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液体火箭发动机一种通用模块化仿真方法
引用本文:魏鹏飞,吴建军,刘洪刚,陈启智.液体火箭发动机一种通用模块化仿真方法[J].推进技术,2005,26(2):147-150.
作者姓名:魏鹏飞  吴建军  刘洪刚  陈启智
作者单位:国防科技大学,航天与材料工程学院,湖南,长沙,410073
基金项目:国家自然科学基金资助项目 (50276068)。
摘    要:为了研制一种较为通用的液体火箭发动机工作过程的仿真软件,依据模块化建模思想,建立发动机各组件的Simulink仿真模块。根据发动机系统中各组件之间的参数信号传递关系,连接各模块的相应输入输出端口即形成整个发动机系统的仿真模型。对某型发动机的起动过程进行仿真计算,结果表明这种模块化的建模仿真方法易操作,较通用。

关 键 词:液体推进剂火箭发动机  模块化设计  仿真模型  数值仿真
文章编号:1001-4055(2005)02-0147-04
修稿时间:2004年5月9日

Investigation of a general module simulation method for liquid propellant rocket engines
WEI Peng-fei,WU Jian-jun,LIU Hong-gang and CHEN Qi-zhi.Investigation of a general module simulation method for liquid propellant rocket engines[J].Journal of Propulsion Technology,2005,26(2):147-150.
Authors:WEI Peng-fei  WU Jian-jun  LIU Hong-gang and CHEN Qi-zhi
Institution:Inst. of Aerospace and Material Engineering,National Univ. of Defence Technology,Changsha 410073,China;Inst. of Aerospace and Material Engineering,National Univ. of Defence Technology,Changsha 410073,China;Inst. of Aerospace and Material Engineering,National Univ. of Defence Technology,Changsha 410073,China;Inst. of Aerospace and Material Engineering,National Univ. of Defence Technology,Changsha 410073,China
Abstract:According to module modeling requirements, the components and the parts in a liquid propellant rocket engine (LRE) were classified firstly. Then, the simulation blocks of LRE components and parts based on MATLAB Simulink were constructed, which can be used to develop a universal simulation software for LRE dynamic characteristics study. Based on the parameter signal transfer relations between LRE components and parts, the LRE simulation model can be set up by connecting the corresponding LRE component input and output ports. The startup process of a certain LRE was simulated. The results show that this simulation method is effective, easier to operate, and more general.
Keywords:Liquid propellant rocket engine  Modularized design  Simulation model  Numerical simulation
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