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:丰志伟[1] 张国斌 张青斌[1] 王璐 周喜生 FENG Zhiwei;ZHANG Guobin;ZHANG Qingbin;WANG Lu;ZHOU Xisheng(College of Aeronautics and Astronautics,National University of Defense Technology,Changsha 410073,China;Aviation Key Laboratory of Science and Technology on Life-Support Technology,Xiangyang 441003,China;AVIC Aerospace Life-Support Industries,Ltd.,Xiangyang 441003,China)
机构地区:[1]国防科技大学空天科学学院,湖南长沙410073 [2]航空防护救生技术航空科技重点实验室,湖北襄阳441003 [3]航空工业航宇救生装备有限公司,湖北襄阳441003
出 处:《国防科技大学学报》2019年第6期44-49,共6页Journal of National University of Defense Technology
基 金:国家自然科学基金资助项目(11772353);航空科学基金资助项目(20152988004)
摘 要:为了改善救生伞背带分系统的安全性,建立降落伞-背带-假人系统的动力学模型,分析背带及脱离锁参数对假人质心过载的影响。针对救生伞假人高速开伞空投试验,采用多体动力学方法建立降落伞、背带脱离锁和假人的十五自由度动力学模型;采用半质量-阻尼弹簧模型建立背带模型,连接降落伞、脱离锁和假人;利用实测过载计算降落伞开伞力。利用所建立的动力学模型仿真典型状态下假人和背带的动力学响应,验证所建立模型的合理性。分析了脱离锁位置、背带松紧程度、背带材料特性对假人质心最大过载的影响,可用于指导背带设计以及确定最佳的背带脱离锁位置。To improve the safety of the webbing subsystem of the survival parachute, the dynamic model of parachute-webbing-dummy system was developed, and the load of the center of mass of dummy was analyzed for the varied parameters of webbing and detachment lock. For the airdrop test of dummy in the high speed, the fifteen degree of freedom dynamic model for the parachute, detachment lock and dummy was developed by using the multi-body dynamic method. The webbing was modeled by semi-mass-damping model to join the parachute, detachment lock and dummy. The parachute opening force was calculated by using the load of test. The dynamic process of dummy and the webbing for the typical condition was simulated by using the proposed model, and the reasonableness of the model was verified. The effect of the load of the dummy mass center was analyzed for the position of detachment lock, the length of webbing, and the property of the webbing material. The results of the analysis can be used for the design of the webbing and the determination of the position of the detachment lock.
分 类 号:V244.2[航空宇航科学与技术—飞行器设计]
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:216.73.216.7