Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (22): 30123.doi: 10.7527/S1000-6893.2024.30123
• Reviews •
Xia LIU1, Jian XU2, Xiaoyu LI1, Huinan LIU1, Xinjing ZHANG1,3,4(), Yujie XU1,3, Haisheng CHEN1,3
Received:
2024-01-09
Revised:
2024-03-22
Accepted:
2024-04-26
Online:
2024-06-05
Published:
2024-05-14
Contact:
Xinjing ZHANG
E-mail:zhangxinjing@iet.cn
Supported by:
CLC Number:
Xia LIU, Jian XU, Xiaoyu LI, Huinan LIU, Xinjing ZHANG, Yujie XU, Haisheng CHEN. Research progress on pneumatic catapult systems[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(22): 30123.
Table 2
Comparison of the literature on compressed air ejection based on the ideal gas model
文献 | 弹射方式 | 基本参数 | 弹射性能 | 研究特点 | |||
---|---|---|---|---|---|---|---|
气源压力/MPa | 气源体积/m3或弹射筒径/m | 弹射行程/ m | 弹射 质量/ kg | 最大弹射速度/(m∙s-1) | |||
[ | 筒式 | 34~36 | 0.1 | 0.9 | 4 | 121 | 关注了气源压力、泄流面积以及弹射长度对弹射性能的影响,有试验结果验证且趋势一致,但试验与仿真数据值偏差略大 |
[ | 筒式 | 25~35 | 0.2~0.32 | <12 | 200 | 178(泄漏) | 考虑了泄漏带来的能量损耗 |
[ | 筒式 | <0.5 | 0.79~0.88 | 25 | 考虑了初始温度的影响 | ||
[ | 筒式 | 2 | 450 | 100 | 57 600 | 95.73 | 考虑了发射阀全开时间的影响,并对弹射过程中的气室温度变化和质量流量进行了研究;但是在理论研究的基本参数取值上过于理想化,未考虑实际应用中的实现难度 |
[ | 筒式 | 0.5 | 1 | 5 | 6.336 | 74 | 已在理论研究指导下搭建弹射原理实验台并完成试验验证 |
[ | 筒式 | 1.8 | 0.137 | 0.04 | 4.5 | 52 | 已试制弹射样机并经某巡飞无人机发射试验验证 |
[ | 筒式 | 0.8 | 0.007 | 0.7 | 2 | 14.9 | 对试制样机开展了不同部署发射方式下的试验 |
[ | 筒式 | 0.8 | 0.025 | 1.03 | 7 | 33.99 | 基于试验验证的仿真模型完成了改进版粒子优化算法研究,提供了一种可靠的优化方法 |
[ | 导轨式 | 2 | 0.08 | 6.2 | 100 | <40 | 考虑了弹射角度,并将各参数对弹射过程运动过载的影响进行了详细分析,有试验结果验证 |
[ | 导轨式 | 4~18 | 0.04~0.20 | 10 | 80 | 49.26 | 将气罐变化温差也纳入考虑并作为发射性能的衡量参数进行研究 |
[ | 导轨式 | 1 | 0.045 | 1.75 | 25 | 21 | 开发了一种用于根据无人机需求来确定各类弹射器尺寸的仿真工具,并对其执行模块进行摩擦和粘滞阻尼块以及硬止动块设置,可用于模拟滑车制动 |
[ | 导轨式 | 0.39~0.59 | 0.08 | 20~30 | 33.1 | 考虑了滑轮组受力及其转动惯量等关键参数对发射过程动态特性的影响 | |
[ | 导轨式 | 0.6~0.8 | 基于工质流经气动元件的气流声导系数及临界压比研究实现发射阀响应时间的优化控制 | ||||
[ | 导轨式 | 0.8 | 0.36 | 10.2 | 170 | 32.5 | 研究了滑车复位阶段的运动特性 |
[ | 导轨式 | 10 | 0.1 | 1 | 120 | 32 | 研究了滑车缓冲阶段运动特性 |
[ | 导轨式 | 0.2~1.0 | 10~30 | 12 | 研究了水下压缩空气弹射系统特性 |
Table 3
Initial parameter settings for CO2 ejection models in the literature[52,54-56]
参数 | 数值 | |||
---|---|---|---|---|
文献[ | 文献[ | 文献[ | 文献[ | |
弹射体质量/kg | 2 000 | 1 000 | 500 | 2 000 |
高压室压力/MPa | 200 | |||
高压室温度/K | >800 | 695 | 320 | 350 |
高压室容积/m³ | 0.004 | 0.01 | 0.1 | |
低压室压力/MPa | 0.1 | 0.1 | 0.1 | 0.1 |
低压室温度/K | 293.15 | 293.15 | 300 | 300 |
低压室容积/m³ | 0.04 | 0.04 | 0.1/0.5/1.0 | |
弹射行程/m | 22.71(最佳发射状态下) | |||
阀门直径/m | 0.015 | 0.015 | 0.1 | 0.04/0.06/0.08/0.1 |
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