Abstract:In ground vehicles, tire consumption is in general mainly due to the mileage covered, and in fact the life span of tires, at least in common situations, is rather long. In the aeronautical context, and for aircraft in particular, instead, tire consumption plays a crucial role in determining the maintenance costs. This is due to the fact that, in aircraft braking, nearly all maneuvers activate the anti-skid controller, which remains in use for long time intervals. In ground vehicles, instead ABS systems are usu… Show more
“…In [6], the landing gear strut was simplified to a torsional spring-damping system in the longitudinal direction, and a detailed gear walk vibration mechanical model was established by using Lagrange's second-type equation. To characterize the effect of landing gear walk on aircraft ABS, a simplified landing gear coupling vibration analysis model based on landing gear walk angle is established in [7][8]. The above study directly simplified the landing gear walking vibration to a low-order vibration system, and the boundary conditions of the simplified model were not analyzed.…”
Currently, there is not enough research on the mechanism that causes the vibration of landing gear walk when an aircraft anti-skid brake is activated. This paper aims to provide a comprehensive analysis of the characteristics of the landing gear walk and the associated research. It shows that the walk vibration is caused by a cantilever beam’s tip mass and that the study should focus on the landing gear walk’s characteristics. Firstly, according to the transverse vibration theory of cantilever beams, the transcendental equation for calculating the natural frequency of the landing gear can be obtained. After that, the influence of the structural parameters of the landing gear on each order of the natural frequency is analyzed. To ensure that the conclusions derived are applicable to all landing gear structures, the structural parameters are selected to cover both small unmanned aerial vehicles and large civil aircraft. Finally, the influence of the axial pressure of the landing gear on its inherent frequency is analyzed.
“…In [6], the landing gear strut was simplified to a torsional spring-damping system in the longitudinal direction, and a detailed gear walk vibration mechanical model was established by using Lagrange's second-type equation. To characterize the effect of landing gear walk on aircraft ABS, a simplified landing gear coupling vibration analysis model based on landing gear walk angle is established in [7][8]. The above study directly simplified the landing gear walking vibration to a low-order vibration system, and the boundary conditions of the simplified model were not analyzed.…”
Currently, there is not enough research on the mechanism that causes the vibration of landing gear walk when an aircraft anti-skid brake is activated. This paper aims to provide a comprehensive analysis of the characteristics of the landing gear walk and the associated research. It shows that the walk vibration is caused by a cantilever beam’s tip mass and that the study should focus on the landing gear walk’s characteristics. Firstly, according to the transverse vibration theory of cantilever beams, the transcendental equation for calculating the natural frequency of the landing gear can be obtained. After that, the influence of the structural parameters of the landing gear on each order of the natural frequency is analyzed. To ensure that the conclusions derived are applicable to all landing gear structures, the structural parameters are selected to cover both small unmanned aerial vehicles and large civil aircraft. Finally, the influence of the axial pressure of the landing gear on its inherent frequency is analyzed.
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