...
首页> 外文期刊>International Journal of Technology >Analysis of the Static Behavior of a New Landing Gear Model based on a Four-bar Linkage Mechanism
【24h】

Analysis of the Static Behavior of a New Landing Gear Model based on a Four-bar Linkage Mechanism

机译:基于四杆连杆机制的新着陆齿轮模型的静态行为分析

获取原文
   

获取外文期刊封面封底 >>

       

摘要

A landing gear model using a four-bar linkage mechanism is proposed in this study. The simulation study was conducted to evaluate the effect of the link dimension variation and coil spring constant on the equivalent stiffness and static deflection of the landing gear. The simulation results show that increasing the landing gear dimension affects the static deflection of the landing gear. However, the linear stiffness of the landing gear system is not much affected by the landing gear dimension variation. Furthermore, the landing gear stiffness characteristic is nonlinear for large landing gear displacement.
机译:在本研究中提出了一种使用四条键合理的起落架模型。进行了仿真研究以评估连杆尺寸变化和螺旋弹簧常数对着陆齿轮的等效刚度和静偏转的影响。仿真结果表明,增加着陆齿轮尺寸影响着陆齿轮的静偏转。然而,着陆齿轮系统的线性刚度并不多于着陆齿轮尺寸变化的影响。此外,着陆齿轮刚度特性是大型着陆齿轮位移的非线性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号