Results 51 to 60 of about 106,651 (339)

Development of a Morphing Landing Gear Composite Door for High Speed Compound Rotorcraft

open access: yesAerospace, 2020
In the framework of fast rotorcraft, smoothness and flushness of external aerodynamic surfaces present challenges for high-speed conditions, where aerodynamics is the driver of helicopter performance.
Antonio Chiariello   +5 more
doaj   +1 more source

Influence of Nose Landing Gear Torsional Damping on the Stability of Aircraft Taxiing Direction

open access: yesAerospace, 2022
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.
Yiyao Jiang   +5 more
doaj   +1 more source

Application of tire dynamics to aircraft landing gear design analysis [PDF]

open access: yes, 1983
The tire plays a key part in many analyses used for design of aircraft landing gear. Examples include structural design of wheels, landing gear shimmy, brake whirl, chatter and squeal, complex combination of chatter and shimmy on main landing gear (MLG ...
Black, R. J.
core   +1 more source

Multimodal Locomotion in Insect‐Inspired Microrobots: A Review of Strategies for Aerial, Surface, Aquatic, and Interfacial Motion

open access: yesAdvanced Robotics Research, EarlyView.
This review identifies key design considerations for insect‐inspired microrobots capable of multimodal locomotion. To draw inspiration, biological and robotic strategies for moving in air, on water surfaces, and underwater are examined, along with approaches for crossing the air–water interface.
Mija Jovchevska   +2 more
wiley   +1 more source

Intelligent Control Based on a Neural Network for Aircraft Landing Gear with a Magnetorheological Damper in Different Landing Scenarios

open access: yesApplied Sciences, 2020
A typical oleo-pneumatic shock-absorbing strut (classic traditional passive damper) in aircraft landing gear has a metering pin extending through the orifice, which can vary the orifice area with the compression and extension of the damper strut. Because
Quoc Viet Luong   +2 more
doaj   +1 more source

Automated packing and piping in an Airbus A320 main landing gear bay: an industrial development case study

open access: yesCEAS Aeronautical Journal
The packing of given hydraulic equipment together with the hydraulic piping is a challenging design task. Both the hydraulic domain and the geometry domain are highly intercoupled as the packing determines the exact location of the connection points and ...
Moritz Neumaier   +5 more
semanticscholar   +1 more source

Gait Analysis of Pak Biawak: A Necrobot Lizard Built using the Skeleton of an Asian Water Monitor (Varanus Salvator)

open access: yesAdvanced Robotics Research, EarlyView.
Pak Biawak, a necrobot, embodies an unusual fusion of biology and robotics. Designed to repurpose natural structures after death, it challenges conventional boundaries between nature and engineering. Its movements are precise yet unsettling, raising questions about sustainability, ethics, and the untapped potential of biointegrated machines.
Leo Foulds   +2 more
wiley   +1 more source

Materials Selection of Optimized Titanium Alloys for Aircraft Applications [PDF]

open access: yesMaterials Research, 2018
The aim of the present work was to explore the correlation between the physical metallurgy of titanium alloys and its main attributes to select optimized materials for structural aircraft applications in the landing gear beam.
Renato Altobelli Antunes   +2 more
doaj   +2 more sources

Assessing the impact of the slopes on runway drainage capacity based on wheel/path surface adhesion conditions

open access: yesAviation, 2021
Aircraft braking distance is dependent on the friction between the main gear tires and runway pavement surface.Pavement texture, which is divided into macrotexture and micro-texture, has a noticeable effect upon friction, especially when the surface is ...
Misagh Ketabdari   +2 more
doaj   +1 more source

Vibration Response Analysis of a Main Landing Gear System for High In-Flight Dynamic Loadings

open access: yesJournal of Physics: Conference Series
The prediction of aircraft vibrations is necessary for identifying possible design optimization points of each on-board system. In this context, the authors investigated the dynamic response of a Main Landing Gear (MLG) conceived for a fast helicopter ...
Maurizio Arena   +7 more
semanticscholar   +1 more source

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