摘要
对于火箭弹来说,引信解除保险可利用的环境力极其有限,其中,利用燃气动力作为引信第二环境力解除保险是目前众多科研工作者研究的一项重要内容。然而,对于不同的火箭弹,其火箭发动机燃烧室可提供的燃气压力是不同的,因此,燃气动力解除保险执行机构的设计也必须针对不同弹种进行,其通用化程度很低。本文设计了一种稳压装置并制作出该装置实验模型样机,通过MAF风洞实验证明了该方案的可行性,为众多科研工作者提供了一个可行的思路。
For rocket projectile, it is extremely limited to remove the fuze insurance by means of environmental force. In which, to use gas power as second environmental force of fuze to remove the insurance is an important research content that the numerous researchers are studied in it. However, for different rocket projectile, the fuel gas pressure provided by its rocket engine combustion chamber is different, accordingly the design of insurance actuator by gas dynamic remove must also be designed to aim at different species, and the degree of its generalization is very low. This paper proposed that it designed a voltage stabilizer, and made the device of experimental MAF prototype. Through the test of experimental model wind tunnel, it validated the feasibility of this scheme. It provides a feasible thinking for scientific research.
出处
《四川兵工学报》
CAS
2011年第11期27-28,共2页
Journal of Sichuan Ordnance
关键词
引信
解除保险
执行机构
稳压装置
fuse
redundancy insurance
actuating mechanism
voltage stabilizer
