Track characteristic analysis system under low-frequency excitation condition
A characteristic analysis and orbit technology, applied in the field of orbit characteristic analysis system, can solve problems such as huge amount of calculation, difficult solution, low calculation efficiency, etc., and achieve the effect of simplifying calculation steps and accurate and efficient calculation.
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[0023] Example: Two degrees of freedom lumped parameter orbital model: where, M r and Ms are the equivalent para-vibration masses of rail and sleeper respectively, K p and C p are the equivalent parametric stiffness and damping of the fastener, respectively, K bf and C bf are the equivalent parametric stiffness and damping of the ballast bed and subgrade, respectively. The model can also be used to solve the supraoccipital and suboccipital pressures during the orbital vibration process.
[0024] In order to consider the impact of ballast bed vibration on the entire track vibration, a three-degree-of-freedom lumped parameter model came into being. In the model, M b is the equivalent vibration mass of the ballast bed, and K b and C b are the equivalent parametric stiffness and damping of the ballast bed respectively, K f and C f are the equivalent stiffness and damping of the subgrade, and the other parameters are the same as the two-degree-of-freedom lumped parameter mo...
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