Dynamic Behavior on Emergency Landing of Light Aircraft with Occupant Restraint System

摘要：

　　The finite element model was established on a certain type of amphibious light aircraft and a dummy with restraint system.Using large dynamic finite element analysis software LS-DYNA numerical simulation was processed to study this aircrafts emergency landing procedure.This paper investigated the dynamic response of the dummy and head injury criterion (HIC) value etc.The results provide certain reference for aircraft emergency landing safety design.

关键词： Restraint System Dummy Airplane Impact Finite Element

作者: Lin Yin Luo Yan Bin He Xuan Liu Xiao Hu Yao

作者单位: Northwestern Polytechnical University,Xian,710072,P.R.C School of Civil Engineering and Transportation,South China University of Technology,Guangzhou,510640 School of Civil Engineering and Transportation,South China University of Technology,Guangzhou,510640

会议类型: 国际会议

会议名称: the 2012 International Conference on Manufacturing Engineering and Automation (2012年制造工程与自动化国际会议(ICMEA2012))

会议地点: 广州

会议语种:英文

页码: 2513-2517

在线出版日期: 2012-11-16（万方平台首次上网日期，不代表论文的发表时间）