某导弹发射车发电机的热设计分析  

Thermal Design Analysis of a Missile Launch Vehicle Generator

作　　者：刘晓斌 李正宇 朱李礼 李轩 张小虎 LIU Xiaobin;LI Zhengyu;ZHU Lili;LI Xuan;ZHANG Xiaohu(Xi’an Modern Control Technology Research Institute,Xi’an 710065,China;The Army Engineering University of PLA Communications Officer School,Chongqing 400035,China)

机构地区：[1]西安现代控制技术研究所,西安710065 [2]陆军工程大学通信士官学校,重庆400035

出　　处：《弹箭与制导学报》2021年第1期105-108,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：针对发电机运行时发热较大且影响输出功率的问题,从某导弹发射车工程样机设计入手,阐述了该型发电机的概念和功能。通过热设计分析,在工程样机阶段优化并解决了该型发电机发热较大的问题,提高了导弹发射车对战场环境和智能化扩展的适应能力。这种热设计分析方法对该系列发电机在导弹发射车中的应用具有指导意义。In view of the problem that this type of generator generates large heat and affects the output power during operation,this paper starts with the design of an engineering prototype of a missile launch vehicle and expounds the concept and function of this type of generator。Through thermal design analysis,the problem of large heating of this type of generator is optimized and solved in the stage of engineering prototype,and adaptability of missile launch vehicle to battlefield environment and intelligent expansion is improved.This thermal design analysis method has very important engineering design guiding significance for the application of this series of generators in missile launch vehicles.

关 键 词：发电机 热设计 散热 

分 类 号：TJ768.28[兵器科学与技术—武器系统与运用工程] TM352[电气工程—电机]