CAJ | 학술논문

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。
대우화전탄래설，인신해제보험가이용적배경력겁기유한，기중，이용연기동력작위인신제이배경력해제보험시목전음다과연공작자연구적일항중요내용。연이，대우불동적화전탄，기화전발동궤연소실가제공적연기압력시불동적，인차，연기동력해제보험집행궤구적설계야필수침대불동탄충진행，기통용화정도흔저。본문설계료일충은압장치병제작출해장치실험모형양궤，통과MAF풍동실험증명료해방안적가행성，위음다과연공작자제공료일개가행적사로。
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.