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轮胎力学特性对飞机前轮摆振的影响分析
引用本文:王光颖,孙立红. 轮胎力学特性对飞机前轮摆振的影响分析[J]. 黑龙江科技学院学报, 2003, 13(2): 38-40
作者姓名:王光颖  孙立红
作者单位:黑龙江科技学院基础部,黑龙江,鸡西,158105
摘    要:应用Smil1ey轮胎力学理论建立了轮胎力学特性模型,以该模型为基础,研究了轮胎侧向刚度和轮胎充气压力对飞机前轮摆振的影响。结果表明:轮胎侧向刚度和轮胎充气压力是影响飞机前轮摆振的重要参数,增加轮胎侧向刚度对摆振不利,增加轮胎充气压力有利于防止摆振。

关 键 词:轮胎力学特性模型 轮胎侧向刚度 前轮摆振
文章编号:1671-0118(2003)02-0038-03

The Effect Analysis of Tire Mechanical Properties on Aircraft Nose Wheel Shimmy
WANG Guangying,SUN Lihong. The Effect Analysis of Tire Mechanical Properties on Aircraft Nose Wheel Shimmy[J]. Journal of Heilongjiang Institute of Science and Technology, 2003, 13(2): 38-40
Authors:WANG Guangying  SUN Lihong
Abstract:The paper describes tire mechanical characteristics model using Smiley mechanical theory of tire. The study not only involves the influence of tire lateral stiffness and tire inflated pressure on aircraft nose wheel shimmy on the basis of the model, but also finds that tire lateral stiffness and tire inflated pressure are one key tire parameter which influences shimmy.
Keywords:tire mechanical characteristics model  tire lateral stiffness  nose wheel shimmy  
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