首页|航行体发射过程中围腔内压力脉动特性研究

航行体发射过程中围腔内压力脉动特性研究

扫码查看
针对水下航行体垂直发射过程中,发射系统高压腔与密封环围腔连通,导致高压气体涌入围腔内引发压力脉动这一问题.采用有限元仿真的方法对其进行分析,探究了高压腔内发射压力、围腔长度和航行体尾部倒角等因素对压力脉动的影响规律.仿真结果表明,高压气体进入围腔内撞击到第二道密封环后发生发射并回流,使整个发射系统受到逐渐衰弱的正弦周期性冲击.随着航行体的进一步运动压力脉动的幅值逐渐降低,整个压力脉动过程的最大峰值可达高压腔内发射压力的1.45倍;增加高压腔内发射压力,围腔内压力脉动峰值增加,峰值到达时间提前;增加围腔长度,压力脉动峰值增加,峰值到达时间延后;航行体尾部存在倒角时,围腔内压力脉动峰值到达时间提前.
Research on pressure pulsation characteristics in the annular cavity during the launch of a vehicle
During the vertical launch process of underwater vehicles,a problem that when the high-pressure chamber of the launch system is connected to the sealed annular cavity,causing high-pressure gas to surge into the cavity and generate pressure pulsations arises.In this study,the finite element simulation method was used to analyze this problem and investig-ate the effects of factors such as launch pressure in the high-pressure chamber,length of the annular cavity,and chamfer at the tail of the vehicle on pressure pulsations.The simulation results indicate that when high-pressure gas enters the annular cavity and impacts the second seal ring,it undergoes launch and back-flow,resulting in gradually weakening sinusoidal peri-odic impacts on the entire launch system.As the vehicle moves further,the amplitude of pressure pulsations gradually de-creases,and the maximum peak value in the entire pressure pulsation process can reach 1.45 times the launch pressure in the high-pressure chamber.Increasing the launch pressure in the high-pressure chamber leads to an increase in the peak of pres-sure pulsations in the annular cavity and an earlier arrival time for the peak.Increasing the length of the annular cavity leads to an increase in the peak value of pressure pulsations and a delayed arrival time for the peak.When there is a chamfer at the tail of the vehicle,the arrival time of the peak of pressure pulsations in the annular cavity is advanced.

underwater vehiclevertical launchannular cavitypressure pulsation

周志、马永、袁卫锋

展开 >

西南科技大学制造过程测试技术教育部重点实验室,四川绵阳 621010

中国船舶集团有限公司第七一三研究所,河南郑州 450015

水下航行体 垂直发射 围腔 压力脉动

2024

舰船科学技术
中国舰船研究院,中国船舶信息中心

舰船科学技术

CSTPCD北大核心
影响因子:0.373
ISSN:1672-7649
年,卷(期):2024.46(17)