首页|运载火箭破裂膜片压敏结构飞秒激光加工试验研究

运载火箭破裂膜片压敏结构飞秒激光加工试验研究

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针对运载火箭纯铝型破裂膜片进行飞秒激光加工膜片压敏结构和性能试验研究,分析了激光功率、扫描层数、刻痕宽度等因素对膜片性能的影响规律.结果显示,采用飞秒激光加工可实现膜片刻痕深度方向的线性去除,且对膜片基材性能无显著影响,膜片性能与剩余厚度之间具有良好的线性关系.适当增加膜片刻痕底部宽度,能有效提高膜片性能的稳定性,研究成果有利于促进运载火箭增压输送系统稳定性与可靠性的提升.
Research on Femtosecond Laser Processing Experiment for Pressure-sensitive Structure of Launch Vehicle Rupture Diaphragm
Femtosecond laser processing experiments on the pressure-sensitive structure and performance of the aluminum rupture diaphragm were carried out,and the effects of laser power,scanning layer and notch width on the performance of the diaphragm were analyzed.It was found that femtosecond laser processing can achieve linear removal of the notch and the femtosecond laser machining has no significant effect on the properties of the diaphragm substrate,and there is a linear relationship between the rupture pressure and the residual thickness.Properly increasing the bottom width of the notch can effectively improve the stability of the performance of the diaphragm,and the result are conducive to improving the stability and reliability of booster conveying system for launch vehicles.

launch vehiclerupture diaphragmfemtosecond laserpressure-sensitive structure

徐世俊、刘晓、匡以武、陈恺、陶沙

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上海航天设备制造总厂有限公司,上海 200245

中国科学院西安光学精密机械研究所,陕西 西安 710119

运载火箭 破裂膜片 飞秒激光 压敏结构

2024

电加工与模具
苏州电加工机床研究所 中国机械工程学会特种加工分会

电加工与模具

CSTPCD北大核心
影响因子:0.285
ISSN:1009-279X
年,卷(期):2024.(6)