Results 21 to 30 of about 2,798 (215)
Structure design and breakaway failure analysis of fuse-pin for civil main landing gear
The landing gear should be able to achieve safe and rapid separation from the aircraft body under overload conditions. To clarify the effect of breakaway groove on the breakaway load of emergency fuse-pin for civil main landing gear, a series of FEM ...
FU Liang +5 more
doaj +1 more source
Analysis of aerodynamic and aeroacoustics of full scale landing gear
The aerodynamic noise of a landing gear is an important source of airframe noise. The analysis of its noise characteristics plays an important role in the design of a low-noise landing gear.
TIAN Siyuan +5 more
doaj +1 more source
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 +5 more
doaj +1 more source
Nose Landing Gear Shimmy Analysis with Variable System Stiffness Under Time-Varying Load
Vertical 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
doaj +1 more source
Dynamic Fatigue Tests Of Landing Gears
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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Preliminary Estimation Methods for the Definition of the Landing Gear [PDF]
The landing gear of an aircraft is an important part of the aircraft structure. The landing and the taking off are most critical parts of a flight mission.
Daniela BARAN +2 more
doaj +1 more source
Research on the Influence of Temperature on the Cushioning Performance of Oil-air Landing Gear
The oil characteristics and inflation pressure inside the oil-air shock absorber will change with the ambient temperature,which will affect the cushioning performance of landing gear.In order to explore the effect of temperature on the cushioning ...
HU Rui, MU Rangke, SONG Dejun, CHEN Yi
doaj +1 more source
Design and Research on Landing Gear Overall Parameters of Pusher Propeller Reconnaissance/Strike UAV
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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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
The aircraft landing gear system is vital in ensuring the aircraft’s functional completeness and operational safety. The mechanical structures of the landing gear must withstand significant operational forces, including repeated high-intensity impact ...
Kailun Deng +4 more
doaj +1 more source

