检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:李鸣皋[1] 柳松杨[2] 柯鹏[3] 赵鑫[1] Li Minggao;Liu Songyang;Ke Peng;Zhao Xin
机构地区:[1]中国人民解放军海军总医院,北京100048 [2]中国人民解放军空军航空医学研究所,北京100053 [3]北京航空航天大学交通科学与工程学院,北京100191
出 处:《航天医学与医学工程》2017年第6期406-410,共5页Space Medicine & Medical Engineering
基 金:总后十二五重大课题(AHJ2011Z001)
摘 要:目的拦阻着舰会产生较大的持续性载荷,给飞行员的生理健康和操控工效带来不利影响,同时人体各部位的运动有可能导致它们与座舱及其内置设备碰撞,有必要评估其中的安全隐患。方法使用已建立的包含刚性座椅模型第5,50,95共3种百分位,HybridⅢ假人有限元模型以及六点式背带约束系统的多刚体-有限元混合人椅背带系统动力学模型开展动力学仿真,评估人体头部和四肢在典型拦阻着舰过程中的运动范围。结果采用文献中公开的典型拦阻着舰过程飞机座椅底部加速度曲线作为输入条件,获得典型拦阻着舰过程中3种不同百分位假人头部、手部和足部的位移数据。结论本文仿真数据可以为改进飞行员背带约束系统和优化座舱仪表布布局提供支持。Objective Sustained acceleration during arrested landing will bring adverse influences to the health and the operation performance of the pilots. During this typical process,the motion ranges of the head,the arms and the legs may be large enough to cause collision with the cockpit or the equipment. Methods Dummybelt-seat systems containing dummies of different sizes were built to investigate the motion ranges of different dummies during the typical arrested landing process. The system model contained the rigid seat model,the P5,P50 and P95 dummies,and the six-point belt system. Results Typical arrested landing acceleration at seat base from literature was used as the boundary condition for the numerical study. The motion ranges of the head,the right hand and the right feet of different dummies were obtained. Conclusion Motion ranges obtained in this research may provide basic support for the design modification of the current belt system as well as the arrangements of equipment in the cockpit.
分 类 号:R857.1[医药卫生—航空、航天与航海医学]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.28