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本文针对某大型飞机前起落架进行了缓冲器参数的理论计算,并用落震动力学仿真进行验证分析。结果表明:理论计算与落震仿真结果基本吻合,该缓冲参数的计算方法可应用于工程实践。
In this paper, the theoretical calculation of the damper parameters for the front landing gear of a large aircraft has been carried out and the verification has been carried out with the falling-ground dynamics simulation. The results show that the theoretical calculation is basically consistent with the simulation results of off-shock. The calculation method of the cushioning parameters can be applied to engineering practice.