摘要以某飞机为原型,首先基于VC++设计了起落架缓冲器的充填参数计算程序,可计算前起与主起单腔定油孔型和单腔变油孔型支柱式起落架的缓冲器设计参数,然后通过VC++实现缓冲器落震性能分析算法,对缓冲器进行了落震分析,得到了起落架缓冲器的功量图曲线。最后与A dam s/A ircraft进行的起落架缓冲器的落震仿真分析结果进行对比,结果说明程序实现较好,在缩短缓冲器初步设计周期的方面有一定工程应用价值。
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