| 发射阀改进后气动发射装置弹道仿真分析 |
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| 引用本文： | 洪刚,吴百海,田烈余. 发射阀改进后气动发射装置弹道仿真分析[J]. 液压气动与密封, 2011, 31(4) |
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| 作者姓名： | 洪刚 吴百海 田烈余 |
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| 作者单位： | 广东工业大学机电工程学院,广东广州,510090 |
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| 摘 要： | 根据气动不平衡式发射装置的内弹道理论建立了该发射装置缓冲面积调节器的流通面积计算数学模型,在仿真初始条件给定的条件下,重点分析了鱼雷质量和发射管长度对于鱼雷弹道的影响.
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| 关 键 词： | 发射阀 鱼雷 仿真 内弹道 |
Research on the Incipient Trajectory of the Improved Gas Launching Device |
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| HONG Gang,WU Bai-hai,TIAN Lie-yu. Research on the Incipient Trajectory of the Improved Gas Launching Device[J]. Hydraulics Pneumatics & Seals, 2011, 31(4) |
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| Authors: | HONG Gang WU Bai-hai TIAN Lie-yu |
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| Affiliation: | LI Zhi-hua ZHOU Kai-hua YAN Yong WU Ji-wei (Weapon Department,Bengbu Navy Petty Officer Academy,Bengbu 233012,China) |
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| Abstract: | The interior trajectory model is established.The method and mathematical models have been tested on the compared simulation design of the shape of the aperture of an old launching valve,and proved its availability for the optimal design of the launching valve. The influence of the torpedo weight and the launch tube to the incipient trajectory is analyzed importantly. |
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| Keywords: | launching device torpedo simulation incipient trajectory |
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