期刊文献+
共找到1篇文章
< 1 >
每页显示 20 50 100
DESIGN OF NEW PASSIVE ADAPTIVE SHOCK ABSORBER OF LANDING GEAR AND STUDY OF ITS LANDING PERFORMANCE
1
作者 朱书华 童明波 许杰 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2009年第1期29-35,共7页
A new passive adaptive shock absorber of the landing gear with double-cavity and dual-damping is studied. Its mathematical model and the virtual prototype are established based on the dynamics simulation software ADAM... A new passive adaptive shock absorber of the landing gear with double-cavity and dual-damping is studied. Its mathematical model and the virtual prototype are established based on the dynamics simulation software ADAMS. The landing dynamic characteristics and the effect of the parameters on the proposed adaptive shock absorber are analyzed. The results show that the proposed adaptive shock absorber has the slightly better landing performance at the normal load case and much less overload at the crudely landing case than the shock absorber with single-cavity and variable orifice. It also can be concluded that the overload of the proposed adaptive shock absorber can be reduced through increasing the volumes of both cavities or decreasing the pressure of the high pressure cavity or increasing the pressure of the low pressure cavity. 展开更多
关键词 landing gear(aircraft) shock absorbers LANDING virtual prototype
在线阅读 下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部