Design and Research on Landing Gear Overall Parameters of Pusher Propeller Reconnaissance/Strike UAV
Hangkong gongcheng jinzhan, 2022 The existing specifications and requirements for the overall layout parameter design of aircraft landing gear are mainly applicable to traditional fighters.If the landing gear of pusher propeller reconnaissance/strike unmanned aerial vehicle(UAV)is ...
ZHENG Yongfeng, SHEN Junyan
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Influence of Variable Side-Stay Geometry on the Shimmy Dynamics of an Aircraft Dual-Wheel Main Landing Gear [PDF]
, 2013 Commercial aircraft are designed to fly but also need to operate safely and efficiently as vehicles on the ground. During taxiing, take-off, and landing the landing gear must operate reliably over a wide range of forward velocities and vertical loads ...
Howcroft, Chris +3 more
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Nose Landing Gear Shimmy Analysis with Variable System Stiffness Under Time-Varying Load
AerospaceVertical load fluctuations alter nose landing gear (NLG) system stiffness and complicate shimmy dynamics. Based on the full-scale NLG static stiffness test data, the relationship between shock absorber stroke and system stiffness was fitted, and a ...
Yiyao Jiang +3 more
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Research Progress on the Effect of Structural Clearance of Aircraft Landing Gear on Shimmy Stability
Hangkong gongcheng jinzhan, 2022 As one of the main factors affecting the shimmy stability of aircraft in high speed rolling,the structural clearance of landing gear determines the safety and comfort of aircraft rolling.In this paper,the existing form of landing gear structural ...
XIANG Zongwei +5 more
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Design and Manufacture of Composite Landing Gear for a Light Unmanned Aerial Vehicle
Applied Sciences, 2021 Unmanned aerial vehicles (UAVs) have become popular for military applications as well as for use in structural inspection, weather monitoring, and festival demonstrations.
Yen-Chu Liang +3 more
semanticscholar +1 more source
A Supervised Neural Network Control for Magnetorheological Damper in an Aircraft Landing Gear
Applied Sciences, 2021 This paper adopts an intelligent controller based on supervised neural network control for a magnetorheological (MR) damper in an aircraft landing gear.
Q. Luong +3 more
semanticscholar +1 more source
Dynamic Fatigue Tests Of Landing Gears
Fatigue of Aircraft Structures, 2020 Landing gears are one of the main components of an aircraft. The landing gear is used not only during take-off and landing but also, in most cases, during ground manoeuvres.
Skorupka Zbigniew
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Advanced 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
Analysis of spin-up and spring back loads of landing gear based on slip rate
Hangkong gongcheng jinzhanThe landing gear spin-up and spring back loads are the important part of the aircraft landing load. In order to effectively analyze the spin-up and spring back loads of the landing gear in the preliminary design stage，the two-wheel strut landing gear ...
WU Ming +3 more
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Application of tire dynamics to aircraft landing gear design analysis [PDF]
, 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.
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