear
Landing impact load design is essential, but the process has rarely been fully described, and some designers have even neglected the differences between wheel-axle and ground-contact loads, as well as loads in the longitudinal direction, especially in ...
Wenbin Liu, Youshan Wang, Yuchen Ji
doaj +3 more sources
Research on the nose landing gear of a military training aircraft [PDF]
This paper presents the analysis of the landing gear configurations and the proposal of a solution for a military training aircraft. The paper presents both landing gears: nose and main because they are inextricably linked.
Ilie NICOLIN, Bogdan Adrian NICOLIN
doaj +2 more sources
A Deep Learning On-Board Health Monitoring Method for Landing Gear Shock-Absorbing Systems [PDF]
This paper proposed a deep learning on-board health monitoring method for landing gear shock-absorbing systems based on dynamic responses during landing. A deep learning model is developed to conduct health monitoring for faults in shock absorbers.
Chunsheng Li, Wang Chen, Wenfeng Qin
doaj +2 more sources
Tire stiffness is one of the important parameters of tire dynamics model. The influence law of tire stiffness on the shimmy of large civil aircraft nose landing gear can provide reference for the anti-shimmy design of large civil aircraft nose landing ...
FENG Guang +5 more
doaj +1 more source
Study on stiffness and shimmy stability of strut-type nose landing gear system
System stiffness (longitudinal, lateral, and torsional stiffness) is a meaningful index for strut nose landing gear design.It arises from profound significance to explore the influence law of system stiffness on shimmy stability for the anti-shimmy ...
FENG Guang +5 more
doaj +1 more source
Preliminary calculation of the landing gear of a military training aircraft [PDF]
The paper presents a preliminary calculation method, which is easy to apply for pre-dimensioning the landing gear. Preliminary calculation of the landing gear includes estimating the loads on landing and determining the position of the nose landing gear ...
Ilie NICOLIN, Bogdan Adrian NICOLIN
doaj +1 more source

