摘要
通过对液路耦联的多发动机系统动态特性仿真研究表明：多发动机开关机时水击对相互间性能影响比较大，若设计不合理，有可能导致异常关机。给出的动力学模型可以用于空间飞行器耦联多发动机系统的结构及工作模式设计和解释一些发动机试车现象。
The dynamic characteristics of liquid feed line coupled multi engine system was studied. The results show that the dynamic characteristics is greatly affected by water hammer during the operation of engine startup and shutdown. Seriously, engine abnormal shutdown caused due to the irrational design. The dynamic model given here can be applied directly to the design of engine structure and operation modes,and to explain relevant phenomena occurring in the engine test
出处
《推进技术》
EI
CAS
CSCD
北大核心
1999年第4期22-25,共4页
Journal of Propulsion Technology
关键词
液体火箭发动机
液路耦联
开关机
动态特性
Liquid propellant rocket engine,Rocket engine fuel system,Water impingement, Dynamic simulation,Dynamic characteristic
