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[an error occurred while processing this directive]脉冲发动机金属膜片式隔舱打开过程研究
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汤亮(1994-),男,陕西汉中人,硕士,研究方向:固体火箭发动机设计。 |
收稿日期: 2019-09-07
网络出版日期: 2025-05-30
Study on the Opening Progress of Pulse Separation Device in Pulse Solid Rocket Motor
Received date: 2019-09-07
Online published: 2025-05-30
汤亮 , 邓康清 , 余小波 , 郭春亮 , 秦沛文 . 脉冲发动机金属膜片式隔舱打开过程研究[J]. 弹箭与制导学报, 2020 , 40(4) : 65 -68 . DOI: 10.15892/j.cnki.djzdxb.2020.04.014
In order to optimize the structure of the metal diaphragm and to predict the opening pressure of the diaphragm in the process of dual-pulse motor design, the quantitative relationship between the structure scale and the predicted opening pressure is established according to the circular plate with bending theory and brittle fracture theory. And the opening process of the diaphragm was numerically simulated with the explicit dynamic finite element method. In addition, the ignition test was carried out. the results show that the fracture cracks extended to the preset defect grove, and the diaphragm ultimately fractured into 6 large fan-shaped fragments and countless small fragments. With the increase of the depth h and width 2c of the preset defect slot, the opening pressure on the metal diaphragm bulkhead decrease, and h has a greater impact on the opening pressure. The test value was 1.02 MPa, about 6% different from the predicted result,indicating that the pressure prediction method of diaphragm opening was feasible.
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