Modeling and analysis of aircraft landing nonlinear dynamics for tire safety assessment is formulated in this paper. Firstly, an aircraft landing process is reviewed to introduce the principle of tire rotation, friction coefficients and random pavement profiles. Secondly, a tire of a main landing gear is simplified to be a rim and a belt ring connected by three spring-damping elements. The traditional 1/4 vehicle model is generalized to construct a new seven-degree-of-freedom single-wheel landing dynamic model in order to describe the vertical, longitudinal and circumferential motions of the tire during different landing phases. The influence of braking force, lift and pavement roughness are considered. Thirdly, numerical analysis of the aircraft landing process is carried out to obtain the variation trend of tire deformation, load and friction at different phases, as well as the movement state of the aircraft fuselage and the tire. Finally, tire safety is evaluated through cumulative tread wear and transient landing load. The former is related with airworthiness requirements on maximum allowable wear depth and replacement cycles, while the latter is compared with structural load limits during touchdown. The results demonstrate that high landing speeds and low-friction surfaces markedly accelerate wear progression, while the overall numerical predictions remain consistent with established physical trends, confirming the validity of the proposed safety assessment method. The proposed methodology addresses a new viewpoint to employ the aircraft landing nonlinear dynamics to carry out tire safety evaluation and maintenance planning in civil aviation.

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