| 空降车-气囊系统着地缓冲过程仿真分析 |
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| 引用本文： | 洪煌杰,王红岩,郝贵祥.空降车-气囊系统着地缓冲过程仿真分析[J].装甲兵工程学院学报,2010,24(4). |
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| 作者姓名： | 洪煌杰 王红岩 郝贵祥 |
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| 作者单位： | 装甲兵工程学院,机械工程系,北京,100072 |
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| 摘 要： | 为了给空降车及其气囊的优化设计提供技术支持,采用有限元方法对空降车气囊缓冲过程进行仿真分析。计算了正常着地工况下的气囊缓冲过程,得到速度、加速度以及气囊内压等时间特性曲线。结果表明:空降车在该工况下着地速度小于3m/s,该气囊符合空降车着地的缓冲性能要求。车体加速度和冲击应力在误差许可范围内,验证了采用此种方法进行空降车气囊缓冲过程的虚拟测试是可行的。
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| 关 键 词： | 空降车 缓冲气囊 有限元方法 冲击 着地速度 |
Simulation and Analysis of Landing Cushion Process for Airborne Vehicle and Airbag |
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| HONG Huang-jie,WANG Hong-yan,HAO Gui-xiang.Simulation and Analysis of Landing Cushion Process for Airborne Vehicle and Airbag[J].Journal of Armored Force Engineering Institute,2010,24(4). |
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| Authors: | HONG Huang-jie WANG Hong-yan HAO Gui-xiang |
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| Institution: | HONG Huang-jie; WANG Hong-yan; HAO Gui-xiang(Department of Mechanical Engineering; Academy of Armored Force Engineering; Beijing 100072; China); |
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| Abstract: | In order to offer technique support to optimization design of airborne vehicle and airbag,a model of airborne vehicle and airbag is established to simulate and analyze airbag cushion process based on finite element method.Airbag cushion process under the situation of landing normally is simulated.Characteristic curve about velocity,acceleration and press are given.The landing velocity of airbag cushion is less than 3m/s under the situation of landing normally.It proves the airbag accord with the request of ... |
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| Keywords: | airborne vehicle cushion airbag finite element method impact landing velocity |
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