某型便携发控系统观瞄发控装置瞬态热仿真分析  

Transient Thermal Simulation Analysis of the Sighting and Launching Control Device of a Portable Launching Control System

作　　者：曾志 惠博 周航 ZENG Zhi;HUI Bo;ZHOU Hang(The 115 Department of 41st Institute of Fourth Academy of CASC,Xi'an,Shaanxi Province,710025 China;The Headquarters of Fourth Academy of CASC,Xi'an,Shaanxi Province,710025 China)

机构地区：[1]中国航天科技集团公司第四研究院第41研究所115室,陕西西安710025 [2]中国航天科技集团公司第四研究院院本部,陕西西安710025

出　　处：《科技创新导报》2020年第28期83-87,97,共6页Science and Technology Innovation Herald

摘　　要：某型便携发控系统观瞄发控装置是某型导弹武器系统的重要组成部分,本文根据观瞄发控装置内部各组件的功耗情况以及工作的环境温度,对观瞄发控装置三维模型进行了合理简化,应用热仿真分析软件进行了观瞄发控装置任务周期内的瞬态热仿真分析,并对仿真结果进行了分析,所获得的结果对观瞄发控装置的设计具有重要的参考价值。The sighting and launch control device of a portable launching control system is an important part of a missile weapon system.According to the power consumption of each component of the sighting and launching control device and the working environment temperature,the three-dimensional model of the sighting and launching control device is rationally simplified and the transient thermal simulation analysis of the sighting and launching control device in the mission cycle is carried out by using Flotherm XT thermal simulation analysis software.The simulation results are analyzed,and the obtained results have important reference value for the design of the sighting and launching control device.

关 键 词：发控系统 密闭机箱 瞬态 热仿真 

分 类 号：V243[航空宇航科学与技术—飞行器设计]