为了改善现有的航空弹射救生系统,提高飞行员安全逃生的成功率,提出了微爆索切割技术在航空穿盖弹射救生系统中的应用。采用非线性动力显式程序LS—DYNA3D,对有机玻璃平板元件、航空舱盖的微爆索切割过程进行了数值计算分析,得到了不同装药量下有机玻璃平板元件、航空舱盖的切割深度,对比了有机玻璃的几何形状对微爆索切割深度的影响。模拟结果表明:有机玻璃平板切割实验对航空舱盖切割实验具有一定的指导意义,研究结果也可为微爆索线性切割航空舱盖的实验设计提供依据。
In order to improve the present aviation ejection lifesaving system and enhance success possibility of safe escape,the application of Miniature Detonating Cord (MDC) on the aviation ejectionescape-system is proposed. The explosion cutting process of plexiglass (PMMA) plate and Canopy by MDC are simulated employing nonlinear dynamic explicit program LS-DYNA3D. The variation of cutting depth with charge quantities is obtained, which agrees well with the experimental result. Simulation result shows that the geometry of PMMA has slight influence on the cutting effect. This study may provide the powerful foundation for the design of the aviation ejection lifesaving system.